Sample records for shock compressed iron

  1. Electrical Conductivity of ɛ-Iron under Shock Compression up to 208G Pa

    NASA Astrophysics Data System (ADS)

    Bi, Yan; Tan, Hua; Jing, Fu-Qian

    2002-02-01

    The electrical conductivity of shock-compressed iron was measured up to 208 GPa by using an improved design in experiment assembly in which the iron sample was encapsulated in a single-crystal sapphire cell. High-pressure shock compressions were generated by the plate impact technique with the two-stage light-gas gun. The measured conductivity of iron varies from 1.45×104 Ω-1 cm-1 at 101 GPa and 2010 K to 7.65×103 Ω-1 cm-1 at 208 GPa and 5220 K. After examining these data together with those reported, we found that the Bloch-Grüneisen expression is still valid at high pressures and temperatures, even up to 208 GPa and 5220 K, at least for ɛ-iron, which is significant in the field of condensed matter physics and deep interior earth science.

  2. The α-γ-ɛ triple point and phase boundaries of iron under shock compression

    NASA Astrophysics Data System (ADS)

    Li, Jun; Wu, Qiang; Xue, Tao; Geng, Huayun; Yu, Jidong; Jin, Ke; Li, Jiabo; Tan, Ye; Xi, Feng

    2017-07-01

    The phase transition of iron under shock compression has attracted much attention in recent decades because of its importance in fields such as condensed matter physics, geophysics, and metallurgy. At room temperature, the transition of iron from the α-phase (bcc) to the ɛ-phase (hpc) occurs at a stress of 13 GPa. At high temperature, a triple point followed by transformation to the γ-phase (fcc) is expected. However, the details of the high-temperature phase transitions of iron are still under debate. Here, we investigate the phase-transition behavior of polycrystalline iron under compression from room temperature to 820 K. The results show that the shock-induced phase transition is determined unequivocally from the measured three-wave-structure profiles, which clearly consist of an elastic wave, a plastic wave, and a phase-transition wave. The phase transition is temperature-dependent, with an average rate Δσtr/ΔT of -6.91 MPa/K below 700 K and -34.7 MPa/K at higher temperatures. The shock α-ɛ and α-γ phase boundaries intersect at 10.6 ± 0.53 GPa and 763 K, which agrees with the α-ɛ-γ triple point from early shock wave experiments and recent laser-heated diamond-anvil cell resistivity and in situ X-ray diffraction data but disagrees with the shock pressure-temperature phase diagram reported in 2009 by Zaretsky [J. Appl. Phys. 106, 023510 (2009)].

  3. Solid - solid and solid - liquid phase transitions of iron and iron alloys under laser shock compression

    NASA Astrophysics Data System (ADS)

    Harmand, M.; Krygier, A.; Appel, K.; Galtier, E.; Hartley, N.; Konopkova, Z.; Lee, H. J.; McBride, E. E.; Miyanishi, K.; Nagler, B.; Nemausat, R.; Vinci, T.; Zhu, D.; Ozaki, N.; Fiquet, G.

    2017-12-01

    An accurate knowledge of the properties of iron and iron alloys at high pressures and temperatures is crucial for understanding and modelling planetary interiors. While Earth-size and Super-Earth Exoplanets are being discovered in increasingly large numbers, access to detailed information on liquid properties, melting curves and even solid phases of iron and iron at the pressures and temperatures of their interiors is still strongly limited. In this context, XFEL sources coupled with high-energy lasers afford unique opportunities to measure microscopic structural properties at far extreme conditions. Also the achievable time resolution allows the shock history and phase transition mechanisms to be followed during laser compression, improving our understanding of the high pressure and high strain experiments. Here we present recent studies devoted to investigate the solid-solid and solid-liquid transition in laser-shocked iron and iron alloys (Fe-Si, Fe-C and Fe-O alloys) using X-ray diffraction and X-ray diffuse scattering. Experiment were performed at the MEC end-station of the LCLS facility at SLAC (USA). Detection of the diffuse scattering allowed the identification of the first liquid peak position along the Hugoniot, up to 4 Mbar. The time resolution shows ultrafast (between several tens and several hundreds of picoseconds) solid-solid and solid-liquid phase transitions. Future developments at XFEL facilities will enable detailed studies of the solid and liquid structures of iron and iron alloys as well as out-of-Hugoniot studies.

  4. Shock wave compression of iron-silicate garnet.

    NASA Technical Reports Server (NTRS)

    Graham, E. K.; Ahrens, T. J.

    1973-01-01

    Shock wave compression data to over 650 kb are presented for single-crystal almandine garnet. The data indicate the initiation of a phase transformation near 200 kb. Total transition to the high-pressure polymorph occurs at approximately 300 kb. The elastic properties of the high-pressure phase are calculated from the metastable Hugoniot data by using the linear shock velocity-particle velocity relationships. The overall results obtained strongly suggest that upper mantle minerals are likely to occur in the ilmenite structure over a substantial part of the lower mantle.

  5. Dynamic X-ray diffraction observation of shocked solid iron up to 170 GPa

    PubMed Central

    Denoeud, Adrien; Ozaki, Norimasa; Benuzzi-Mounaix, Alessandra; Uranishi, Hiroyuki; Kondo, Yoshihiko; Kodama, Ryosuke; Brambrink, Erik; Ravasio, Alessandra; Bocoum, Maimouna; Boudenne, Jean-Michel; Harmand, Marion; Guyot, François; Mazevet, Stephane; Riley, David; Makita, Mikako; Sano, Takayoshi; Sakawa, Youichi; Inubushi, Yuichi; Gregori, Gianluca; Koenig, Michel; Morard, Guillaume

    2016-01-01

    Investigation of the iron phase diagram under high pressure and temperature is crucial for the determination of the composition of the cores of rocky planets and for better understanding the generation of planetary magnetic fields. Here we present X-ray diffraction results from laser-driven shock-compressed single-crystal and polycrystalline iron, indicating the presence of solid hexagonal close-packed iron up to pressure of at least 170 GPa along the principal Hugoniot, corresponding to a temperature of 4,150 K. This is confirmed by the agreement between the pressure obtained from the measurement of the iron volume in the sample and the inferred shock strength from velocimetry deductions. Results presented in this study are of the first importance regarding pure Fe phase diagram probed under dynamic compression and can be applied to study conditions that are relevant to Earth and super-Earth cores. PMID:27357672

  6. Shock temperature measurement of transparent materials under shock compression

    NASA Astrophysics Data System (ADS)

    Hu, Jinbiao

    1999-06-01

    Under shock compression, some materials have very small absorptance. So it's emissivity is very small too. For this kinds of materials, although they stand in high temperature state under shock compression, the temperature can not be detected easily by using optical radiation technique because of the low emissivity. In this paper, an optical radiation temperature measurement technique of measuring temperature of very low emissive material under shock compression was proposed. For making sure this technique, temperature of crystal NaCl at shock pressure 41 GPa was measured. The result agrees with the results of Kormer et al and Ahrens et al very well. This shows that this technique is reliable and can be used to measuring low emissive shock temperature.

  7. Dynamic strength properties and alpha-phase shock Hugoniot of iron and steel

    NASA Astrophysics Data System (ADS)

    Thomas, S. A.; Hawkins, M. C.; Matthes, M. K.; Gray, G. T.; Hixson, R. S.

    2018-05-01

    The properties of iron and steel are of considerable interest scientifically to the dynamic materials properties' community, as well as to a broader audience, for many applications. This is true in part because of the existence of a solid-solid phase (α-ɛ) transition at relatively modest stress (13 GPa). Because of this, there is a significant amount of data on iron and steel alloy shock compression properties at stresses above 13 GPa, but much less fundamental data under stress conditions lower than that, where the metals are in the α-phase. New data have been obtained under relatively low stress (below 10 GPa) conditions in which samples are subjected to low-velocity symmetric impact on the order of 0.2 to 0.4 km/s. We used well-developed flyer plate impact methods combined with velocity interferometry to measure wave speeds and strength properties in compression and tension. The shock α-phase Hugoniot data reported here are compared with literature values. A comparison of spall strength and Hugoniot elastic limit is made between different types of steel studied and for pure iron.

  8. Quasi-isentropic Compression of Iron and Magnesium Oxide to 3 Mbar at the Omega Laser Facility

    NASA Astrophysics Data System (ADS)

    Wang, J.; Smith, R. F.; Coppari, F.; Eggert, J. H.; Boehly, T.; Collins, G.; Duffy, T. S.

    2011-12-01

    Developing a high-pressure, modest temperature ramp compression drive permits exploration of new regions of thermodynamic space, inaccessible through traditional methods of shock or static compression, and of particular relevance to material conditions found in planetary interiors both within and outside our solar system. Ramp compression is a developing technique that allows materials to be compressed along a quasi-isentropic path and provides the ability to study materials in the solid state to higher pressures than can be achieved with diamond anvil cell or shock wave methods. Iron and magnesium oxide are geologically important materials each representative of one of the two major interior regions (core and mantle) of terrestrial planets. An experimental platform for ramp loading of iron (Fe) and magnesium oxide (MgO), has been established and tested in experiments at the Omega Laser Facility, University of Rochester. Omega is a 60-beam ultraviolet (352 nm) neodymium glass laser which is capable of delivery kilojoules of energy in ~10 ns pulses onto targets of a few mm in dimension. In the current experiments, we used a composite ramped laser pulse involving typically 15 beams with total energy of 2.6-3.3 kJ. The laser beams were used to launch spatially planar ramp compression waves into Fe and MgO targets. Each target had four steps that were approximately 5-7 μm thick. Detection of the ramp wave arrival and its velocity at the free surface of each step was made using a VISAR velocity interferometer. Through the use of Lagrangian analysis on the measured wave profiles, stress-density states in iron and magnesium oxide have been determined to pressures of 291 GPa and 260 GPa respectively. For Fe, the α-ɛ transition of iron is overdriven by an initial shock pulse of ~90.1 GPa followed by ramp compression to the peak pressure. The results will be compared with shock compression and diamond anvil cell data for both materials.

  9. Thermophysical properties of multi-shock compressed dense argon.

    PubMed

    Chen, Q F; Zheng, J; Gu, Y J; Chen, Y L; Cai, L C; Shen, Z J

    2014-02-21

    In contrast to the single shock compression state that can be obtained directly via experimental measurements, the multi-shock compression states, however, have to be calculated with the aid of theoretical models. In order to determine experimentally the multiple shock states, a diagnostic approach with the Doppler pins system (DPS) and the pyrometer was used to probe multiple shocks in dense argon plasmas. Plasma was generated by a shock reverberation technique. The shock was produced using the flyer plate impact accelerated up to ∼6.1 km/s by a two-stage light gas gun and introduced into the plenum argon gas sample, which was pre-compressed from the environmental pressure to about 20 MPa. The time-resolved optical radiation histories were determined using a multi-wavelength channel optical transience radiance pyrometer. Simultaneously, the particle velocity profiles of the LiF window was measured with multi-DPS. The states of multi-shock compression argon plasma were determined from the measured shock velocities combining the particle velocity profiles. We performed the experiments on dense argon plasmas to determine the principal Hugonoit up to 21 GPa, the re-shock pressure up to 73 GPa, and the maximum measure pressure of the fourth shock up to 158 GPa. The results are used to validate the existing self-consistent variational theory model in the partial ionization region and create new theoretical models.

  10. Thermophysical properties of multi-shock compressed dense argon

    NASA Astrophysics Data System (ADS)

    Chen, Q. F.; Zheng, J.; Gu, Y. J.; Chen, Y. L.; Cai, L. C.; Shen, Z. J.

    2014-02-01

    In contrast to the single shock compression state that can be obtained directly via experimental measurements, the multi-shock compression states, however, have to be calculated with the aid of theoretical models. In order to determine experimentally the multiple shock states, a diagnostic approach with the Doppler pins system (DPS) and the pyrometer was used to probe multiple shocks in dense argon plasmas. Plasma was generated by a shock reverberation technique. The shock was produced using the flyer plate impact accelerated up to ˜6.1 km/s by a two-stage light gas gun and introduced into the plenum argon gas sample, which was pre-compressed from the environmental pressure to about 20 MPa. The time-resolved optical radiation histories were determined using a multi-wavelength channel optical transience radiance pyrometer. Simultaneously, the particle velocity profiles of the LiF window was measured with multi-DPS. The states of multi-shock compression argon plasma were determined from the measured shock velocities combining the particle velocity profiles. We performed the experiments on dense argon plasmas to determine the principal Hugonoit up to 21 GPa, the re-shock pressure up to 73 GPa, and the maximum measure pressure of the fourth shock up to 158 GPa. The results are used to validate the existing self-consistent variational theory model in the partial ionization region and create new theoretical models.

  11. Interaction of two laser shocks inside iron samples

    NASA Astrophysics Data System (ADS)

    de Rességuier, T.; Hallouin, M.

    2001-11-01

    The interaction of two plane symmetric shocks in a solid sample induces a significant increase of both the pressure and the temperature in the central zone where the incident compressive pulses cross each other. In iron samples, such loading conditions may produce typical structural defects (twins, dislocations) and phase transitions that can be revealed by posttest examination of the recovered targets. We have used two high-power laser beams to irradiate simultaneously both surfaces of thin iron foils. The recovered samples have been sectioned and observed in optical microscopy. A very dense twin distribution in the central zone has confirmed the pressure amplification due to the interaction of the incident shocks. The occurrence of a phase transition has been inferred from the presence of short characteristic twins. Spall fraction has been observed near both irradiated surfaces, and additional damage has been evidenced at the center of the samples. Numerical tools have been adapted to simulate the experiments. Computations have provided estimates of the stress histories inside the samples, and the ability of simple twin, phase change, and spall models has been tested to predict the observed results.

  12. Optical Radiation from Shock-Compressed Materials. Ph.D. Thesis

    NASA Technical Reports Server (NTRS)

    Svendsen, Robert F., Jr.

    1987-01-01

    Recent observations of shock-induced radiation from oxides, silicates, and metals of geophysical interest constrain the shock-compressed temperature of these materials. The relationships between the temperature inferred from the observed radiation and the temperature of the shock-compressed film or foil and/or window were investigated. Changes of the temperature field in each target component away from that of their respective shock-compressed states occur because of: shock-impedance mismatch between target components; thermal mismatch between target components; surface roughness at target interfaces; and conduction within and between target components. In particular, conduction may affect the temperature of the film/foil window interface on the time scale of the experiments, and so control the intensity and history of the dominant thermal radiation sources in the target. This type of model was used to interpret the radiation emitted by a variety of shock-compressed materials and interfaces.

  13. Shock-wave studies of anomalous compressibility of glassy carbon

    DOE Office of Scientific and Technical Information (OSTI.GOV)

    Molodets, A. M., E-mail: molodets@icp.ac.ru; Golyshev, A. A.; Savinykh, A. S.

    2016-02-15

    The physico-mechanical properties of amorphous glassy carbon are investigated under shock compression up to 10 GPa. Experiments are carried out on the continuous recording of the mass velocity of compression pulses propagating in glassy carbon samples with initial densities of 1.502(5) g/cm{sup 3} and 1.55(2) g/cm{sup 3}. It is shown that, in both cases, a compression wave in glassy carbon contains a leading precursor with amplitude of 0.135(5) GPa. It is established that, in the range of pressures up to 2 GPa, a shock discontinuity in glassy carbon is transformed into a broadened compression wave, and shock waves are formedmore » in the release wave, which generally means the anomalous compressibility of the material in both the compression and release waves. It is shown that, at pressure higher than 3 GPa, anomalous behavior turns into normal behavior, accompanied by the formation of a shock compression wave. In the investigated area of pressure, possible structural changes in glassy carbon under shock compression have a reversible character. A physico-mechanical model of glassy carbon is proposed that involves the equation of state and a constitutive relation for Poisson’s ratio and allows the numerical simulation of physico-mechanical and thermophysical properties of glassy carbon of different densities in the region of its anomalous compressibility.« less

  14. Hugoniot and refractive indices of bromoform under shock compression

    NASA Astrophysics Data System (ADS)

    Liu, Q. C.; Zeng, X. L.; Zhou, X. M.; Luo, S. N.

    2018-01-01

    We investigate physical properties of bromoform (liquid CHBr3) including compressibility and refractive index under dynamic extreme conditions of shock compression. Planar shock experiments are conducted along with high-speed laser interferometry. Our experiments and previous results establish a linear shock velocity-particle velocity relation for particle velocities below 1.77 km/s, as well as the Hugoniot and isentropic compression curves up to ˜21 GPa. Shock-state refractive indices of CHBr3 up to 2.3 GPa or ˜26% compression, as a function of density, can be described with a linear relation and follows the Gladstone-Dale relation. The velocity corrections for laser interferometry measurements at 1550 nm are also obtained.

  15. Dissipative processes under the shock compression of glass

    NASA Astrophysics Data System (ADS)

    Savinykh, A. S.; Kanel, G. I.; Cherepanov, I. A.; Razorenov, S. V.

    2016-03-01

    New experimental data on the behavior of the K8 and TF1 glasses under shock-wave loading conditions are obtained. It is found that the propagation of shock waves is close to the self-similar one in the maximum compression stress range 4-12 GPa. Deviations from a general deformation diagram, which are related to viscous dissipation, take place when the final state of compression is approached. The parameter region in which failure waves form in glass is found not to be limited to the elastic compression stress range, as was thought earlier. The failure front velocity increases with the shock compression stress. Outside the region covered by a failure wave, the glasses demonstrate a high tensile dynamic strength (6-7 GPa) in the case of elastic compression, and this strength is still very high after transition through the elastic limit in a compression wave.

  16. Shock waves in weakly compressed granular media.

    PubMed

    van den Wildenberg, Siet; van Loo, Rogier; van Hecke, Martin

    2013-11-22

    We experimentally probe nonlinear wave propagation in weakly compressed granular media and observe a crossover from quasilinear sound waves at low impact to shock waves at high impact. We show that this crossover impact grows with the confining pressure P0, whereas the shock wave speed is independent of P0-two hallmarks of granular shocks predicted recently. The shocks exhibit surprising power law attenuation, which we model with a logarithmic law implying that shock dissipation is weak and qualitatively different from other granular dissipation mechanisms. We show that elastic and potential energy balance in the leading part of the shocks.

  17. Shock compression of [001] single crystal silicon

    NASA Astrophysics Data System (ADS)

    Zhao, S.; Hahn, E. N.; Kad, B.; Remington, B. A.; Bringa, E. M.; Meyers, M. A.

    2016-05-01

    Silicon is ubiquitous in our advanced technological society, yet our current understanding of change to its mechanical response at extreme pressures and strain-rates is far from complete. This is due to its brittleness, making recovery experiments difficult. High-power, short-duration, laser-driven, shock compression and recovery experiments on [001] silicon (using impedance-matched momentum traps) unveiled remarkable structural changes observed by transmission electron microscopy. As laser energy increases, corresponding to an increase in peak shock pressure, the following plastic responses are are observed: surface cleavage along {111} planes, dislocations and stacking faults; bands of amorphized material initially forming on crystallographic orientations consistent with dislocation slip; and coarse regions of amorphized material. Molecular dynamics simulations approach equivalent length and time scales to laser experiments and reveal the evolution of shock-induced partial dislocations and their crucial role in the preliminary stages of amorphization. Application of coupled hydrostatic and shear stresses produce amorphization below the hydrostatically determined critical melting pressure under dynamic shock compression.

  18. Frequency shift measurement in shock-compressed materials

    DOEpatents

    Moore, David S.; Schmidt, Stephen C.

    1985-01-01

    A method for determining molecular vibrational frequencies in shock-compressed transparent materials. A single laser beam pulse is directed into a sample material while the material is shock-compressed from a direction opposite that of the incident laser beam. A Stokes beam produced by stimulated Raman scattering is emitted back along the path of the incident laser beam, that is, in the opposite direction to that of the incident laser beam. The Stokes beam is separated from the incident beam and its frequency measured. The difference in frequency between the Stokes beam and the incident beam is representative of the characteristic frequency of the Raman active mode of the sample. Both the incident beam and the Stokes beam pass perpendicularly through the shock front advancing through the sample, thereby minimizing adverse effects of refraction.

  19. Compression Shocks in Two-Dimensional Gas Flows

    NASA Technical Reports Server (NTRS)

    Busemann, A.

    1949-01-01

    The following are arguments on the compression shocks in gas flow start with a simplified representation of the results of the study made by Th. Meyer as published in the Forschungsheft 62 of the VDI, supplemented by several amplifications for the application.In the treatment of compression shocks, the equation of energy, the equation of continuity, the momentum equation, the equation of state of the particular gas, as well as the condition Of the second law of thermodynamics that no decrease of entropy is possible in an isolated system, must be taken into consideration. The result is that, in those cases where the sudden change of state according to the second law of thermodynamics is possible, there always occurs a compression of the gas which is uniquely determined by the other conditions.

  20. In situ X-Ray Diffraction of Shock-Compressed Fused Silica

    NASA Astrophysics Data System (ADS)

    Tracy, Sally June; Turneaure, Stefan J.; Duffy, Thomas S.

    2018-03-01

    Because of its widespread applications in materials science and geophysics, SiO2 has been extensively examined under shock compression. Both quartz and fused silica transform through a so-called "mixed-phase region" to a dense, low compressibility high-pressure phase. For decades, the nature of this phase has been a subject of debate. Proposed structures include crystalline stishovite, another high-pressure crystalline phase, or a dense amorphous phase. Here we use plate-impact experiments and pulsed synchrotron x-ray diffraction to examine the structure of fused silica shock compressed to 63 GPa. In contrast to recent laser-driven compression experiments, we find that fused silica adopts a dense amorphous structure at 34 GPa and below. When compressed above 34 GPa, fused silica transforms to untextured polycrystalline stishovite. Our results can explain previously ambiguous features of the shock-compression behavior of fused silica and are consistent with recent molecular dynamics simulations. Stishovite grain sizes are estimated to be ˜5 - 30 nm for compression over a few hundred nanosecond time scale.

  1. Shock compression of [001] single crystal silicon

    DOE PAGES

    Zhao, S.; Remington, B.; Hahn, E. N.; ...

    2016-03-14

    Silicon is ubiquitous in our advanced technological society, yet our current understanding of change to its mechanical response at extreme pressures and strain-rates is far from complete. This is due to its brittleness, making recovery experiments difficult. High-power, short-duration, laser-driven, shock compression and recovery experiments on [001] silicon (using impedance-matched momentum traps) unveiled remarkable structural changes observed by transmission electron microscopy. As laser energy increases, corresponding to an increase in peak shock pressure, the following plastic responses are are observed: surface cleavage along {111} planes, dislocations and stacking faults; bands of amorphized material initially forming on crystallographic orientations consistent withmore » dislocation slip; and coarse regions of amorphized material. Molecular dynamics simulations approach equivalent length and time scales to laser experiments and reveal the evolution of shock-induced partial dislocations and their crucial role in the preliminary stages of amorphization. Furthermore, application of coupled hydrostatic and shear stresses produce amorphization below the hydrostatically determined critical melting pressure under dynamic shock compression.« less

  2. Fast Electron Deposition in Laser Shock Compressed Plastic Targets

    NASA Astrophysics Data System (ADS)

    Hall, T. A.; Ellwi, S.; Batani, D.; Bernardinello, A.; Masella, V.; Koenig, M.; Benuzzi, A.; Krishnan, J.; Pisani, F.; Djaoui, A.; Norreys, P.; Neely, D.; Rose, S.; Key, M. H.; Fews, P.

    1998-08-01

    We present the first results of fast electron deposition in a laser shock compressed plasma. The interaction of a 3 ps, 15 J laser pulse with solid polyethylene targets is used to produce fast electrons on one side of foil targets and a 2 ns duration laser pulse is used to drive a shock wave into the target from the opposite side. Kα emission from chlorine fluor buried layers is used to measure the electron transport. The hot electron range in the shock compressed plastic is found to be approximately twice as large as the range in the solid density plastic.

  3. Bacterial survival following shock compression in the GigaPascal range

    NASA Astrophysics Data System (ADS)

    Hazael, Rachael; Fitzmaurice, Brianna C.; Foglia, Fabrizia; Appleby-Thomas, Gareth J.; McMillan, Paul F.

    2017-09-01

    The possibility that life can exist within previously unconsidered habitats is causing us to expand our understanding of potential planetary biospheres. Significant populations of living organisms have been identified at depths extending up to several km below the Earth's surface; whereas laboratory experiments have shown that microbial species can survive following exposure to GigaPascal (GPa) pressures. Understanding the degree to which simple organisms such as microbes survive such extreme pressurization under static compression conditions is being actively investigated. The survival of bacteria under dynamic shock compression is also of interest. Such studies are being partly driven to test the hypothesis of potential transport of biological organisms between planetary systems. Shock compression is also of interest for the potential modification and sterilization of foodstuffs and agricultural products. Here we report the survival of Shewanella oneidensis bacteria exposed to dynamic (shock) compression. The samples examined included: (a) a "wild type" (WT) strain and (b) a "pressure adapted" (PA) population obtained by culturing survivors from static compression experiments to 750 MPa. Following exposure to peak shock pressures of 1.5 and 2.5 GPa the proportion of survivors was established as the number of colony forming units (CFU) present after recovery to ambient conditions. The data were compared with previous results in which the same bacterial samples were exposed to static pressurization to the same pressures, for 15 minutes each. The results indicate that shock compression leads to survival of a significantly greater proportion of both WT and PA organisms. The significantly shorter duration of the pressure pulse during the shock experiments (2-3 μs) likely contributes to the increased survival of the microbial species. One reason for this can involve the crossover from deformable to rigid solid-like mechanical relaxational behavior that occurs for

  4. Proton spectra diagnostics for shock-compression studies

    NASA Astrophysics Data System (ADS)

    Welch, D. R.; Harris, D. B.; Bennish, A. H.; Miley, G. H.

    1984-12-01

    The energy spectra of fusion products escaping long-pulse-length laser-imploded deuterium-tritium filled glass microballoons have been measured with a time-of-flight spectrometer. The D(d,p)T reaction proton energy spectra showed two distinct peaks, indicating two burn phases in the target. The first burn phase is attributed to a spherically converging shock, while the second is attributed to subsequent compression heating. The analysis of these spectra provides the first conclusive proof of significant compression yields in these targets, where approximately half of the yield occurs during the compression burn phase.

  5. Dynamic XRD, Shock and Static Compression of CaF2

    NASA Astrophysics Data System (ADS)

    Kalita, Patricia; Specht, Paul; Root, Seth; Sinclair, Nicholas; Schuman, Adam; White, Melanie; Cornelius, Andrew; Smith, Jesse; Sinogeikin, Stanislav

    2017-06-01

    The high-pressure behavior of CaF2 is probed with x-ray diffraction (XRD) combined with both dynamic compression, using a two-stage light gas gun, and static compression, using diamond anvil cells. We use XRD to follow the unfolding of a shock-driven, fluorite to cotunnite phase transition, on the timescale of nanoseconds. The dynamic behavior of CaF2 under shock loading is contrasted with that under static compression. This work leverages experimental capabilities at the Advanced Photon Source: dynamic XRD and shock experiments at the Dynamic Compression Sector, as well as XRD and static compression in diamond anvil cell at the High-Pressure Collaborative Access Team. These experiments and cross-platform comparisons, open the door to an unprecedented understanding of equations of state and phase transitions at the microstructural level and at different time scales and will ultimately improve our capability to simulate the behavior of materials at extreme conditions. Sandia National Laboratories is a multi-mission laboratory managed and operated by Sandia Corporation, a wholly owned subsidiary of Lockheed Martin Corporation, for the U.S. Department of Energy's National Nuclear Security Administration under contract DE-AC04-94AL85000.

  6. Equation of state for shock compression of distended solids

    NASA Astrophysics Data System (ADS)

    Grady, Dennis; Fenton, Gregg; Vogler, Tracy

    2014-05-01

    Shock Hugoniot data for full-density and porous compounds of boron carbide, silicon dioxide, tantalum pentoxide, uranium dioxide and playa alluvium are investigated for the purpose of equation-of-state representation of intense shock compression. Complications of multivalued Hugoniot behavior characteristic of highly distended solids are addressed through the application of enthalpy-based equations of state of the form originally proposed by Rice and Walsh in the late 1950's. Additive measures of cold and thermal pressure intrinsic to the Mie-Gruneisen EOS framework is replaced by isobaric additive functions of the cold and thermal specific volume components in the enthalpy-based formulation. Additionally, experimental evidence reveals enhancement of shock-induced phase transformation on the Hugoniot with increasing levels of initial distension for silicon dioxide, uranium dioxide and possibly boron carbide. Methods for addressing this experimentally observed feature of the shock compression are incorporated into the EOS model.

  7. Anomalous elastic response of silicon to uniaxial shock compression on nanosecond time scales.

    PubMed

    Loveridge-Smith, A; Allen, A; Belak, J; Boehly, T; Hauer, A; Holian, B; Kalantar, D; Kyrala, G; Lee, R W; Lomdahl, P; Meyers, M A; Paisley, D; Pollaine, S; Remington, B; Swift, D C; Weber, S; Wark, J S

    2001-03-12

    We have used x-ray diffraction with subnanosecond temporal resolution to measure the lattice parameters of orthogonal planes in shock compressed single crystals of silicon (Si) and copper (Cu). Despite uniaxial compression along the (400) direction of Si reducing the lattice spacing by nearly 11%, no observable changes occur in planes with normals orthogonal to the shock propagation direction. In contrast, shocked Cu shows prompt hydrostaticlike compression. These results are consistent with simple estimates of plastic strain rates based on dislocation velocity data.

  8. Experimental Study of Shock Generated Compressible Vortex Ring

    NASA Astrophysics Data System (ADS)

    Das, Debopam; Arakeri, Jaywant H.; Krothapalli, Anjaneyulu

    2000-11-01

    Formation of a compressible vortex ring and generation of sound associated with it is studied experimentally. Impulse of a shock wave is used to generate a vortex ring from the open end of a shock-tube. Vortex ring formation process has been studied in details using particle image Velocimetry (PIV). As the shock wave exits the tube it diffracts and expands. A circular vortex sheet forms at the edge and rolls up into a vortex ring. Far field microphone measurement shows that the acoustic pressure consists of a spike due to shock wave followed by a low frequency pressure wave of decaying nature, superimposed with high frequency pressure wave. Acoustic waves consist of waves due to expansion, waves formed in the tube during diaphragm breakage and waves associated with the vortex ring and shear-layer vortices. Unsteady evolution of the vortex ring and shear-layer vortices in the jet behind the ring is studied by measuring the velocity field using PIV. Corresponding vorticity field, circulation around the vortex core and growth rate of the vortex core is calculated from the measured velocity field. The velocity field in a compressible vortex ring differs from that of an incompressible ring due to the contribution from both shock and vortex ring.

  9. Transparency of the strong shock-compressed diamond for 532 nm laser light

    DOE Office of Scientific and Technical Information (OSTI.GOV)

    Zhang, Zhiyu; Department of Engineering Physics, Tsinghua University, Beijing 100084; Zhao, Yang

    2016-04-15

    An optical reflectivity and transmissivity model for the shock-compressed diamond is established and used to calculate the optical reflectivity and transmissivity of the diamond under different shock compressions. The simulated results indicate that the reflection occurs at the shock front and does not depend on the thickness of the compressed diamond, but the transmissivity decreases with the thickness. The simulated reflectivity is consistent with the experimental results in the literature, which validates the model. It is shown that the diamond keeps transparent when the shock pressure is lower than 2.00 Mbar, and becomes opaque but does not reflect the probemore » laser as the shock pressure increases from 2.00 Mbar to 4.60 Mbar and reflects the probe laser markedly when the shock pressure is higher than 4.60 Mbar.« less

  10. Shock compression dynamics under a microscope.

    NASA Astrophysics Data System (ADS)

    Dlott, Dana

    2015-06-01

    We have developed a tabletop laser flyer launch system1 that solves many of the problems that plagued previous efforts. Using a novel mechanism where a spatially-uniform laser pulse creates a shock in a glass substrate just underneath a metal foil, we can launch tiny (0.7 mm diameter x 100 μm thick) flyers at speeds ranging from 0-5 km/s and the foils are flat, cold and intact. This tabletop launch system, where we often launch 100 flyers per day, provides a platform for a wide variety of time-resolved spectroscopies. The shocked material is viewed by a microscope objective that transmits near-infrared light from a photon Doppler velocimeter to monitor the flyer, and collects the light for spectroscopic and video images. Fluorescent probes, which have been highly developed for the biomedical sciences, have proven especially useful for these experiments. Using emission measurements, we have investigated the fundamental mechanisms of many shock wave effects including: viscoelastic compression of high molecular weight polymers, visualization of shocks in porous media such as sand, where we can observe the behavior of individual grains of sand, shock attenuation by passing the shock through reactive materials that undergo endothermic chemical reactions, and shock initiation of nanoenergetic materials.

  11. Amorphization and nanocrystallization of silcon under shock compression

    DOE PAGES

    Remington, B. A.; Wehrenberg, C. E.; Zhao, S.; ...

    2015-11-06

    High-power, short-duration, laser-driven, shock compression and recovery experiments on [001] silicon unveiled remarkable structural changes above a pressure threshold. Two distinct amorphous regions were identified: (a) a bulk amorphous layer close to the surface and (b) amorphous bands initially aligned with {111} slip planes. Further increase of the laser energy leads to the re-crystallization of amorphous silicon into nanocrystals with high concentration of nano-twins. This amorphization is produced by the combined effect of high magnitude hydrostatic and shear stresses under dynamic shock compression. Shock-induced defects play a very important role in the onset of amorphization. Calculations of the free energymore » changes with pressure and shear, using the Patel-Cohen methodology, are in agreement with the experimental results. Molecular dynamics simulation corroborates the amorphization, showing that it is initiated by the nucleation and propagation of partial dislocations. As a result, the nucleation of amorphization is analyzed qualitatively by classical nucleation theory.« less

  12. Frequency shift measurement in shock-compressed materials

    DOEpatents

    Moore, D.S.; Schmidt, S.C.

    1984-02-21

    A method is disclosed for determining molecular vibrational frequencies in shock-compressed transparent materials. A single laser beam pulse is directed into a sample material while the material is shock-compressed from a direction opposite that of the incident laser beam. A Stokes beam produced by stimulated Raman scattering is emitted back along the path of the incident laser beam, that is, in the opposite direction to that of the incident laser beam. The Stokes beam is separated from the incident beam and its frequency measured. The difference in frequency between the Stokes beam and the incident beam is representative of the characteristic frequency of the Raman active mode of the sample. Both the incident beam and the Stokes beam pass perpendicularly through the stock front advancing through the sample, thereby minimizing adverse effects of refraction.

  13. Ultrafast shock compression of self-assembled monolayers: a molecular picture.

    PubMed

    Patterson, James E; Dlott, Dana D

    2005-03-24

    Simulations of self-assembled monolayers (SAMs) are performed to interpret experimental measurements of ultrafast approximately 1 GPa (volume compression deltaV approximately 0.1) planar shock compression dynamics probed by vibrational sum-frequency generation (SFG) spectroscopy (Lagutchev, A. S.; Patterson, J. E.; Huang, W.; Dlott, D. D. J. Phys. Chem. B 2005, 109, XXXX). The SAMs investigated are octadecanethiol (ODT) and pentadecanethiol (PDT) on Au(111) and Ag(111) substrates, and benzyl mercaptan (BMT) on Au(111). In the alkane SAMs, SFG is sensitive to the instantaneous orientation of the terminal methyl; in BMT it is sensitive to the phenyl orientation. Computed structures of alkane SAMs are in good agreement with experiment. In alkanes, the energies of gauche defects increase with increasing number and depth below the methyl plane, with the exception of ODT/Au where both single and double gauche defects at the two uppermost dihedrals have similar energies. Simulations of isothermal uniaxial compression of SAM lattices show that chain and methyl tilting is predominant in PDT/Au, ODT/Ag and PDT/Ag, whereas single and double gauche defect formation is predominant in ODT/Au. Time-resolved shock data showing transient SFG signal loss of ODT/Au and PDT/Au are fit by calculations of the terminal group orientations as a function of deltaV and their contributions to the SFG hyperpolarizability. The highly elastic response of PDT/Au results from shock-generated methyl and chain tilting. The viscoelastic response of ODT/Au results from shock generation of single and double gauche defects. Isothermal compression simulations help explain and fit the time dependence of shock spectra but generally underestimate the magnitude of SFG signal loss because they do not include effects of high-strain-rate dynamics and shock front and surface irregularities.

  14. Ultrafast Kα x-ray Thomson scattering from shock compressed lithium hydride

    DOE PAGES

    Kritcher, A. L.; Neumayer, P.; Castor, J.; ...

    2009-04-13

    Spectrally and temporally resolved x-ray Thomson scattering using ultrafast Ti Kα x rays has provided experimental validation for modeling of the compression and heating of shocked matter. The coalescence of two shocks launched into a solid density LiH target by a shaped 6 ns heater beam was observed from rapid heating to temperatures of 2.2 eV, enabling tests of shock timing models. Here, the temperature evolution of the target at various times during shock progression was characterized from the intensity of the elastic scattering component. The observation of scattering from plasmons, electron plasma oscillations, at shock coalescence indicates a transitionmore » to a dense metallic plasma state in LiH. From the frequency shift of the measured plasmon feature the electron density was directly determined with high accuracy, providing a material compression of a factor of 3 times solid density. The quality of data achieved in these experiments demonstrates the capability for single shot dynamic characterization of dense shock compressed matter. Here, the conditions probed in this experiment are relevant for the study of the physics of planetary formation and to characterize inertial confinement fusion targets for experiments such as on the National Ignition Facility, Lawrence Livermore National Laboratory.« less

  15. Investigations of Compression Shocks and Boundary Layers in Gases Moving at High Speed

    NASA Technical Reports Server (NTRS)

    Ackeret, J.; Feldmann, F.; Rott, N.

    1947-01-01

    The mutual influences of compression shocks and friction boundary layers were investigated by means of high speed wind tunnels.Schlieren optics provided a clear picture of the flow phenomena and were used for determining the location of the compression shocks, measurement of shock angles, and also for Mach angles. Pressure measurement and humidity measurements were also taken into consideration.Results along with a mathematical model are described.

  16. Shock and Static Compression of Nitrobenzene

    NASA Astrophysics Data System (ADS)

    Kozu, Naoshi; Arai, Mitsuru; Tamura, Masamitsu; Fujihisa, Hiroshi; Aoki, Katsutoshi; Yoshida, Masatake

    2000-08-01

    The Hugoniot and static compression curve (isotherm) were investigated using explosive plane wave generators and diamond anvil cells, respectively. The obtained Hugoniot from the shock experiments is represented by two linear lines: Us=2.52+1.23 up (0.8shock velocity and the particle velocity in km/s, respectively. A kink exists at around 15 GPa. The line for the higher particle velocities agrees well with the Hugoniot of detonation products calculated by the CHEETAH code. This suggests that nitrobenzene detonates in this range. Under static high pressure over 7 GPa, nitrobenzene undergoes a reaction that is expected to be polymerization. Considering the Hugoniot and the isotherm, it is plausible that shocked nitrobenzene (<15 GPa) is in the liquid state.

  17. Shock Melting of Iron Silicide as Determined by In Situ X-ray Diffraction.

    NASA Astrophysics Data System (ADS)

    Newman, M.; Kraus, R. G.; Wicks, J. K.; Smith, R.; Duffy, T. S.

    2016-12-01

    The equation of state of core alloys at pressures and temperatures near the solid-liquid coexistence curve is important for understanding the dynamics at the inner core boundary of the Earth and super-Earths. Here, we present a series of laser driven shock experiments on textured polycrystalline Fe-15Si. These experiments were conducted at the Omega and Omega EP laser facilities. Particle velocities in the Fe-15Si samples were measured using a line VISAR and were used to infer the thermodynamic state of the shocked samples. In situ x-ray diffraction measurements were used to probe the melting transition and investigate the potential decomposition of Fe-15Si in to hcp and B2 structures. This work examines the kinetic effects of decomposition due to the short time scale of dynamic compression experiments. In addition, the thermodynamic data collected in these experiments adds to a limited body of information regarding the equation of state of Fe-15Si, which is a candidate for the composition in Earth's outer core. Our experimental results show a highly textured solid phase upon shock compression to pressures ranging from 170 to 300 GPa. Below 320 GPa, we observe diffraction peaks consistent with decomposition of the D03 starting material in to an hcp and a cubic (potentially B2) structure. Upon shock compression above 320 GPa, the intense and textured solid diffraction peaks give way to diffuse scattering and loss of texture, consistent with melting along the Hugoniot. When comparing these results to that of pure iron, we can ascertain that addition of 15 wt% silicon increases the equilibrium melting temperature significantly, or that the addition of silicon significantly increases the metastability of the solid phase, relative to the liquid. This work was performed under the auspices of the U.S. Department of Energy by Lawrence Livermore National Laboratory under Contract DE-AC52-07NA27344.

  18. Equation of State for Shock Compression of High Distension Solids

    NASA Astrophysics Data System (ADS)

    Grady, Dennis

    2013-06-01

    Shock Hugoniot data for full-density and porous compounds of boron carbide, silicon dioxide, tantalum pentoxide, uranium dioxide and playa alluvium are investigated for the purpose of equation-of-state representation of intense shock compression. Complications of multivalued Hugoniot behavior characteristic of highly distended solids are addressed through the application of enthalpy-based equations of state of the form originally proposed by Rice and Walsh in the late 1950's. Additivity of cold and thermal pressure intrinsic to the Mie-Gruneisen EOS framework is replaced by isobaric additive functions of the cold and thermal specific volume components in the enthalpy-based formulation. Additionally, experimental evidence supports acceleration of shock-induced phase transformation on the Hugoniot with increasing levels of initial distention for silicon dioxide, uranium dioxide and possibly boron carbide. Methods for addressing this experimentally observed facet of the shock compression are introduced into the EOS model.

  19. Time-resolved Sensing of Meso-scale Shock Compression with Multilayer Photonic Crystal Structures

    NASA Astrophysics Data System (ADS)

    Scripka, David; Lee, Gyuhyon; Summers, Christopher J.; Thadhani, Naresh

    2017-06-01

    Multilayer Photonic Crystal structures can provide spatially and temporally resolved data needed to validate theoretical and computational models relevant for understanding shock compression in heterogeneous materials. Two classes of 1-D photonic crystal multilayer structures were studied: optical microcavities (OMC) and distributed Bragg reflectors (DBR). These 0.5 to 5 micron thick structures were composed of SiO2, Al2O3, Ag, and PMMA layers fabricated primarily via e-beam evaporation. The multilayers have unique spectral signatures inherently linked to their time-resolved physical states. By observing shock-induced changes in these signatures, an optically-based pressure sensor was developed. Results to date indicate that both OMCs and DBRs exhibit nanosecond-resolved spectral shifts of several to 10s of nanometers under laser-driven shock compression loads of 0-10 GPa, with the magnitude of the shift strongly correlating to the shock load magnitude. Additionally, spatially and temporally resolved spectral shifts under heterogeneous laser-driven shock compression created by partial beam blocking have been successfully demonstrated. These results illustrate the potential for multilayer structures to serve as meso-scale sensors, capturing temporal and spatial pressure profile evolutions in shock-compressed heterogeneous materials, and revealing meso-scale pressure distributions across a shocked surface. Supported by DTRA Grant HDTRA1-12-1-005 and DoD, AFOSR, National Defense Science and Eng. Graduate Fellowship, 32 CFR 168a.

  20. Shock compression experiments on Lithium Deuteride (LiD) single crystals

    DOE PAGES

    Knudson, M. D.; Desjarlais, M. P.; Lemke, R. W.

    2016-12-21

    Shock compression experiments in the few hundred GPa (multi-Mabr) regime were performed on Lithium Deuteride (LiD) single crystals. This study utilized the high velocity flyer plate capability of the Sandia Z Machine to perform impact experiments at flyer plate velocities in the range of 17-32 km/s. Measurements included pressure, density, and temperature between ~200-600 GPa along the Principal Hugoniot – the locus of end states achievable through compression by large amplitude shock waves – as well as pressure and density of re - shock states up to ~900 GPa. Lastly, the experimental measurements are compared with recent density functional theorymore » calculations as well as a new tabular equation of state developed at Los Alamos National Labs.« less

  1. Effect of shock waves on the statistics and scaling in compressible isotropic turbulence

    NASA Astrophysics Data System (ADS)

    Wang, Jianchun; Wan, Minping; Chen, Song; Xie, Chenyue; Chen, Shiyi

    2018-04-01

    The statistics and scaling of compressible isotropic turbulence in the presence of large-scale shock waves are investigated by using numerical simulations at turbulent Mach number Mt ranging from 0.30 to 0.65. The spectra of the compressible velocity component, density, pressure, and temperature exhibit a k-2 scaling at different turbulent Mach numbers. The scaling exponents for structure functions of the compressible velocity component and thermodynamic variables are close to 1 at high orders n ≥3 . The probability density functions of increments of the compressible velocity component and thermodynamic variables exhibit a power-law region with the exponent -2 . Models for the conditional average of increments of the compressible velocity component and thermodynamic variables are developed based on the ideal shock relations and are verified by numerical simulations. The overall statistics of the compressible velocity component and thermodynamic variables are similar to one another at different turbulent Mach numbers. It is shown that the effect of shock waves on the compressible velocity spectrum and kinetic energy transfer is different from that of acoustic waves.

  2. Laser shock compression experiments on precompressed water in ``SG-II'' laser facility

    NASA Astrophysics Data System (ADS)

    Shu, Hua; Huang, Xiuguang; Ye, Junjian; Fu, Sizu

    2017-06-01

    Laser shock compression experiments on precompressed samples offer the possibility to obtain new hugoniot data over a significantly broader range of density-temperature phase than was previously achievable. This technique was developed in ``SG-II'' laser facility. Hugoniot data were obtained for water in 300 GPa pressure range by laser-driven shock compression of samples statically precompressed in diamond-anvil cells.

  3. Enhanced densification under shock compression in porous silicon

    NASA Astrophysics Data System (ADS)

    Lane, J. Matthew D.; Thompson, Aidan P.; Vogler, Tracy J.

    2014-10-01

    Under shock compression, most porous materials exhibit lower densities for a given pressure than that of a full-dense sample of the same material. However, some porous materials exhibit an anomalous, or enhanced, densification under shock compression. We demonstrate a molecular mechanism that drives this behavior. We also present evidence from atomistic simulation that silicon belongs to this anomalous class of materials. Atomistic simulations indicate that local shear strain in the neighborhood of collapsing pores nucleates a local solid-solid phase transformation even when bulk pressures are below the thermodynamic phase transformation pressure. This metastable, local, and partial, solid-solid phase transformation, which accounts for the enhanced densification in silicon, is driven by the local stress state near the void, not equilibrium thermodynamics. This mechanism may also explain the phenomenon in other covalently bonded materials.

  4. Transformation of shock-compressed graphite to hexagonal diamond in nanoseconds

    PubMed Central

    Turneaure, Stefan J.; Sharma, Surinder M.; Volz, Travis J.; Winey, J. M.; Gupta, Yogendra M.

    2017-01-01

    The graphite-to-diamond transformation under shock compression has been of broad scientific interest since 1961. The formation of hexagonal diamond (HD) is of particular interest because it is expected to be harder than cubic diamond and due to its use in terrestrial sciences as a marker at meteorite impact sites. However, the formation of diamond having a fully hexagonal structure continues to be questioned and remains unresolved. Using real-time (nanosecond), in situ x-ray diffraction measurements, we show unequivocally that highly oriented pyrolytic graphite, shock-compressed along the c axis to 50 GPa, transforms to highly oriented elastically strained HD with the (100)HD plane parallel to the graphite basal plane. These findings contradict recent molecular dynamics simulation results for the shock-induced graphite-to-diamond transformation and provide a benchmark for future theoretical simulations. Additionally, our results show that an earlier report of HD forming only above 170 GPa for shocked pyrolytic graphite may lead to incorrect interpretations of meteorite impact events. PMID:29098183

  5. Single-shot Ellipsometry of Shocked Iron to 275 GPa

    NASA Astrophysics Data System (ADS)

    Grant, Sean; Ao, Tommy; Bernstein, Aaron; Davis, Jean-Paul; Ditmire, Todd; Dolan, Daniel; Lin, Jung-Fu; Porwitzky, Andrew; Seagle, Christopher

    2017-06-01

    We have studied the properties of iron under shock conditions using time-resolved ellipsometry, a technique that probes the dielectric value of materials under dynamic conditions, on the STAR gas gun facility at Sandia National Laboratories. We performed experiments on a two-stage gas gun ranging from the α - ɛ transition (75 GPa) to the solid-liquid transition (275 GPa). For the first time, we report the dielectric results of shocked iron at those conditions. In addition, the time-resolved ellipsometry diagnostic is being implemented on the Sandia pulsed power Z-machine. The goal of upcoming Z experiments will be to employ the ``shock-ramp'' technique to reach pressure and temperature conditions relevant to the Earth core, and to use ellipsometry to obtain the iron electric conductivities needed for benchmarking material models. Sandia National Laboratories is a multi-mission laboratory managed and operated by Sandia Corporation, a wholly owned subsidiary of Lockheed Martin Corporation, for the U.S. Department of Energy's National Nuclear Security Administration under contract DE-AC04-94AL85000. SAND2017-1952 A.

  6. Experimental evidence for superionic water ice using shock compression

    NASA Astrophysics Data System (ADS)

    Millot, Marius; Hamel, Sebastien; Rygg, J. Ryan; Celliers, Peter M.; Collins, Gilbert W.; Coppari, Federica; Fratanduono, Dayne E.; Jeanloz, Raymond; Swift, Damian C.; Eggert, Jon H.

    2018-03-01

    In stark contrast to common ice, Ih, water ice at planetary interior conditions has been predicted to become superionic with fast-diffusing (that is, liquid-like) hydrogen ions moving within a solid lattice of oxygen. Likely to constitute a large fraction of icy giant planets, this extraordinary phase has not been observed in the laboratory. Here, we report laser-driven shock-compression experiments on water ice VII. Using time-resolved optical pyrometry and laser velocimetry measurements as well as supporting density functional theory-molecular dynamics (DFT-MD) simulations, we document the shock equation of state of H2O to unprecedented extreme conditions and unravel thermodynamic signatures showing that ice melts near 5,000 K at 190 GPa. Optical reflectivity and absorption measurements also demonstrate the low electronic conductivity of ice, which, combined with previous measurements of the total electrical conductivity under reverberating shock compression, provides experimental evidence for superionic conduction in water ice at planetary interior conditions, verifying a 30-year-old prediction.

  7. First-principles calculation of the reflectance of shock-compressed xenon

    DOE Office of Scientific and Technical Information (OSTI.GOV)

    Norman, G. E.; Saitov, I. M., E-mail: saitovilnur@gmail.com; Stegailov, V. V.

    2015-05-15

    Within electron density functional theory (DFT), the reflectance of radiation from shock-compressed xenon plasma is calculated. The dependence of the reflectance on the frequency of the incident radiation and on the plasma density is considered. The Fresnel formula is used. The expression for the longitudinal dielectric tensor in the long-wavelength limit is used to calculate the imaginary part of the dielectric function (DF). The real part of the DF is determined by the Kramers-Kronig transformation. The results are compared with experimental data. An approach is proposed to estimate the plasma frequency in shock-compressed xenon.

  8. Ultra high-speed x-ray imaging of laser-driven shock compression using synchrotron light

    NASA Astrophysics Data System (ADS)

    Olbinado, Margie P.; Cantelli, Valentina; Mathon, Olivier; Pascarelli, Sakura; Grenzer, Joerg; Pelka, Alexander; Roedel, Melanie; Prencipe, Irene; Laso Garcia, Alejandro; Helbig, Uwe; Kraus, Dominik; Schramm, Ulrich; Cowan, Tom; Scheel, Mario; Pradel, Pierre; De Resseguier, Thibaut; Rack, Alexander

    2018-02-01

    A high-power, nanosecond pulsed laser impacting the surface of a material can generate an ablation plasma that drives a shock wave into it; while in situ x-ray imaging can provide a time-resolved probe of the shock-induced material behaviour on macroscopic length scales. Here, we report on an investigation into laser-driven shock compression of a polyurethane foam and a graphite rod by means of single-pulse synchrotron x-ray phase-contrast imaging with MHz frame rate. A 6 J, 10 ns pulsed laser was used to generate shock compression. Physical processes governing the laser-induced dynamic response such as elastic compression, compaction, pore collapse, fracture, and fragmentation have been imaged; and the advantage of exploiting the partial spatial coherence of a synchrotron source for studying low-density, carbon-based materials is emphasized. The successful combination of a high-energy laser and ultra high-speed x-ray imaging using synchrotron light demonstrates the potentiality of accessing complementary information from scientific studies of laser-driven shock compression.

  9. Shock-Wave Pulse Compression and Stretching of Dodecane and Mineral Oils

    NASA Astrophysics Data System (ADS)

    Bannikova, I. A.; Zubareva, A. N.; Utkin, A. V.

    2018-04-01

    The behavior of dodecane, vacuum, and transformer oils under shock-wave pulse compression and stretching are studied experimentally. The wave profiles are registered using a VISAR laser interferometer. The shock adiabats, the dependence of the sound velocity on the pressure, and the maximum negative pressures developed in the studied liquids are determined. It is shown that the negative pressure value does not depend on the deformation rate in the case of oils and is a strong function of the compression pulse amplitude in the case of dodecane.

  10. High-energy synchrotron X-ray radiography of shock-compressed materials

    NASA Astrophysics Data System (ADS)

    Rutherford, Michael E.; Chapman, David J.; Collinson, Mark A.; Jones, David R.; Music, Jasmina; Stafford, Samuel J. P.; Tear, Gareth R.; White, Thomas G.; Winters, John B. R.; Drakopoulos, Michael; Eakins, Daniel E.

    2015-06-01

    This presentation will discuss the development and application of a high-energy (50 to 250 keV) synchrotron X-ray imaging method to study shock-compressed, high-Z samples at Beamline I12 at the Diamond Light Source synchrotron (Rutherford-Appleton Laboratory, UK). Shock waves are driven into materials using a portable, single-stage gas gun designed by the Institute of Shock Physics. Following plate impact, material deformation is probed in-situ by white-beam X-ray radiography and complimentary velocimetry diagnostics. The high energies, large beam size (13 x 13 mm), and appreciable sample volumes (~ 1 cm3) viable for study at Beamline I12 compliment existing in-house pulsed X-ray capabilities and studies at the Dynamic Compression Sector. The authors gratefully acknowledge the ongoing support of Imperial College London, EPSRC, STFC and the Diamond Light Source, and AWE Plc.

  11. Molecular dynamics simulation of the plastic behavior anisotropy of shock-compressed monocrystal nickel

    NASA Astrophysics Data System (ADS)

    Chen, Ya-Zhou; Zhou, Liu-Cheng; He, Wei-Feng; Sun, Yu; Li, Ying-Hong; Jiao, Yang; Luo, Si-Hai

    2017-01-01

    Molecular dynamics simulations were used to study the plastic behavior of monocrystalline nickel under shock compression along the [100] and [110] orientations. The shock Hugoniot relation, local stress curve, and process of microstructure development were determined. Results showed the apparent anisotropic behavior of monocrystalline nickel under shock compression. The separation of elastic and plastic waves was also obvious. Plastic deformation was more severely altered along the [110] direction than the [100] direction. The main microstructure phase transformed from face-centered cubic to body-centered cubic and generated a large-scale and low-density stacking fault along the family of { 111 } crystal planes under shock compression along the [100] direction. By contrast, the main mechanism of plastic deformation in the [110] direction was the nucleation of the hexagonal, close-packed phase, which generated a high density of stacking faults along the [110] and [1̅10] directions.

  12. Development of a broadband reflectivity diagnostic for laser driven shock compression experiments

    DOE PAGES

    Ali, S. J.; Bolme, C. A.; Collins, G. W.; ...

    2015-04-16

    Here, a normal-incidence visible and near-infrared shock wave optical reflectivity diagnostic was constructed to investigate changes in the optical properties of materials under dynamic laser compression. Documenting wavelength- and time-dependent changes in the optical properties of laser-shock compressed samples has been difficult, primarily due to the small sample sizes and short time scales involved, but we succeeded in doing so by broadening a series of time delayed 800-nm pulses from an ultrafast Ti:sapphire laser to generate high-intensity broadband light at nanosecond time scales. This diagnostic was demonstrated over the wavelength range 450–1150 nm with up to 16 time displaced spectramore » during a single shock experiment. Simultaneous off-normal incidence velocity interferometry (velocity interferometer system for any reflector) characterized the sample under laser-compression and also provided an independent reflectivity measurement at 532 nm wavelength. The shock-driven semiconductor-to-metallic transition in germanium was documented by the way of reflectivity measurements with 0.5 ns time resolution and a wavelength resolution of 10 nm.« less

  13. Transformation of shock-compressed graphite to hexagonal diamond in nanoseconds

    DOE Office of Scientific and Technical Information (OSTI.GOV)

    Turneaure, Stefan J.; Sharma, Surinder M.; Volz, Travis J.

    The graphite-to-diamond transformation under shock compression has been of broad scientific interest since 1961. The formation of hexagonal diamond (HD) is of particular interest because it is expected to be harder than cubic diamond and due to its use in terrestrial sciences as a marker at meteorite impact sites. However, the formation of diamond having a fully hexagonal structure continues to be questioned and remains unresolved. Using real-time (nanosecond), in situ x-ray diffraction measurements, we show unequivocally that highly oriented pyrolytic graphite, shock-compressed along the c axis to 50 GPa, transforms to highly oriented elastically strained HD with the (100)HDmore » plane parallel to the graphite basal plane. These findings contradict recent molecular dynamics simulation results for the shock-induced graphite-to-diamond transformation and provide a benchmark for future theoretical simulations. Additionally, our results show that an earlier report of HD forming only above 170 GPa for shocked pyrolytic graphite may lead to incorrect interpretations of meteorite impact events.« less

  14. Transformation of shock-compressed graphite to hexagonal diamond in nanoseconds

    DOE PAGES

    Turneaure, Stefan J.; Sharma, Surinder M.; Volz, Travis J.; ...

    2017-10-27

    The graphite-to-diamond transformation under shock compression has been of broad scientific interest since 1961. The formation of hexagonal diamond (HD) is of particular interest because it is expected to be harder than cubic diamond and due to its use in terrestrial sciences as a marker at meteorite impact sites. However, the formation of diamond having a fully hexagonal structure continues to be questioned and remains unresolved. Using real-time (nanosecond), in situ x-ray diffraction measurements, we show unequivocally that highly oriented pyrolytic graphite, shock-compressed along the c axis to 50 GPa, transforms to highly oriented elastically strained HD with the (100)HDmore » plane parallel to the graphite basal plane. These findings contradict recent molecular dynamics simulation results for the shock-induced graphite-to-diamond transformation and provide a benchmark for future theoretical simulations. Additionally, our results show that an earlier report of HD forming only above 170 GPa for shocked pyrolytic graphite may lead to incorrect interpretations of meteorite impact events.« less

  15. The effect of shock dynamics on compressibility of ignition-scale National Ignition Facility implosions

    DOE Office of Scientific and Technical Information (OSTI.GOV)

    Zylstra, A. B.; Frenje, J. A.; Séguin, F. H.

    The effects of shock dynamics on compressibility of indirect-drive ignition-scale surrogate implosions, CH shells filled with D 3He gas, have been studied using charged-particle spectroscopy. Spectral measurements of D 3He protons produced at the shock-bang time probe the shock dynamics and in-flight characteristics of an implosion. The proton shock yield is found to vary by over an order of magnitude. A simple model relates the observed yield to incipient hot-spot adiabat, suggesting that implosions with rapid radiation-power increase during the main drive pulse may have a 2x higher hot-spot adiabat, potentially reducing compressibility. A self-consistent 1-D implosion model was usedmore » to infer the areal density (pR) and the shell center-of-mass radius (R cm) from the downshift of the shock-produced D 3He protons. The observed pR at shock-bang time is substantially higher for implosions, where the laser drive is on until near the compression bang time ('short-coast'), while longer-coasting implosions have lower pR. This corresponds to a much larger temporal difference between the shock- and compression-bang time in the long-coast implosions (~800 ps) than in the short-coast (~400 ps); this will be verified with a future direct bang-time diagnostic. This model-inferred differential bang time contradicts radiation-hydrodynamic simulations, which predict constant 700–800 ps differential independent of coasting time. This result is potentially explained by uncertainties in modeling late-time ablation drive on the capsule. In an ignition experiment, an earlier shock-bang time resulting in an earlier onset of shell deceleration, potentially reducing compression and, thus, fuel pR.« less

  16. The effect of shock dynamics on compressibility of ignition-scale National Ignition Facility implosions

    DOE PAGES

    Zylstra, A. B.; Frenje, J. A.; Séguin, F. H.; ...

    2014-11-03

    The effects of shock dynamics on compressibility of indirect-drive ignition-scale surrogate implosions, CH shells filled with D 3He gas, have been studied using charged-particle spectroscopy. Spectral measurements of D 3He protons produced at the shock-bang time probe the shock dynamics and in-flight characteristics of an implosion. The proton shock yield is found to vary by over an order of magnitude. A simple model relates the observed yield to incipient hot-spot adiabat, suggesting that implosions with rapid radiation-power increase during the main drive pulse may have a 2x higher hot-spot adiabat, potentially reducing compressibility. A self-consistent 1-D implosion model was usedmore » to infer the areal density (pR) and the shell center-of-mass radius (R cm) from the downshift of the shock-produced D 3He protons. The observed pR at shock-bang time is substantially higher for implosions, where the laser drive is on until near the compression bang time ('short-coast'), while longer-coasting implosions have lower pR. This corresponds to a much larger temporal difference between the shock- and compression-bang time in the long-coast implosions (~800 ps) than in the short-coast (~400 ps); this will be verified with a future direct bang-time diagnostic. This model-inferred differential bang time contradicts radiation-hydrodynamic simulations, which predict constant 700–800 ps differential independent of coasting time. This result is potentially explained by uncertainties in modeling late-time ablation drive on the capsule. In an ignition experiment, an earlier shock-bang time resulting in an earlier onset of shell deceleration, potentially reducing compression and, thus, fuel pR.« less

  17. Laser-driven shock compression of gold foam in the terapascal pressure range

    NASA Astrophysics Data System (ADS)

    Liu, Wei; Duan, Xiaoxi; Jiang, Shaoen; Wang, Zhebin; Sun, Liang; Liu, Hao; Yang, Weiming; Zhang, Huan; Ye, Qing; Wang, Peng; Li, Yulong; Yi, Lin; Dong, Suo

    2018-06-01

    Shock compression experiments are carried out on gold foam with an initial density of 3.2 g/cm3 through indirectly laser-driven shock waves at the SG-III prototype laser facility. The impedance-matching technique is applied to determine the equation-of-state (EOS) data of the shocked gold foam. A passive shock breakout diagnostic system is employed to obtain the shock velocities in both the standard material and gold foam. The gold foams are compressed to a maximum density of 20 g/cm3 under a shock pressure of about 2 TPa. The effects of the unsteadiness of shock waves on the EOS measurement are quantitatively analyzed and corrected. The correction of unsteady waves, as well as the good planarity of the shock waves and the low preheating of the gold foam, contributes high-confidence EOS data for the gold foam. The corrected experimental data are compared with the Hugoniot states from the SESAME library. The comparison suggests that the database is suitable for describing the states of gold foam with an initial density of 3.2 g/cm3 under a pressure of about 2 TPa.

  18. Method and apparatus for determining pressure-induced frequency-shifts in shock-compressed materials

    DOEpatents

    Moore, David S.; Schmidt, Stephen C.

    1985-01-01

    A method and an apparatus for conducting coherent anti-Stokes Raman scattering spectroscopy in shock-compressed materials are disclosed. The apparatus includes a sample vessel having an optically transparent wall and an opposing optically reflective wall. Two coherent laser beams, a pump beam and a broadband Stokes beam, are directed through the window and focused on a portion of the sample. In the preferred embodiment, a projectile is fired from a high-pressure gas gun to impact the outside of the reflective wall, generating a planar shock wave which travels through the sample toward the window. The pump and Stokes beams result in the emission from the shock-compressed sample of a coherent anti-Stokes beam, which is emitted toward the approaching reflective wall of the vessel and reflected back through the window. The anti-Stokes beam is folded into a spectrometer for frequency analysis. The results of such analysis are useful for determining chemical and physical phenomena which occur during the shock-compression of the sample.

  19. Ultrafast visualization of crystallization and grain growth in shock-compressed SiO2

    PubMed Central

    Gleason, A. E.; Bolme, C. A.; Lee, H. J.; Nagler, B.; Galtier, E.; Milathianaki, D.; Hawreliak, J.; Kraus, R. G.; Eggert, J. H.; Fratanduono, D. E.; Collins, G. W.; Sandberg, R.; Yang, W.; Mao, W. L.

    2015-01-01

    Pressure- and temperature-induced phase transitions have been studied for more than a century but very little is known about the non-equilibrium processes by which the atoms rearrange. Shock compression generates a nearly instantaneous propagating high-pressure/temperature condition while in situ X-ray diffraction (XRD) probes the time-dependent atomic arrangement. Here we present in situ pump–probe XRD measurements on shock-compressed fused silica, revealing an amorphous to crystalline high-pressure stishovite phase transition. Using the size broadening of the diffraction peaks, the growth of nanocrystalline stishovite grains is resolved on the nanosecond timescale just after shock compression. At applied pressures above 18 GPa the nuclueation of stishovite appears to be kinetically limited to 1.4±0.4 ns. The functional form of this grain growth suggests homogeneous nucleation and attachment as the growth mechanism. These are the first observations of crystalline grain growth in the shock front between low- and high-pressure states via XRD. PMID:26337754

  20. Method and apparatus for determining pressure-induced frequency-shifts in shock-compressed materials

    DOEpatents

    Moore, D.S.; Schmidt, S.C.

    1983-12-16

    A method and an apparatus for conducting coherent anti-Stokes Raman scattering spectroscopy in shock-compressed materials are disclosed. The apparatus includes a sample vessel having an optically transparent wall and an opposing optically reflective wall. Two coherent laser beams, a pump beam and a broadband Stokes beam, are directed through the window and focused on a portion of the sample. In the preferred embodiment, a projectile is fired from a high-pressure gas gun to impact the outside of the reflective wall, generating a planar shock wave which travels through the sample toward the window. The pump and Stokes beams result in the emission from the shock-compressed sample of a coherent anti-Stokes beam, which is emitted toward the approaching reflective wall of the vessel and reflected back through the window. The anti-Stokes beam is folded into a spectrometer for frequency analysis. The results of such analysis are useful for determining chemical and physical phenomena which occur during the shock-compression of the sample.

  1. In situ observation of stishovite formation in shock-compressed fused silica

    NASA Astrophysics Data System (ADS)

    Tracy, Sally June; Turneaure, Stefan; Duffy, Thomas

    2017-06-01

    Silica, SiO2, has widespread applications ranging from optical components to refractory materials and is of geological importance as one of the major oxide components of the Earth's crust and mantle. The response of silica phases to dynamic loading has long been of interest for understanding the structural evolution of this fundamental oxide. Under shock compression both crystalline quartz and fused silica are characterized by the occurrence of a broad `mixed-phase region' (15-40 GPa) and a dense, high-pressure phase with much lower compressibility. Despite decades of study, the nature of this transformation and the identity of the high-pressure phase(s) remain poorly understood. In situ x-ray diffraction experiments on shock-compressed fused silica were conducted at the Dynamic Compression Sector of the Advanced Photon Source. The lattice-level structure was investigated through time-resolved x-ray diffraction measurements on samples reaching peak stress ranging from 12 to 47 GPa. Our results demonstrate that SiO2 adopts a dense amorphous structure in the `mixed-phase region' and abruptly transforms to stishovite above 34 GPa. These results provide clear evidence that high-pressure crystalline silicate phases can form from amorphous starting materials on the time-scale of laboratory shock experiments.

  2. Shock Compression Induced Hot Spots in Energetic Material Detected by Thermal Imaging Microscopy

    NASA Astrophysics Data System (ADS)

    Chen, Ming-Wei; Dlott, Dana

    2014-06-01

    The chemical reaction of powder energetic material is of great interest in energy and pyrotechnic applications since the high reaction temperature. Under the shock compression, the chemical reaction appears in the sub-microsecond to microsecond time scale, and releases a large amount of energy. Experimental and theoretical research progresses have been made in the past decade, in order to characterize the process under the shock compression. However, the knowledge of energy release and temperature change of this procedure is still limited, due to the difficulties of detecting technologies. We have constructed a thermal imaging microscopy apparatus, and studied the temperature change in energetic materials under the long-wavelength infrared (LWIR) and ultrasound exposure. Additionally, the real-time detection of the localized heating and energy concentration in composite material is capable with our thermal imaging microscopy apparatus. Recently, this apparatus is combined with our laser driven flyer plate system to provide a lab-scale source of shock compression to energetic material. A fast temperature increase of thermite particulars induced by the shock compression is directly observed by thermal imaging with 15-20 μm spatial resolution. Temperature change during the shock loading is evaluated to be at the order of 10^9K/s, through the direct measurement of mid-wavelength infrared (MWIR) emission intensity change. We observe preliminary results to confirm the hot spots appear with shock compression on energetic crystals, and will discuss the data and analysis in further detail. M.-W. Chen, S. You, K. S. Suslick, and D. D. Dlott, {Rev. Sci. Instr., 85, 023705 (2014) M.-W. Chen, S. You, K. S. Suslick, and D. D. Dlott, {Appl. Phys. Lett., 104, 061907 (2014)} K. E. Brown, W. L. Shaw, X. Zheng, and D. D. Dlott, {Rev. Sci. Instr., 83, 103901 (2012)}

  3. Using phase contrast imaging to measure the properties of shock compressed aerogel

    NASA Astrophysics Data System (ADS)

    Hawreliak, James; Erskine, Dave; Schropp, Andres; Galtier, Eric C.; Heimann, Phil

    2017-01-01

    The Hugoniot states of low density materials, such as silica aerogel, are used in high energy density physics research because they can achieve a range of high temperature and pressure states through shock compression. The shock properties of 100mg/cc silica aerogel were studied at the Materials in Extreme Conditions end station using x-ray phase contrast imaging of spherically expanding shock waves. The shockwaves were generated by focusing a high power 532nm laser to a 50μm focal spot on a thin aluminum ablator. The shock speed was measured in separate experiments using line-VISAR measurements from the reflecting shock front. The relative timing between the x-ray probe and the optical laser pump was varied so x-ray PCI images were taken at pressures between 10GPa and 30GPa. Modeling the compression of the foam in the strong shock limit uses a Gruneisen parameter of 0.49 to fit the data rather than a value of 0.66 that would correspond to a plasma state.

  4. Enhanced densification under shock compression in porous silicon

    DOE PAGES

    Lane, J. Matthew; Thompson, Aidan Patrick; Vogler, Tracy

    2014-10-27

    Under shock compression, most porous materials exhibit lower densities for a given pressure than that of a full-dense sample of the same material. However, some porous materials exhibit an anomalous, or enhanced, densification under shock compression. The mechanism driving this behavior was not completely determined. We present evidence from atomistic simulation that pure silicon belongs to this anomalous class of materials and demonstrate the associated mechanisms responsible for the effect in porous silicon. Atomistic response indicates that local shear strain in the neighborhood of collapsing pores catalyzes a local solid-solid phase transformation even when bulk pressures are below the thermodynamicmore » phase transformation pressure. This metastable, local, and partial, solid-solid phase transformation, which accounts for the enhanced densification in silicon, is driven by the local stress state near the void, not equilibrium thermodynamics. This mechanism may also explain the phenomenon in other covalently bonded materials.« less

  5. The History of the APS Topical Group on Shock Compression of Condensed Matter

    NASA Astrophysics Data System (ADS)

    Forbes, Jerry W.

    2002-07-01

    In order to provide broader scientific recognition and to advance the science of shock compressed condensed matter, a group of American Physical Society (APS) members worked within the Society to make this field an active part of the APS. Individual papers were presented at APS meetings starting in the 1940's and shock wave sessions were organized starting with the 1967 Pasadena meeting. Shock wave topical conferences began in 1979 in Pullman, WA. Signatures were obtained on a petition in 1984 from a balanced cross-section of the shock wave community to form an APS Topical Group (TG). The APS Council officially accepted the formation of the Shock Compression of Condensed Matter (SCCM) TG at its October 1984 meeting. This action firmly aligned the shock wave field with a major physical science organization. Most early topical conferences were sanctioned by the APS while those held after 1992 were official APS meetings. The topical group organizes a shock wave topical conference in odd numbered years while participating in shock wave/high pressure sessions at APS general meetings in even numbered years.

  6. Transformation of shock-compressed graphite to hexagonal diamond in nanoseconds

    DOE Office of Scientific and Technical Information (OSTI.GOV)

    Turneaure, Stefan J.; Sharma, Surinder M.; Volz, Travis J.

    2017-10-01

    The graphite-to-diamond transformation under shock compression has been of broad scientific interest since 1961. The formation of hexagonal diamond (HD) is of particular interest because it is expected to be harder than cubic diamond and due to its use in terrestrial sciences as a marker at meteorite impact sites. However, the formation of diamond having a fully hexagonal structure continues to be questioned and remains unresolved. Using real-time (nanosecond), in situ x-ray diffraction measurements, we show unequivocally that highly oriented pyrolytic graphite, shock-compressed along the c axis to 50 GPa, transforms to highly oriented elastically strained HD with the (100)HDmore » plane parallel to the graphite basal plane.« less

  7. Microstructural fingerprints of phase transitions in shock-loaded iron

    NASA Astrophysics Data System (ADS)

    Wang, S. J.; Sui, M. L.; Chen, Y. T.; Lu, Q. H.; Ma, E.; Pei, X. Y.; Li, Q. Z.; Hu, H. B.

    2013-01-01

    The complex structural transformation in crystals under static pressure or shock loading has been a subject of long-standing interest to materials scientists and physicists. The polymorphic transformation is of particular importance for iron (Fe), due to its technological and sociological significance in the development of human civilization, as well as its prominent presence in the earth's core. The martensitic transformation α-->ɛ (bcc-->hcp) in iron under shock-loading, due to its reversible and transient nature, requires non-trivial detective work to uncover its occurrence. Here we reveal refined microstructural fingerprints, needle-like colonies and three sets of {112}<111> twins with a threefold symmetry, with tell-tale features that are indicative of two sequential martensitic transformations in the reversible α-->ɛ phase transition, even though no ɛ is retained in the post-shock samples. The signature orientation relationships are consistent with previously-proposed transformation mechanisms, and the unique microstructural fingerprints enable a quantitative assessment of the volume fraction transformed.

  8. Ultrafast visualization of crystallization and grain growth in shock-compressed SiO 2

    DOE PAGES

    Gleason, A. E.; Bolme, C. A.; Lee, H. J.; ...

    2015-09-04

    Pressure- and temperature-induced phase transitions have been studied for more than a century but very little is known about the non-equilibrium processes by which the atoms rearrange. Shock compression generates a nearly instantaneous propagating high-pressure/temperature condition while in situ X-ray diffraction (XRD) probes the time-dependent atomic arrangement. Here we present in situ pump–probe XRD measurements on shock-compressed fused silica, revealing an amorphous to crystalline high-pressure stishovite phase transition. Using the size broadening of the diffraction peaks, the growth of nanocrystalline stishovite grains is resolved on the nanosecond timescale just after shock compression. At applied pressures above 18 GPa the nuclueationmore » of stishovite appears to be kinetically limited to 1.4 ± 0.4 ns. The functional form of this grain growth suggests homogeneous nucleation and attachment as the growth mechanism. As a result, these are the first observations of crystalline grain growth in the shock front between low- and high-pressure states via XRD.« less

  9. Laser-shock damage of iron-based materials

    NASA Astrophysics Data System (ADS)

    Chu, Jinn P.; Banas, Grzegorz; Lawrence, Frederick V.; Rigsbee, James M.; Elsayed-Ali, Hani E.

    1993-05-01

    The effects of laser shock processing on the microstructure and mechanical properties of the manganese (1 percent C and 14 percent Mn) steels have been low carbon (0.04 wt. percent C) and Hadfield studied. Laser shock processing was performed with a 1.054 micrometers wavelength Nd-phosphate laser operating in a pulse mode (600 ps pulse length and up to 200 J energy) with power densities above 10 to the 11th power W/cm2. Shock waves were generated by volume expansion of the plasma formed when the material was laser irradiated. Maximum shock wave intensities were obtained using an energy-absorbing black paint coating without a plasma-confining overlay. Maximum modification of compressive residual stresses were achieved when laser shock processing induced deformation occurred without melting. Mechanical properties were improved through modifying the microstructure by laser shock processing. High density arrays of dislocations (greater than 10 to the 11th power/cm2) were generated in low carbon steel by high strain-rate deformation of laser shock processing, resulting in surface hardness increases of 30 to 80 percent. In austenitic Hadfield steel, laser shock processing caused extensive formation of Epsilon-hcp martensite (35 vol. percent), producing increases of 50 to 130 percent in surface hardness. The laser shock processing strengthening effect in Hadfield steel was attributed to the combined effects of the partial dislocation/stacking fault arrays and the grain refinement due to presence of the Epsilon-hcp martensite.

  10. The size effects upon shock plastic compression of nanocrystals

    NASA Astrophysics Data System (ADS)

    Malygin, G. A.; Klyavin, O. V.

    2017-10-01

    For the first time a theoretical analysis of scale effects upon the shock plastic compression of nanocrystals is implemented in the context of a dislocation kinetic approach based on the equations and relationships of dislocation kinetics. The yield point of crystals τy is established as a quantitative function of their cross-section size D and the rate of shock deformation as τy ɛ2/3 D. This dependence is valid in the case of elastic stress relaxation on account of emission of dislocations from single-pole Frank-Read sources near the crystal surface.

  11. Thermal history of shock-compressed solids

    NASA Technical Reports Server (NTRS)

    Svendsen, B.; Ahrens, T. J.

    1985-01-01

    An isotropic, heterogeneous, viscous thermoplastic model of the uniaxially shock-compressed state in transparent solids is examined with a view to determining the conditions under which this radiation may be nominally thermal or nonthermal. Regions of locally high temperatures producing thermal radiation may develop only where the local viscosity is low and the Maxwell time is short; alternatively, regions of low elastic moduli and long Maxwell time could experience sustained elastic deformation, leading to microfracture and triboluminescence. Attention is given to the cases of MgO and SiO2.

  12. Shock Compression of Liquid Noble Gases to Multi-Mbar Pressures

    NASA Astrophysics Data System (ADS)

    Root, Seth

    2011-10-01

    The high pressure - high temperature behavior of noble gases is of considerable interest because of their use in z-pinch liners for fusion studies and for understanding astrophysical and planetary evolution. However, our understanding of the equation of state (EOS) of the noble gases at extreme conditions is limited. A prime example of this is the liquid xenon Hugoniot. Previous EOS models rapidly diverged on the Hugoniot above 1 Mbar because of differences in the treatment of the electronic contribution to the free energy. Similar divergences are observed for krypton EOS. Combining shock compression experiments and density functional theory (DFT) simulations, we can determine the thermo-physical behavior of matter under extreme conditions. The experimental and DFT results have been instrumental to recent developments in planetary astrophysics and inertial confinement fusion. Shock compression experiments are performed using Sandia's Z-Accelerator to determine the Hugoniot of liquid xenon and krypton in the Mbar regime. Under strong pressure, krypton and xenon undergo an insulator to metal transition. In the metallic state, the shock front becomes reflective allowing for a direct measurement of the sample's shock velocity using laser interferometry. The Hugoniot state is determined using a Monte Carlo analysis method that accounts for systematic error in the standards and for correlations. DFT simulations at these extreme conditions show good agreement with the experimental data - demonstrating the attention to detail required for dealing with elements with relativistic core states and d-state electrons. The results from shock compression experiments and DFT simulations are presented for liquid xenon to 840 GPa and for liquid krypton to 800 GPa, decidedly increasing the range of known behavior of both gases. Sandia National Laboratories is a multi-program laboratory managed and operated by Sandia Corporation, a wholly owned subsidiary of Lockheed Martin Company

  13. Shock compression and flash-heating of molecular adsorbates on the picosecond time scale

    NASA Astrophysics Data System (ADS)

    Berg, Christopher Michael

    An ultrafast nonlinear coherent laser spectroscopy termed broadband multiplex vibrational sum-frequency generation (SFG) with nonresonant suppression was employed to monitor vibrational transitions of molecular adsorbates on metallic substrates during laser-driven shock compression and flash-heating. Adsorbates were in the form of well-ordered self-assembled monolayers (SAMs) and included molecular explosive simulants, such as nitroaromatics, and long chain-length alkanethiols. Based on reflectance measurements of the metallic substrates, femtosecond flash-heating pulses were capable of producing large-amplitude temperature jumps with DeltaT = 500 K. Laser-driven shock compression of SAMs produced pressures up to 2 GPa, where 1 GPa ≈ 1 x 104 atm. Shock pressures were estimated via comparison with frequency shifts observed in the monolayer vibrational transitions during hydrostatic pressure measurements in a SiC anvil cell. Molecular dynamics during flash-heating and shock loading were probed with vibrational SFG spectroscopy with picosecond temporal resolution and sub-nanometer spatial resolution. Flash-heating studies of 4-nitrobenzenethiolate (NBT) on Au provided insight into effects from hot-electron excitation of the molecular adsorbates at early pump-probe delay times. At longer delay times, effects from the excitation of SAM lattice modes and lower-energy NBT vibrations were shown. In addition, flash-heating studies of alkanethiolates demonstrated chain disordering behaviors as well as interface thermal conductances across the Au-SAM junction, which was of specific interest within the context of molecular electronics. Shock compression studies of molecular explosive simulants, such as 4-nitrobenzoate (NBA), demonstrated the proficiency of this technique to observe shock-induced molecular dynamics, in this case orientational dynamics, on the picosecond time scale. Results validated the utilization of these refined shock loading techniques to probe the shock

  14. Structural changes in shock compressed silicon observed using time-resolved x-ray diffraction at the Dynamic Compression Sector

    NASA Astrophysics Data System (ADS)

    Turneaure, Stefan; Zdanowicz, E.; Sinclair, N.; Graber, T.; Gupta, Y. M.

    2015-06-01

    Structural changes in shock compressed silicon were observed directly using time-resolved x-ray diffraction (XRD) measurements at the Dynamic Compression Sector at the Advanced Photon Source. The silicon samples were impacted by polycarbonate impactors accelerated to velocities greater than 5 km/s using a two-stage light gas gun resulting in impact stresses of about 25 GPa. The 23.5 keV synchrotron x-ray beam passed through the polycarbonate impactor, the silicon sample, and an x-ray window (polycarbonate or LiF) at an angle of 30 degrees relative to the impact plane. Four XRD frames (~ 100 ps snapshots) were obtained with 153.4 ns between frames near the time of impact. The XRD measurements indicate that in the peak shocked state, the silicon samples completely transformed to a high-pressure phase. XRD results for both shocked polycrystalline silicon and single crystal silicon will be presented and compared. Work supported by DOE/NNSA.

  15. Directional amorphization of boron carbide subjected to laser shock compression

    PubMed Central

    Zhao, Shiteng; Kad, Bimal; Remington, Bruce A.; LaSalvia, Jerry C.; Wehrenberg, Christopher E.; Behler, Kristopher D.; Meyers, Marc A.

    2016-01-01

    Solid-state shock-wave propagation is strongly nonequilibrium in nature and hence rate dependent. Using high-power pulsed-laser-driven shock compression, unprecedented high strain rates can be achieved; here we report the directional amorphization in boron carbide polycrystals. At a shock pressure of 45∼50 GPa, multiple planar faults, slightly deviated from maximum shear direction, occur a few hundred nanometers below the shock surface. High-resolution transmission electron microscopy reveals that these planar faults are precursors of directional amorphization. It is proposed that the shear stresses cause the amorphization and that pressure assists the process by ensuring the integrity of the specimen. Thermal energy conversion calculations including heat transfer suggest that amorphization is a solid-state process. Such a phenomenon has significant effect on the ballistic performance of B4C. PMID:27733513

  16. Directional amorphization of boron carbide subjected to laser shock compression.

    PubMed

    Zhao, Shiteng; Kad, Bimal; Remington, Bruce A; LaSalvia, Jerry C; Wehrenberg, Christopher E; Behler, Kristopher D; Meyers, Marc A

    2016-10-25

    Solid-state shock-wave propagation is strongly nonequilibrium in nature and hence rate dependent. Using high-power pulsed-laser-driven shock compression, unprecedented high strain rates can be achieved; here we report the directional amorphization in boron carbide polycrystals. At a shock pressure of 45∼50 GPa, multiple planar faults, slightly deviated from maximum shear direction, occur a few hundred nanometers below the shock surface. High-resolution transmission electron microscopy reveals that these planar faults are precursors of directional amorphization. It is proposed that the shear stresses cause the amorphization and that pressure assists the process by ensuring the integrity of the specimen. Thermal energy conversion calculations including heat transfer suggest that amorphization is a solid-state process. Such a phenomenon has significant effect on the ballistic performance of B 4 C.

  17. Strength properties and structure of a submicrocrystalline Al-Mg-Mn alloy under shock compression

    NASA Astrophysics Data System (ADS)

    Petrova, A. N.; Brodova, I. G.; Razorenov, S. V.

    2017-06-01

    The results of studying the strength of a submicrocrystalline aluminum A5083 alloy (chemical composition was 4.4Mg-0.6Mn-0.11Si-0.23Fe-0.03Cr-0.02Cu-0.06Ti wt % and Al base) under shockwave compression are presented. The submicrocrystalline structure of the alloy was produced in the process of dynamic channel-angular pressing at a strain rate of 104 s-1. The average size of crystallites in the alloy was 180-460 nm. Hugoniot elastic limit σHEL, dynamic yield stress σy, and the spall strength σSP of the submicrocrystalline alloy were determined based on the free-surface velocity profiles of samples during shock compression. It has been established that upon shock compression, the σHEL and σy of the submicrocrystalline alloy are higher than those of the coarse-grained alloy and σsp does not depend on the grain size. The maximum value of σHEL reached for the submicrocrystalline alloy is 0.66 GPa, which is greater than that in the coarse-crystalline alloy by 78%. The dynamic yield stress is σy = 0.31 GPa, which is higher than that of the coarse-crystalline alloy by 63%. The spall strength is σsp = 1.49 GPa. The evolution of the submicrocrystalline structure of the alloy during shock compression was studied. It has been established that a mixed nonequilibrium grain-subgrain structure with a fragment size of about 400 nm is retained after shock compression, and the dislocation density and the hardness of the alloy are increased.

  18. Emission lifetimes of a fluorescent dye under shock compression

    DOE PAGES

    Liu, Wei-long; Bassett, Will P.; Christensen, James M.; ...

    2015-10-15

    The emission lifetimes of rhodamine 6G (R6G), were measured under shock compression to 9.1 GPa, with the dual intent of better understanding molecular photophysics in extreme environments and assessing the usefulness of fluorescence lifetime microscopy to measure spatially-dependent pressure distributions in shocked microstructured media. R6G was studied as free dye dissolved in poly-methyl methacrylate (PMMA), or dye encapsulated in silica microparticles suspended in PMMA. Thin layers of these materials in impedance-matched geometries were subjected to planar single-stage shocks created by laser-driven flyer plates. A synchronized femtosecond laser excited the dye at selected times relative to flyer plate arrival and themore » emission lifetimes were measured with a streak camera. Lifetimes decreased when shocks arrived. The lifetime decrease was attributed to a shock-induced enhancement of R6G nonradiative relaxation. At least part of the relaxation involved shock-enhanced intersystem crossing. For free dye in PMMA, the lifetime decrease during the shock was shown to be a linear function of shock pressure from 0-9 GPa, with a slope of -0.22 ns·GPa -1. Furthermore, the linear relationship makes it simple to convert lifetimes into pressures. Lifetime measurements in shocked microenvironments may be better than emission intensity measurements, since lifetimes are sensitive to the surrounding environment, but insensitive to intensity variations associated with the motion and optical properties of a dynamically changing structure.« less

  19. Ultrafast transformation of graphite to diamond: an ab initio study of graphite under shock compression.

    PubMed

    Mundy, Christopher J; Curioni, Alessandro; Goldman, Nir; Will Kuo, I-F; Reed, Evan J; Fried, Laurence E; Ianuzzi, Marcella

    2008-05-14

    We report herein ab initio molecular dynamics simulations of graphite under shock compression in conjunction with the multiscale shock technique. Our simulations reveal that a novel short-lived layered diamond intermediate is formed within a few hundred of femtoseconds upon shock loading at a shock velocity of 12 kms (longitudinal stress>130 GPa), followed by formation of cubic diamond. The layered diamond state differs from the experimentally observed hexagonal diamond intermediate found at lower pressures and previous hydrostatic calculations in that a rapid buckling of the graphitic planes produces a mixture of hexagonal and cubic diamond (layered diamond). Direct calculation of the x-ray absorption spectra in our simulations reveals that the electronic structure of the final state closely resembles that of compressed cubic diamond.

  20. Shock compression response of forsterite above 250 GPa

    PubMed Central

    Sekine, Toshimori; Ozaki, Norimasa; Miyanishi, Kohei; Asaumi, Yuto; Kimura, Tomoaki; Albertazzi, Bruno; Sato, Yuya; Sakawa, Youichi; Sano, Takayoshi; Sugita, Seiji; Matsui, Takafumi; Kodama, Ryosuke

    2016-01-01

    Forsterite (Mg2SiO4) is one of the major planetary materials, and its behavior under extreme conditions is important to understand the interior structure of large planets, such as super-Earths, and large-scale planetary impact events. Previous shock compression measurements of forsterite indicate that it may melt below 200 GPa, but these measurements did not go beyond 200 GPa. We report the shock response of forsterite above ~250 GPa, obtained using the laser shock wave technique. We simultaneously measured the Hugoniot and temperature of shocked forsterite and interpreted the results to suggest the following: (i) incongruent crystallization of MgO at 271 to 285 GPa, (ii) phase transition of MgO at 285 to 344 GPa, and (iii) remelting above ~470 to 500 GPa. These exothermic and endothermic reactions are seen to occur under extreme conditions of pressure and temperature. They indicate complex structural and chemical changes in the system MgO-SiO2 at extreme pressures and temperatures and will affect the way we understand the interior processes of large rocky planets as well as material transformation by impacts in the formation of planetary systems. PMID:27493993

  1. Shock compression of Fe-FeS mixture up to 204 GPa

    NASA Astrophysics Data System (ADS)

    Huang, Haijun; Wu, Shijie; Hu, Xiaojun; Wang, Qingsong; Wang, Xiang; Fei, Yingwei

    2013-02-01

    AbstractUsing a two-stage light gas gun, we obtained new <span class="hlt">shock</span> wave Hugoniot data for an <span class="hlt">iron</span>-sulfur alloy (Fe-11.8wt%S) over the pressure range of 94-204 GPa. A least-squares fit to the Hugoniot data yields a linear relationship between <span class="hlt">shock</span> velocity DS and particle velocity u, DS (km/s) =3.60(0.14) +1.57(0.05) u. The measured Hugoniot data for Fe-11.8wt%S agree well with the calculated results based on the thermodynamic parameters of Fe and FeS using the additive law. By comparing the calculated densities along the adiabatic core temperature with the PREM density profile, an <span class="hlt">iron</span> core with 10 wt.% sulfur (S) provides the best solution for the composition of the Earth's outer core.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1328805-directional-amorphization-boron-carbide-subjected-laser-shock-compression','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1328805-directional-amorphization-boron-carbide-subjected-laser-shock-compression"><span>Directional amorphization of boron carbide subjected to laser <span class="hlt">shock</span> <span class="hlt">compression</span></span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>Zhao, Shiteng; Kad, Bimal; Remington, Bruce A.; ...</p> <p>2016-10-12</p> <p>Solid-state <span class="hlt">shock</span>-wave propagation is strongly nonequilibrium in nature and hence rate dependent. When using high-power pulsed-laser-driven <span class="hlt">shock</span> <span class="hlt">compression</span>, an unprecedented high strain rates can be achieved; we report the directional amorphization in boron carbide polycrystals. At a <span class="hlt">shock</span> pressure of 45~50 GPa, multiple planar faults, slightly deviated from maximum shear direction, occur a few hundred nanometers below the <span class="hlt">shock</span> surface. High-resolution transmission electron microscopy reveals that these planar faults are precursors of directional amorphization. We also propose that the shear stresses cause the amorphization and that pressure assists the process by ensuring the integrity of the specimen. Thermal energy conversionmore » calculations including heat transfer suggest that amorphization is a solid-state process. Such a phenomenon has significant effect on the ballistic performance of B 4C.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017RSOS....460939S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017RSOS....460939S"><span>A new apparatus to induce lysis of planktonic microbial cells by <span class="hlt">shock</span> <span class="hlt">compression</span>, cavitation and spray</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Schiffer, A.; Gardner, M. N.; Lynn, R. H.; Tagarielli, V. L.</p> <p>2017-03-01</p> <p>Experiments were conducted on an aqueous growth medium containing cultures of Escherichia coli (E. coli) XL1-Blue, to investigate, in a single experiment, the effect of two types of dynamic mechanical loading on cellular integrity. A bespoke <span class="hlt">shock</span> tube was used to subject separate portions of a planktonic bacterial culture to two different loading sequences: (i) <span class="hlt">shock</span> <span class="hlt">compression</span> followed by cavitation, and (ii) <span class="hlt">shock</span> <span class="hlt">compression</span> followed by spray. The apparatus allows the generation of an adjustable loading <span class="hlt">shock</span> wave of magnitude up to 300 MPa in a sterile laboratory environment. Cultures of E. coli were tested with this apparatus and the spread-plate technique was used to measure the survivability after mechanical loading. The loading sequence (ii) gave higher mortality than (i), suggesting that the bacteria are more vulnerable to shear deformation and cavitation than to hydrostatic <span class="hlt">compression</span>. We present the results of preliminary experiments and suggestions for further experimental work; we discuss the potential applications of this technique to sterilize large volumes of fluid samples.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/12570505','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/12570505"><span>Use of a wave reverberation technique to infer the density <span class="hlt">compression</span> of <span class="hlt">shocked</span> liquid deuterium to 75 GPa.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Knudson, M D; Hanson, D L; Bailey, J E; Hall, C A; Asay, J R</p> <p>2003-01-24</p> <p>A novel approach was developed to probe density <span class="hlt">compression</span> of liquid deuterium (L-D2) along the principal Hugoniot. Relative transit times of <span class="hlt">shock</span> waves reverberating within the sample are shown to be sensitive to the <span class="hlt">compression</span> due to the first <span class="hlt">shock</span>. This technique has proven to be more sensitive than the conventional method of inferring density from the <span class="hlt">shock</span> and mass velocity, at least in this high-pressure regime. Results in the range of 22-75 GPa indicate an approximately fourfold density <span class="hlt">compression</span>, and provide data to differentiate between proposed theories for hydrogen and its isotopes.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4773851','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4773851"><span><span class="hlt">Shock</span> Wave Response of <span class="hlt">Iron</span>-based In Situ Metallic Glass Matrix Composites</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Khanolkar, Gauri R.; Rauls, Michael B.; Kelly, James P.; Graeve, Olivia A.; Hodge, Andrea M.; Eliasson, Veronica</p> <p>2016-01-01</p> <p>The response of amorphous steels to <span class="hlt">shock</span> wave <span class="hlt">compression</span> has been explored for the first time. Further, the effect of partial devitrification on the <span class="hlt">shock</span> response of bulk metallic glasses is examined by conducting experiments on two <span class="hlt">iron</span>-based in situ metallic glass matrix composites, containing varying amounts of crystalline precipitates, both with initial composition Fe49.7Cr17.7Mn1.9Mo7.4W1.6B15.2C3.8Si2.4. The samples, designated SAM2X5-600 and SAM2X5-630, are X-ray amorphous and partially crystalline, respectively, due to differences in sintering parameters during sample preparation. <span class="hlt">Shock</span> response is determined by making velocity measurements using interferometry techniques at the rear free surface of the samples, which have been subjected to impact from a high-velocity projectile launched from a powder gun. Experiments have yielded results indicating a Hugoniot Elastic Limit (HEL) to be 8.58 ± 0.53 GPa for SAM2X5-600 and 11.76 ± 1.26 GPa for SAM2X5-630. The latter HEL result is higher than elastic limits for any BMG reported in the literature thus far. SAM2X5-600 catastrophically loses post-yield strength whereas SAM2X5-630, while showing some strain-softening, retains strength beyond the HEL. The presence of crystallinity within the amorphous matrix is thus seen to significantly aid in strengthening the material as well as preserving material strength beyond yielding. PMID:26932846</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/26932846','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/26932846"><span><span class="hlt">Shock</span> Wave Response of <span class="hlt">Iron</span>-based In Situ Metallic Glass Matrix Composites.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Khanolkar, Gauri R; Rauls, Michael B; Kelly, James P; Graeve, Olivia A; Hodge, Andrea M; Eliasson, Veronica</p> <p>2016-03-02</p> <p>The response of amorphous steels to <span class="hlt">shock</span> wave <span class="hlt">compression</span> has been explored for the first time. Further, the effect of partial devitrification on the <span class="hlt">shock</span> response of bulk metallic glasses is examined by conducting experiments on two <span class="hlt">iron</span>-based in situ metallic glass matrix composites, containing varying amounts of crystalline precipitates, both with initial composition Fe49.7Cr17.7Mn1.9Mo7.4W1.6B15.2C3.8Si2.4. The samples, designated SAM2X5-600 and SAM2X5-630, are X-ray amorphous and partially crystalline, respectively, due to differences in sintering parameters during sample preparation. <span class="hlt">Shock</span> response is determined by making velocity measurements using interferometry techniques at the rear free surface of the samples, which have been subjected to impact from a high-velocity projectile launched from a powder gun. Experiments have yielded results indicating a Hugoniot Elastic Limit (HEL) to be 8.58 ± 0.53 GPa for SAM2X5-600 and 11.76 ± 1.26 GPa for SAM2X5-630. The latter HEL result is higher than elastic limits for any BMG reported in the literature thus far. SAM2X5-600 catastrophically loses post-yield strength whereas SAM2X5-630, while showing some strain-softening, retains strength beyond the HEL. The presence of crystallinity within the amorphous matrix is thus seen to significantly aid in strengthening the material as well as preserving material strength beyond yielding.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017AGUFMMR34B..02D','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017AGUFMMR34B..02D"><span>Ultrahigh Pressure Dynamic <span class="hlt">Compression</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Duffy, T. S.</p> <p>2017-12-01</p> <p>Laser-based dynamic <span class="hlt">compression</span> provides a new opportunity to study the lattice structure and other properties of geological materials to ultrahigh pressure conditions ranging from 100 - 1000 GPa (1 TPa) and beyond. Such studies have fundamental applications to understanding the Earth's core as well as the interior structure of super-Earths and giant planets. This talk will review recent dynamic <span class="hlt">compression</span> experiments using high-powered lasers on materials including Fe-Si, MgO, and SiC. Experiments were conducted at the Omega laser (University of Rochester) and the Linac Coherent Light Source (LCLS, Stanford). At Omega, laser drives as large as 2 kJ are applied over 10 ns to samples that are 50 microns thick. At peak <span class="hlt">compression</span>, the sample is probed with quasi-monochromatic X-rays from a laser-plasma source and diffraction is recorded on image plates. At LCLS, <span class="hlt">shock</span> waves are driven into the sample using a 40-J laser with a 10-ns pulse. The sample is probed with X-rays form the LCLS free electron laser providing 1012 photons in a monochromatic pulse near 10 keV energy. Diffraction is recorded using pixel array detectors. By varying the delay between the laser and the x-ray beam, the sample can be probed at various times relative to the <span class="hlt">shock</span> wave transiting the sample. By controlling the shape and duration of the incident laser pulse, either <span class="hlt">shock</span> or ramp (shockless) loading can be produced. Ramp <span class="hlt">compression</span> produces less heating than <span class="hlt">shock</span> <span class="hlt">compression</span>, allowing samples to be probed to ultrahigh pressures without melting. Results for <span class="hlt">iron</span> alloys, oxides, and carbides provide new constraints on equations of state and phase transitions that are relevant to the interior structure of large, extrasolar terrestrial-type planets.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2012GeoRL..39.5306L','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2012GeoRL..39.5306L"><span>Structure of <span class="hlt">shock</span> <span class="hlt">compressed</span> model basaltic glass: Insights from O K-edge X-ray Raman scattering and high-resolution 27Al NMR spectroscopy</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Lee, Sung Keun; Park, Sun Young; Kim, Hyo-Im; Tschauner, Oliver; Asimow, Paul; Bai, Ligang; Xiao, Yuming; Chow, Paul</p> <p>2012-03-01</p> <p>The detailed atomic structures of <span class="hlt">shock</span> <span class="hlt">compressed</span> basaltic glasses are not well understood. Here, we explore the structures of <span class="hlt">shock</span> <span class="hlt">compressed</span> silicate glass with a diopside-anorthite eutectic composition (Di64An36), a common Fe-free model basaltic composition, using oxygen K-edge X-ray Raman scattering and high- resolution 27Al solid-state NMR spectroscopy and report previously unknown details of <span class="hlt">shock</span>-induced changes in the atomic configurations. A topologically driven densification of the Di64An36 glass is indicated by the increase in oxygen K-edge energy for the glass upon <span class="hlt">shock</span> <span class="hlt">compression</span>. The first experimental evidence of the increase in the fraction of highly coordinated Al in <span class="hlt">shock</span> <span class="hlt">compressed</span> glass is found in the 27Al NMR spectra. This unambiguous evidence of <span class="hlt">shock</span>-induced changes in Al coordination environments provides atomistic insights into <span class="hlt">shock</span> <span class="hlt">compression</span> in basaltic glasses and allows us to microscopically constrain the magnitude of impact events or relevant processes involving natural basalts on Earth and planetary surfaces.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5179968','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5179968"><span>Hugoniot equation of state of rock materials under <span class="hlt">shock</span> <span class="hlt">compression</span></span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Braithwaite, C. H.; Zhao, J.</p> <p>2017-01-01</p> <p>Two sets of <span class="hlt">shock</span> <span class="hlt">compression</span> tests (i.e. conventional and reverse impact) were conducted to determine the <span class="hlt">shock</span> response of two rock materials using a plate impact facility. Embedded manganin stress gauges were used for the measurements of longitudinal stress and <span class="hlt">shock</span> velocity. Photon Doppler velocimetry was used to capture the free surface velocity of the target. Experimental data were obtained on a fine-grained marble and a coarse-grained gabbro over a <span class="hlt">shock</span> pressure range of approximately 1.5–12 GPa. Gabbro exhibited a linear Hugoniot equation of state (EOS) in the pressure–particle velocity (P–up) plane, while for marble a nonlinear response was observed. The EOS relations between <span class="hlt">shock</span> velocity (US) and particle velocity (up) are linearly fitted as US = 2.62 + 3.319up and US = 5.4 85 + 1.038up for marble and gabbro, respectively. This article is part of the themed issue ‘Experimental testing and modelling of brittle materials at high strain rates’. PMID:27956506</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015APS..SHK.Z3002L','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015APS..SHK.Z3002L"><span>Enhanced densification, strength and molecular mechanisms in <span class="hlt">shock</span> <span class="hlt">compressed</span> porous silicon</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Lane, J. Matthew D.; Vogler, Tracy J.</p> <p>2015-06-01</p> <p>In most porous materials, void collapse during <span class="hlt">shock</span> <span class="hlt">compression</span> couples mechanical energy to thermal energy. Increased temperature drives up pressures and lowers densities in the final Hugoniot states as compared to full-density samples. Some materials, however, exhibit an anomalous enhanced densification in their Hugoniot states when porosity is introduced. We have recently shown that silicon is such a material, and demonstrated a molecular mechanism for the effect using molecular simulation. We will review results from large-scale non-equilibrium molecular dynamics (NEMD) and Hugoniotstat simulations of <span class="hlt">shock</span> <span class="hlt">compressed</span> porous silicon, highlighting the mechanism by which porosity produces local shear which nucleate partial phase transition and localized melting at <span class="hlt">shock</span> pressures below typical thresholds in these materials. Further, we will characterize the stress states and strength of the material as a function of porosity from 5 to 50 percent and with various porosity microstructures. Sandia National Laboratories is a multi program laboratory managed and operated by Sandia Corporation, a wholly owned subsidiary of Lockheed Martin Corporation, for the U.S. Department of Energy's National Nuclear Security Administration under contract DE-AC04-94AL85000.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19950009605','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19950009605"><span><span class="hlt">Shock</span> and thermal history of <span class="hlt">iron</span> and chondritic meteorites</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Goldstein, Joseph I.</p> <p>1994-01-01</p> <p>This research grant included a study of the <span class="hlt">shock</span> and thermal history of <span class="hlt">iron</span> and chondritic meteorites. The important research findings are to be found in the 20 publications that were published as a result of the research support. A complete bibliographic reference to all these papers is given.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017APS..SHK.L7002N','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017APS..SHK.L7002N"><span><span class="hlt">Shock</span> Induced Phase Changes in Forsterite and <span class="hlt">Iron</span> Silicide</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Newman, M.; Asimow, P.; Kraus, R. G.; Smith, R.; Coppari, F.; Eggert, J. H.; Wicks, J.; Tracy, S.; Duffy, T.</p> <p>2017-06-01</p> <p>The equation of state of magnesium silicates and <span class="hlt">iron</span> alloys at the pressures and temperatures near the melt curve is important for understanding the thermal evolution and interior structure of rocky planets. Here, we present a series of laser driven <span class="hlt">shock</span> experiments on single crystal Mg2SiO4 and textured polycrystalline <span class="hlt">iron</span> silicide (Fe-15Si), conducted at LLE. In situ x-ray diffraction measurements were used to probe the melting transition and investigate the potential decomposition of forsterite into solid MgO and silica rich liquid and Fe-15Si in to silicon rich B2 and <span class="hlt">iron</span> rich hcp structures. This work examines kinetic effects of chemical decomposition due to the short time scale of laser-<span class="hlt">shock</span> experiments. Preliminary results demonstrate solid-solid and solid-liquid phase transitions on both the forsterite and Fe-15Si Hugoniots. For Fe-15Si, we observe a texture preserving martensitic transformation of D03 Fe-15Si into an hcp structure and melting at 318 GPa. For forsterite, we observe diffraction consistent with B1 MgO and melting at 215 GPa. This work was performed under the auspices of the U.S. Department of Energy by Lawrence Livermore National Laboratory under Contract DE-AC52-07NA27344.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2009ChPhL..26c8301L','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2009ChPhL..26c8301L"><span>CROSS-DISCIPLINARY PHYSICS AND RELATED AREAS OF SCIENCE AND TECHNOLOGY: Measurement on Effective Shear Viscosity Coefficient of <span class="hlt">Iron</span> under <span class="hlt">Shock</span> <span class="hlt">Compression</span> at 100 GPa</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Li, Yi-Lei; Liu, Fu-Sheng; Zhang, Ming-Jian; Ma, Xiao-Juan; Li, Ying-Lei; Zhang, Ji-Chun</p> <p>2009-03-01</p> <p>The oscillatory damping curve of a <span class="hlt">shock</span> front propagating in <span class="hlt">iron</span> <span class="hlt">shocked</span> to 103 GPa is measured by use of two-stage light-gas gun and electric pin techniques. The corresponding effective shear viscosity coefficient is deduced to be about 2000 Pa·s from Miller and Ahrens' formula. The result is consistent with that of Mineev's data at 31GPa, while it is higher by five orders than the predictions based on the static measurements at about 5 GPa and 2000 K and molecular dynamic simulation up to 135-375 GPa and 4300-6000 K, and the discussions are presented.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5383840','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5383840"><span>A new apparatus to induce lysis of planktonic microbial cells by <span class="hlt">shock</span> <span class="hlt">compression</span>, cavitation and spray</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Schiffer, A.; Gardner, M. N.; Lynn, R. H.</p> <p>2017-01-01</p> <p>Experiments were conducted on an aqueous growth medium containing cultures of Escherichia coli (E. coli) XL1-Blue, to investigate, in a single experiment, the effect of two types of dynamic mechanical loading on cellular integrity. A bespoke <span class="hlt">shock</span> tube was used to subject separate portions of a planktonic bacterial culture to two different loading sequences: (i) <span class="hlt">shock</span> <span class="hlt">compression</span> followed by cavitation, and (ii) <span class="hlt">shock</span> <span class="hlt">compression</span> followed by spray. The apparatus allows the generation of an adjustable loading <span class="hlt">shock</span> wave of magnitude up to 300 MPa in a sterile laboratory environment. Cultures of E. coli were tested with this apparatus and the spread-plate technique was used to measure the survivability after mechanical loading. The loading sequence (ii) gave higher mortality than (i), suggesting that the bacteria are more vulnerable to shear deformation and cavitation than to hydrostatic <span class="hlt">compression</span>. We present the results of preliminary experiments and suggestions for further experimental work; we discuss the potential applications of this technique to sterilize large volumes of fluid samples. PMID:28405383</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/28405383','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/28405383"><span>A new apparatus to induce lysis of planktonic microbial cells by <span class="hlt">shock</span> <span class="hlt">compression</span>, cavitation and spray.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Schiffer, A; Gardner, M N; Lynn, R H; Tagarielli, V L</p> <p>2017-03-01</p> <p>Experiments were conducted on an aqueous growth medium containing cultures of Escherichia coli ( E. coli ) XL1-Blue, to investigate, in a single experiment, the effect of two types of dynamic mechanical loading on cellular integrity. A bespoke <span class="hlt">shock</span> tube was used to subject separate portions of a planktonic bacterial culture to two different loading sequences: (i) <span class="hlt">shock</span> <span class="hlt">compression</span> followed by cavitation, and (ii) <span class="hlt">shock</span> <span class="hlt">compression</span> followed by spray. The apparatus allows the generation of an adjustable loading <span class="hlt">shock</span> wave of magnitude up to 300 MPa in a sterile laboratory environment. Cultures of E. coli were tested with this apparatus and the spread-plate technique was used to measure the survivability after mechanical loading. The loading sequence (ii) gave higher mortality than (i), suggesting that the bacteria are more vulnerable to shear deformation and cavitation than to hydrostatic <span class="hlt">compression</span>. We present the results of preliminary experiments and suggestions for further experimental work; we discuss the potential applications of this technique to sterilize large volumes of fluid samples.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://www.dtic.mil/docs/citations/ADA601361','DTIC-ST'); return false;" href="http://www.dtic.mil/docs/citations/ADA601361"><span>Analysis of <span class="hlt">Shock</span> <span class="hlt">Compression</span> of Strong Single Crystals With Logarithmic Thermoelastic-Plastic Theory</span></a></p> <p><a target="_blank" href="http://www.dtic.mil/">DTIC Science & Technology</a></p> <p></p> <p>2014-05-01</p> <p>Royal Society of London Series A, 465, 307–334. Clayton, J. (2010a). Modeling nonlinear electromechanical behavior of <span class="hlt">shocked</span> silicon carbide . Journal...and fourth-order longitudinal elastic constants by <span class="hlt">shock</span> <span class="hlt">compression</span> techniques–application to sapphire and fused quartz. Journal of the Acoustical...Vogler, T., & Clayton, J. (2008). Heterogeneous deformation and spall of an extruded tungsten alloy: Plate impact experiments and crystal plasticity</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015APS..SHK.C5004H','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015APS..SHK.C5004H"><span>Physics of <span class="hlt">Shock</span> <span class="hlt">Compression</span> and Release: NEMD Simulations of Tantalum and Silicon</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Hahn, Eric; Meyers, Marc; Zhao, Shiteng; Remington, Bruce; Bringa, Eduardo; Germann, Tim; Ravelo, Ramon; Hammerberg, James</p> <p>2015-06-01</p> <p><span class="hlt">Shock</span> <span class="hlt">compression</span> and release allow us to evaluate physical deformation and damage mechanisms occurring in extreme environments. SPaSM and LAMMPS molecular dynamics codes were employed to simulate single and polycrystalline tantalum and silicon at strain rates above 108 s-1. Visualization and analysis was accomplished using OVITO, Crystal Analysis Tool, and a redesigned orientation imaging function implemented into SPaSM. A comparison between interatomic potentials for both Si and Ta (as pertaining to <span class="hlt">shock</span> conditions) is conducted and the influence on phase transformation and plastic relaxation is discussed. Partial dislocations, shear induced disordering, and metastable phase changes are observed in <span class="hlt">compressed</span> silicon. For tantalum, the role of grain boundary and twin intersections are evaluated for their role in ductile spallation. Finally, the temperature dependent response of both Ta and Si is investigated.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/985406','DOE-PATENT-XML'); return false;" href="https://www.osti.gov/servlets/purl/985406"><span>Gas turbine power plant with supersonic <span class="hlt">shock</span> <span class="hlt">compression</span> ramps</span></a></p> <p><a target="_blank" href="http://www.osti.gov/doepatents">DOEpatents</a></p> <p>Lawlor, Shawn P [Bellevue, WA; Novaresi, Mark A [San Diego, CA; Cornelius, Charles C [Kirkland, WA</p> <p>2008-10-14</p> <p>A gas turbine engine. The engine is based on the use of a gas turbine driven rotor having a <span class="hlt">compression</span> ramp traveling at a local supersonic inlet velocity (based on the combination of inlet gas velocity and tangential speed of the ramp) which <span class="hlt">compresses</span> inlet gas against a stationary sidewall. The supersonic compressor efficiently achieves high <span class="hlt">compression</span> ratios while utilizing a compact, stabilized gasdynamic flow path. Operated at supersonic speeds, the inlet stabilizes an oblique/normal <span class="hlt">shock</span> system in the gasdynamic flow path formed between the rim of the rotor, the strakes, and a stationary external housing. Part load efficiency is enhanced by use of a lean pre-mix system, a pre-swirl compressor, and a bypass stream to bleed a portion of the gas after passing through the pre-swirl compressor to the combustion gas outlet. Use of a stationary low NOx combustor provides excellent emissions results.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017JAP...121k5904F','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017JAP...121k5904F"><span>Equation of state of Mo from <span class="hlt">shock</span> <span class="hlt">compression</span> experiments on preheated samples</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Fat'yanov, O. V.; Asimow, P. D.</p> <p>2017-03-01</p> <p>We present a reanalysis of reported Hugoniot data for Mo, including both experiments <span class="hlt">shocked</span> from ambient temperature (T) and those preheated to 1673 K, using the most general methods of least-squares fitting to constrain the Grüneisen model. This updated Mie-Grüneisen equation of state (EOS) is used to construct a family of maximum likelihood Hugoniots of Mo from initial temperatures of 298 to 2350 K and a parameterization valid over this range. We adopted a single linear function at each initial temperature over the entire range of particle velocities considered. Total uncertainties of all the EOS parameters and correlation coefficients for these uncertainties are given. The improved predictive capabilities of our EOS for Mo are confirmed by (1) better agreement between calculated bulk sound speeds and published measurements along the principal Hugoniot, (2) good agreement between our Grüneisen data and three reported high-pressure γ ( V ) functions obtained from <span class="hlt">shock-compression</span> of porous samples, and (3) very good agreement between our 1 bar Grüneisen values and γ ( T ) at ambient pressure recalculated from reported experimental data on the adiabatic bulk modulus K s ( T ) . Our analysis shows that an EOS constructed from <span class="hlt">shock</span> <span class="hlt">compression</span> data allows a much more accurate prediction of γ ( T ) values at 1 bar than those based on static <span class="hlt">compression</span> measurements or first-principles calculations. Published calibrations of the Mie-Grüneisen EOS for Mo using static <span class="hlt">compression</span> measurements only do not reproduce even low-pressure asymptotic values of γ ( T ) at 1 bar, where the most accurate experimental data are available.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017APS..SHK.F9057B','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017APS..SHK.F9057B"><span>Laser <span class="hlt">Shock</span> <span class="hlt">Compression</span> Studies of Phase Changes in Ce3 Al Metallic Glass</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Bryant, Alex; Wehrenberg, Christopher; Alamgir, Faisal; Remington, Bruce; Thadhani, Naresh</p> <p>2017-06-01</p> <p>Laser <span class="hlt">shock-compression</span> of Ce3 Al metallic glass (MG) was performed to probe pressure-induced phase transitions. Ce3 Al MG has been previously shown to crystallize into a single crystal FCC phase during static <span class="hlt">compression</span> at 25 GPa. In the present work, experiments were performed using the 3J Nd:YAG pulse laser at Georgia Tech and the high energy laser at the OMEGA facility. Characterization of <span class="hlt">shock</span> <span class="hlt">compressed</span> samples recovered from the OMEGA laser experiments were performed using XRD and PDF measurements at the NSLS-2 synchrotron at Brookhaven National Lab. The results showed evidence of a permanent polyamorphous phase change at pressures > 10 GPa and crystallization at pressures > 75 GPa. Particle velocities were measured using VISAR in experiments performed at Georgia Tech and simulated using Hyades and Abaqus to create an empirical equation of state and correlate with results obtained from XRD and PDF characterization. The results attained to-date in terms of the evolution of the high pressure amorphous and crystalline phases and their correlations with the <span class="hlt">shock</span> conditions will be presented. This work is supported in part by ARO Grant No. W9HNF-09-1-0403 and the National Science Foundation Graduate Research Fellowship Program awarded to Alex Bryant under Grant No. 0946809.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_3");'>3</a></li> <li><a href="#" onclick='return showDiv("page_4");'>4</a></li> <li class="active"><span>5</span></li> <li><a href="#" onclick='return showDiv("page_6");'>6</a></li> <li><a href="#" onclick='return showDiv("page_7");'>7</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_5 --> <div id="page_6" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_4");'>4</a></li> <li><a href="#" onclick='return showDiv("page_5");'>5</a></li> <li class="active"><span>6</span></li> <li><a href="#" onclick='return showDiv("page_7");'>7</a></li> <li><a href="#" onclick='return showDiv("page_8");'>8</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="101"> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016JAP...120d3107K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016JAP...120d3107K"><span>Exploration of CdTe quantum dots as mesoscale pressure sensors via time-resolved <span class="hlt">shock-compression</span> photoluminescent emission spectroscopy</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Kang, Zhitao; Banishev, Alexandr A.; Lee, Gyuhyon; Scripka, David A.; Breidenich, Jennifer; Xiao, Pan; Christensen, James; Zhou, Min; Summers, Christopher J.; Dlott, Dana D.; Thadhani, Naresh N.</p> <p>2016-07-01</p> <p>The nanometer size of CdTe quantum dots (QDs) and their unique optical properties, including size-tunable narrow photoluminescent emission, broad absorption, fast photoluminescence decay, and negligible light scattering, are ideal features for spectrally tagging the <span class="hlt">shock</span> response of localized regions in highly heterogeneous materials such as particulate media. In this work, the time-resolved laser-excited photoluminescence response of QDs to <span class="hlt">shock-compression</span> was investigated to explore their utilization as mesoscale sensors for pressure measurements and in situ diagnostics during <span class="hlt">shock</span> loading experiments. Laser-driven <span class="hlt">shock-compression</span> experiments with steady-state <span class="hlt">shock</span> pressures ranging from 2.0 to 13 GPa were performed on nanocomposite films of CdTe QDs dispersed in a soft polyvinyl alcohol polymer matrix and in a hard inorganic sodium silicate glass matrix. Time-resolved photoluminescent emission spectroscopy was used to correlate photoluminescence changes with the history of <span class="hlt">shock</span> pressure and the dynamics of the matrix material surrounding the QDs. The results revealed pressure-induced blueshifts in emitted wavelength, decreases in photoluminescent emission intensity, reductions in peak width, and matrix-dependent response times. Data obtained for these QD response characteristics serve as indicators for their use as possible time-resolved diagnostics of the dynamic <span class="hlt">shock-compression</span> response of matrix materials in which such QDs are embedded as in situ sensors.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/27740787','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/27740787"><span>Neurofilaments Function as <span class="hlt">Shock</span> Absorbers: <span class="hlt">Compression</span> Response Arising from Disordered Proteins.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Kornreich, Micha; Malka-Gibor, Eti; Zuker, Ben; Laser-Azogui, Adi; Beck, Roy</p> <p>2016-09-30</p> <p>What can cells gain by using disordered, rather than folded, proteins in the architecture of their skeleton? Disordered proteins take multiple coexisting conformations, and often contain segments which act as random-walk-shaped polymers. Using x-ray scattering we measure the <span class="hlt">compression</span> response of disordered protein hydrogels, which are the main stress-responsive component of neuron cells. We find that at high <span class="hlt">compression</span> their mechanics are dominated by gaslike steric and ionic repulsions. At low <span class="hlt">compression</span>, specific attractive interactions dominate. This is demonstrated by the considerable hydrogel expansion induced by the truncation of critical short protein segments. Accordingly, the floppy disordered proteins form a weakly cross-bridged hydrogel, and act as <span class="hlt">shock</span> absorbers that sustain large deformations without failure.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016PhRvL.117n8101K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016PhRvL.117n8101K"><span>Neurofilaments Function as <span class="hlt">Shock</span> Absorbers: <span class="hlt">Compression</span> Response Arising from Disordered Proteins</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Kornreich, Micha; Malka-Gibor, Eti; Zuker, Ben; Laser-Azogui, Adi; Beck, Roy</p> <p>2016-09-01</p> <p>What can cells gain by using disordered, rather than folded, proteins in the architecture of their skeleton? Disordered proteins take multiple coexisting conformations, and often contain segments which act as random-walk-shaped polymers. Using x-ray scattering we measure the <span class="hlt">compression</span> response of disordered protein hydrogels, which are the main stress-responsive component of neuron cells. We find that at high <span class="hlt">compression</span> their mechanics are dominated by gaslike steric and ionic repulsions. At low <span class="hlt">compression</span>, specific attractive interactions dominate. This is demonstrated by the considerable hydrogel expansion induced by the truncation of critical short protein segments. Accordingly, the floppy disordered proteins form a weakly cross-bridged hydrogel, and act as <span class="hlt">shock</span> absorbers that sustain large deformations without failure.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2000SPIE.3888..294S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2000SPIE.3888..294S"><span>Process and application of <span class="hlt">shock</span> <span class="hlt">compression</span> by nanosecond pulses of frequency-doubled Nd:YAG laser</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Sano, Yuji; Kimura, Motohiko; Mukai, Naruhiko; Yoda, Masaki; Obata, Minoru; Ogisu, Tatsuki</p> <p>2000-02-01</p> <p>The authors have developed a new process of laser-induced <span class="hlt">shock</span> <span class="hlt">compression</span> to introduce a residual <span class="hlt">compressive</span> stress on material surface, which is effective for prevention of stress corrosion cracking (SCC) and enhancement of fatigue strength of metal materials. The process developed is unique and beneficial. It requires no pre-conditioning for the surface, whereas the conventional process requires that the so-called sacrificial layer is made to protect the surface from damage. The new process can be freely applied to water- immersed components, since it uses water-penetrable green light of a frequency-doubled Nd:YAG laser. The process developed has the potential to open up new high-power laser applications in manufacturing and maintenance technologies. The laser-induced <span class="hlt">shock</span> <span class="hlt">compression</span> process (LSP) can be used to improve a residual stress field from tensile to <span class="hlt">compressive</span>. In order to understand the physics and optimize the process, the propagation of a <span class="hlt">shock</span> wave generated by the impulse of laser irradiation and the dynamic response of the material were analyzed by time-dependent elasto-plastic calculations with a finite element program using laser-induced plasma pressure as an external load. The analysis shows that a permanent strain and a residual <span class="hlt">compressive</span> stress remain after the passage of the <span class="hlt">shock</span> wave with amplitude exceeding the yield strength of the material. A practical system materializing the LSP was designed, manufactured, and tested to confirm the applicability to core components of light water reactors (LWRs). The system accesses the target component and remotely irradiates laser pulses to the heat affected zone (HAZ) along weld lines. Various functional tests were conducted using a full-scale mockup facility, in which remote maintenance work in a reactor vessel could be simulated. The results showed that the system remotely accessed the target weld lines and successfully introduced a residual <span class="hlt">compressive</span> stress. After sufficient training</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018JChPh.148i4504I','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018JChPh.148i4504I"><span>Effect of a core-softened O-O interatomic interaction on the <span class="hlt">shock</span> <span class="hlt">compression</span> of fused silica</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Izvekov, Sergei; Weingarten, N. Scott; Byrd, Edward F. C.</p> <p>2018-03-01</p> <p>Isotropic soft-core potentials have attracted considerable attention due to their ability to reproduce thermodynamic, dynamic, and structural anomalies observed in tetrahedral network-forming compounds such as water and silica. The aim of the present work is to assess the relevance of effective core-softening pertinent to the oxygen-oxygen interaction in silica to the thermodynamics and phase change mechanisms that occur in <span class="hlt">shock</span> <span class="hlt">compressed</span> fused silica. We utilize the MD simulation method with a recently published numerical interatomic potential derived from an ab initio MD simulation of liquid silica via force-matching. The resulting potential indicates an effective shoulder-like core-softening of the oxygen-oxygen repulsion. To better understand the role of the core-softening we analyze two derivative force-matching potentials in which the soft-core is replaced with a repulsive core either in the three-body potential term or in all the potential terms. Our analysis is further augmented by a comparison with several popular empirical models for silica that lack an explicit core-softening. The first outstanding feature of <span class="hlt">shock</span> <span class="hlt">compressed</span> glass reproduced with the soft-core models but not with the other models is that the <span class="hlt">shock</span> <span class="hlt">compression</span> values at pressures above 20 GPa are larger than those observed under hydrostatic <span class="hlt">compression</span> (an anomalous <span class="hlt">shock</span> Hugoniot densification). Our calculations indicate the occurrence of a phase transformation along the <span class="hlt">shock</span> Hugoniot that we link to the O-O repulsion core-softening. The phase transformation is associated with a Hugoniot temperature reversal similar to that observed experimentally. With the soft-core models, the phase change is an isostructural transformation between amorphous polymorphs with no associated melting event. We further examine the nature of the structural transformation by comparing it to the Hugoniot calculations for stishovite. For stishovite, the Hugoniot exhibits temperature reversal and associated</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/22597723-exploration-cdte-quantum-dots-mesoscale-pressure-sensors-via-time-resolved-shock-compression-photoluminescent-emission-spectroscopy','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/22597723-exploration-cdte-quantum-dots-mesoscale-pressure-sensors-via-time-resolved-shock-compression-photoluminescent-emission-spectroscopy"><span>Exploration of CdTe quantum dots as mesoscale pressure sensors via time-resolved <span class="hlt">shock-compression</span> photoluminescent emission spectroscopy</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Kang, Zhitao; School of Materials Science and Engineering, Georgia Institute of Technology, Atlanta, Georgia 30332-0245; Banishev, Alexandr A.</p> <p></p> <p>The nanometer size of CdTe quantum dots (QDs) and their unique optical properties, including size-tunable narrow photoluminescent emission, broad absorption, fast photoluminescence decay, and negligible light scattering, are ideal features for spectrally tagging the <span class="hlt">shock</span> response of localized regions in highly heterogeneous materials such as particulate media. In this work, the time-resolved laser-excited photoluminescence response of QDs to <span class="hlt">shock-compression</span> was investigated to explore their utilization as mesoscale sensors for pressure measurements and in situ diagnostics during <span class="hlt">shock</span> loading experiments. Laser-driven <span class="hlt">shock-compression</span> experiments with steady-state <span class="hlt">shock</span> pressures ranging from 2.0 to 13 GPa were performed on nanocomposite films of CdTe QDs dispersedmore » in a soft polyvinyl alcohol polymer matrix and in a hard inorganic sodium silicate glass matrix. Time-resolved photoluminescent emission spectroscopy was used to correlate photoluminescence changes with the history of <span class="hlt">shock</span> pressure and the dynamics of the matrix material surrounding the QDs. The results revealed pressure-induced blueshifts in emitted wavelength, decreases in photoluminescent emission intensity, reductions in peak width, and matrix-dependent response times. Data obtained for these QD response characteristics serve as indicators for their use as possible time-resolved diagnostics of the dynamic <span class="hlt">shock-compression</span> response of matrix materials in which such QDs are embedded as in situ sensors.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2011APS..DPPNO8010F','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2011APS..DPPNO8010F"><span>X-ray Scattering Measurement of the Heat Capacity Ratio in <span class="hlt">Shock</span> <span class="hlt">Compressed</span> Matter</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Fortmann, C.; Lee, H. J.; Doeppner, Tilo; Kritcher, A. L.; Landen, O. L.; Falcone, R. W.; Glenzer, S. H.</p> <p>2011-10-01</p> <p>We developed accurate x-ray scattering techniques to measure properties of matter under extreme conditions of density and temperature in intense laser-solid interaction experiments. We report on novel applications of x-ray scattering to measure the heat-capacity ratio γ =cp /cv of a Be plasma which determines the equation of state of the system. Ultraintense laser radiation is focussed onto both sides of a Be foil, creating two counterpropagating planar <span class="hlt">shock</span> waves that collide in the target center. A second set of lasers produces Zn He- α radiation of 8.9 keV energy that scatters from the <span class="hlt">shock-compressed</span> matter. We observe temperatures of 10eV and 15eV and mass densities of 5g/cm3 and 11g/cm3 before and after the <span class="hlt">shock</span> collision. Applying the Rankine-Hugoniot relations for counterpropagating <span class="hlt">shocks</span> we then infer γ as a function of density using only the measured mass <span class="hlt">compression</span> ratios. Our results agree with equation of state models and DFT simulations. This work performed under the auspices of the U.S. Department of Energy by Lawrence Livermore National Laboratory under Contract DE-AC52-07NA27344. We acknowledge support from the Alexander von Humboldt-Foundation.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018JSWSC...8A...8K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018JSWSC...8A...8K"><span>The density <span class="hlt">compression</span> ratio of <span class="hlt">shock</span> fronts associated with coronal mass ejections</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Kwon, Ryun-Young; Vourlidas, Angelos</p> <p>2018-02-01</p> <p>We present a new method to extract the three-dimensional electron density profile and density <span class="hlt">compression</span> ratio of <span class="hlt">shock</span> fronts associated with coronal mass ejections (CMEs) observed in white light coronagraph images. We demonstrate the method with two examples of fast halo CMEs (˜2000 km s-1) observed on 2011 March 7 and 2014 February 25. Our method uses the ellipsoid model to derive the three-dimensional geometry and kinematics of the fronts. The density profiles of the sheaths are modeled with double-Gaussian functions with four free parameters, and the electrons are distributed within thin shells behind the front. The modeled densities are integrated along the lines of sight to be compared with the observed brightness in COR2-A, and a χ2 approach is used to obtain the optimal parameters for the Gaussian profiles. The upstream densities are obtained from both the inversion of the brightness in a pre-event image and an empirical model. Then the density ratio and Alfvénic Mach number are derived. We find that the density <span class="hlt">compression</span> peaks around the CME nose, and decreases at larger position angles. The behavior is consistent with a driven <span class="hlt">shock</span> at the nose and a freely propagating <span class="hlt">shock</span> wave at the CME flanks. Interestingly, we find that the supercritical region extends over a large area of the <span class="hlt">shock</span> and lasts longer (several tens of minutes) than past reports. It follows that CME <span class="hlt">shocks</span> are capable of accelerating energetic particles in the corona over extended spatial and temporal scales and are likely responsible for the wide longitudinal distribution of these particles in the inner heliosphere. Our results also demonstrate the power of multi-viewpoint coronagraphic observations and forward modeling in remotely deriving key <span class="hlt">shock</span> properties in an otherwise inaccessible regime.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/26972122','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/26972122"><span>Nanosecond formation of diamond and lonsdaleite by <span class="hlt">shock</span> <span class="hlt">compression</span> of graphite.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Kraus, D; Ravasio, A; Gauthier, M; Gericke, D O; Vorberger, J; Frydrych, S; Helfrich, J; Fletcher, L B; Schaumann, G; Nagler, B; Barbrel, B; Bachmann, B; Gamboa, E J; Göde, S; Granados, E; Gregori, G; Lee, H J; Neumayer, P; Schumaker, W; Döppner, T; Falcone, R W; Glenzer, S H; Roth, M</p> <p>2016-03-14</p> <p>The <span class="hlt">shock</span>-induced transition from graphite to diamond has been of great scientific and technological interest since the discovery of microscopic diamonds in remnants of explosively driven graphite. Furthermore, <span class="hlt">shock</span> synthesis of diamond and lonsdaleite, a speculative hexagonal carbon polymorph with unique hardness, is expected to happen during violent meteor impacts. Here, we show unprecedented in situ X-ray diffraction measurements of diamond formation on nanosecond timescales by <span class="hlt">shock</span> <span class="hlt">compression</span> of pyrolytic as well as polycrystalline graphite to pressures from 19 GPa up to 228 GPa. While we observe the transition to diamond starting at 50 GPa for both pyrolytic and polycrystalline graphite, we also record the direct formation of lonsdaleite above 170 GPa for pyrolytic samples only. Our experiment provides new insights into the processes of the <span class="hlt">shock</span>-induced transition from graphite to diamond and uniquely resolves the dynamics that explain the main natural occurrence of the lonsdaleite crystal structure being close to meteor impact sites.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1249384-nanosecond-formation-diamond-lonsdaleite-shock-compression-graphite','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1249384-nanosecond-formation-diamond-lonsdaleite-shock-compression-graphite"><span>Nanosecond formation of diamond and lonsdaleite by <span class="hlt">shock</span> <span class="hlt">compression</span> of graphite</span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>Kraus, D.; Ravasio, A.; Gauthier, M.; ...</p> <p>2016-03-14</p> <p>The <span class="hlt">shock</span>-induced transition from graphite to diamond has been of great scientific and technological interest since the discovery of microscopic diamonds in remnants of explosively driven graphite. Furthermore, <span class="hlt">shock</span> synthesis of diamond and lonsdaleite, a speculative hexagonal carbon polymorph with unique hardness, is expected to happen during violent meteor impacts. Here, we show unprecedented in situ X-ray diffraction measurements of diamond formation on nanosecond timescales by <span class="hlt">shock</span> <span class="hlt">compression</span> of pyrolytic as well as polycrystalline graphite to pressures from 19 GPa up to 228 GPa. While we observe the transition to diamond starting at 50 GPa for both pyrolytic and polycrystallinemore » graphite, we also record the direct formation of lonsdaleite above 170 GPa for pyrolytic samples only. In conclusion, our experiment provides new insights into the processes of the <span class="hlt">shock</span>-induced transition from graphite to diamond and uniquely resolves the dynamics that explain the main natural occurrence of the lonsdaleite crystal structure being close to meteor impact sites.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4793081','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4793081"><span>Nanosecond formation of diamond and lonsdaleite by <span class="hlt">shock</span> <span class="hlt">compression</span> of graphite</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Kraus, D.; Ravasio, A.; Gauthier, M.; Gericke, D. O.; Vorberger, J.; Frydrych, S.; Helfrich, J.; Fletcher, L. B.; Schaumann, G.; Nagler, B.; Barbrel, B.; Bachmann, B.; Gamboa, E. J.; Göde, S.; Granados, E.; Gregori, G.; Lee, H. J.; Neumayer, P.; Schumaker, W.; Döppner, T.; Falcone, R. W.; Glenzer, S. H.; Roth, M.</p> <p>2016-01-01</p> <p>The <span class="hlt">shock</span>-induced transition from graphite to diamond has been of great scientific and technological interest since the discovery of microscopic diamonds in remnants of explosively driven graphite. Furthermore, <span class="hlt">shock</span> synthesis of diamond and lonsdaleite, a speculative hexagonal carbon polymorph with unique hardness, is expected to happen during violent meteor impacts. Here, we show unprecedented in situ X-ray diffraction measurements of diamond formation on nanosecond timescales by <span class="hlt">shock</span> <span class="hlt">compression</span> of pyrolytic as well as polycrystalline graphite to pressures from 19 GPa up to 228 GPa. While we observe the transition to diamond starting at 50 GPa for both pyrolytic and polycrystalline graphite, we also record the direct formation of lonsdaleite above 170 GPa for pyrolytic samples only. Our experiment provides new insights into the processes of the <span class="hlt">shock</span>-induced transition from graphite to diamond and uniquely resolves the dynamics that explain the main natural occurrence of the lonsdaleite crystal structure being close to meteor impact sites. PMID:26972122</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2008PhRvE..78f6115S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2008PhRvE..78f6115S"><span><span class="hlt">Shock</span> formation and the ideal shape of ramp <span class="hlt">compression</span> waves</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Swift, Damian C.; Kraus, Richard G.; Loomis, Eric N.; Hicks, Damien G.; McNaney, James M.; Johnson, Randall P.</p> <p>2008-12-01</p> <p>We derive expressions for <span class="hlt">shock</span> formation based on the local curvature of the flow characteristics during dynamic <span class="hlt">compression</span>. Given a specific ramp adiabat, calculated for instance from the equation of state for a substance, the ideal nonlinear shape for an applied ramp loading history can be determined. We discuss the region affected by lateral release, which can be presented in compact form for the ideal loading history. Example calculations are given for representative metals and plastic ablators. Continuum dynamics (hydrocode) simulations were in good agreement with the algebraic forms. Example applications are presented for several classes of laser-loading experiment, identifying conditions where <span class="hlt">shocks</span> are desired but not formed, and where long-duration ramps are desired.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017AGUFMMR43C0487S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017AGUFMMR43C0487S"><span>Melting of <span class="hlt">Iron</span> to 290 Gigapascals</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Sinmyo, R.; Hirose, K.; Ohishi, Y.</p> <p>2017-12-01</p> <p>The Earth's core is composed mainly of <span class="hlt">iron</span>. Since liquid core coexists with solid core at the inner core boundary (ICB), the melting point of <span class="hlt">iron</span> at 330 gigapascals offers a key constraint on core temperatures. However, previous results using a laser-heated diamond-anvil cell (DAC) have been largely inconsistent with each other, likely because of an intrinsic large temperature gradient and its temporal fluctuation. Here we employed an internal-resistance-heated DAC and determined the melting temperature of pure <span class="hlt">iron</span> up to 290 gigapascals, the highest ever in static <span class="hlt">compression</span> experiments. A small extrapolation indicates a melting point of 5500 ± 80 kelvin at the ICB, about 500-1000 degrees lower than earlier <span class="hlt">shock-compression</span> data. It suggests a relatively low temperature for the core-mantle boundary, which avoids global melting of the lowermost mantle in the last more than 1.5 billion years.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=20040065781&hterms=Harvard&qs=N%3D0%26Ntk%3DAll%26Ntx%3Dmode%2Bmatchall%26Ntt%3DHarvard','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=20040065781&hterms=Harvard&qs=N%3D0%26Ntk%3DAll%26Ntx%3Dmode%2Bmatchall%26Ntt%3DHarvard"><span>The <span class="hlt">Shock</span> <span class="hlt">Compression</span> Laboratory at Harvard: A New Facility for Planetary Impact Processes</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Stewart, S. T.</p> <p>2004-01-01</p> <p>The <span class="hlt">Shock</span> <span class="hlt">Compression</span> Laboratory in the Department of Earth and Planetary Sciences at Harvard is a new facility for the study of impact and collisional phenomena. The following describes the experimental capabilities of the laboratory.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018ShWav.tmp...47W','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018ShWav.tmp...47W"><span><span class="hlt">Shock</span> wave and flame front induced detonation in a rapid <span class="hlt">compression</span> machine</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Wang, Y.; Qi, Y.; Xiang, S.; Mével, R.; Wang, Z.</p> <p>2018-05-01</p> <p>The present study focuses on one mode of detonation initiation observed in a rapid <span class="hlt">compression</span> machine (RCM). This mode is referred to as <span class="hlt">shock</span> wave and flame front-induced detonation (SWFID). Experimental high-speed imaging and two-dimensional numerical simulations with skeletal chemistry are combined to unravel the dominant steps of detonation initiation under SWFID conditions. It is shown that the interaction between the <span class="hlt">shock</span> wave generated by the end-gas auto-ignition and the spherical flame creates a region of high pressure and temperature which enables the acceleration of the flame front and the detonation onset. The experimental observation lacks adequate spatial and temporal resolution despite good reproducibility of the detonation onset. Based on the numerical results, phenomenological interpretation of the event within the framework of <span class="hlt">shock</span> wave refraction indicates that the formation of a free-precursor <span class="hlt">shock</span> wave at the transition between regular and irregular refraction may be responsible for detonation onset. The present results along with previous findings on <span class="hlt">shock</span> wave reflection-induced detonation in the RCM indicate that super-knock occurs after the interaction of the <span class="hlt">shock</span> wave generated by end-gas auto-ignition with the RCM walls, preignition flame, or another <span class="hlt">shock</span> wave.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1418956-equation-state-shock-compression-warm-dense-sodiuma-first-principles-study','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1418956-equation-state-shock-compression-warm-dense-sodiuma-first-principles-study"><span>Equation of state and <span class="hlt">shock</span> <span class="hlt">compression</span> of warm dense sodium—A first-principles study</span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>Zhang, Shuai; Driver, Kevin P.; Soubiran, Francois; ...</p> <p>2017-02-21</p> <p>As one of the simple alkali metals, sodium has been of fundamental interest for <span class="hlt">shock</span> physics experiments, but knowledge of its equation of state (EOS) in hot, dense regimes is not well known. By combining path integral Monte Carlo (PIMC) results for partially ionized states at high temperatures and density functional theory molecular dynamics (DFT-MD) results at lower temperatures, we have constructed a coherent equation of state for sodium over a wide density-temperature range of 1.93-11.60 g/cm 3 and 10 3–1.29×10 8 K. We find that a localized, Hartree-Fock nodal structure in PIMC yields pressures and internal energies that aremore » consistent with DFT-MD at intermediate temperatures of 2×10 6 K. Since PIMC and DFT-MD provide a first-principles treatment of electron shell and excitation effects, we are able to identify two <span class="hlt">compression</span> maxima in the <span class="hlt">shock</span> Hugoniot curve corresponding to K-shell and L-shell ionization. Our Hugoniot curves provide a benchmark for widely used EOS models: SESAME, LEOS, and Purgatorio. Due to the low ambient density, sodium has an unusually high first <span class="hlt">compression</span> maximum along the <span class="hlt">shock</span> Hugoniot curve. At beyond 10 7 K, we show that the radiation effect leads to very high <span class="hlt">compression</span> along the Hugoniot curve, surpassing relativistic corrections, and observe an increasing deviation of the <span class="hlt">shock</span> and particle velocities from a linear relation. Here, we also compute the temperature-density dependence of thermal and pressure ionization processes.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017APS..SHK.V6005R','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017APS..SHK.V6005R"><span><span class="hlt">Shock</span> <span class="hlt">Compression</span> Response of Calcium Fluoride (CaF2)</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Root, Seth</p> <p>2017-06-01</p> <p>The fluorite crystal structure is a textbook lattice that is observed for many systems, such as CaF2, Mg2 Si, and CeO2. Specifically, CaF2 is a useful material for studying the fluorite system because it is readily available as a single crystal. Under static <span class="hlt">compression</span>, CaF2 is known to have at least three solid phases: fluorite, cotunnite, and a Ni2 In phase. Along the Hugoniot CaF2 undergoes a fluorite to cotunnite phase transition, however, at higher <span class="hlt">shock</span> pressures it is unknown whether CaF2 undergoes another solid phase transition or melts directly from the cotunnite phase. In this work, we conducted planar <span class="hlt">shock</span> <span class="hlt">compression</span> experiments on CaF2 using Sandia's Z-machine and a two-stage light gun up to 900 GPa. In addition, we use density functional theory (DFT) based quantum molecular dynamics (QMD) simulations to provide insight into the CaF2 state along the Hugoniot. In collaboration with: Michael Desjarlais, Ray Lemke, Patricia Kalita, Scott Alexander, Sandia National Laboratories. Sandia National Laboratories is a multi-mission laboratory managed and operated by Sandia Corporation, a wholly owned subsidiary of Lockheed Martin Corporation, for the U.S. Department of Energy's National Nuclear Security Administration under contract DE-AC04-94AL850.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015JAP...117h5901G','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015JAP...117h5901G"><span>Morphological changes in polycrystalline Fe after <span class="hlt">compression</span> and release</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Gunkelmann, Nina; Tramontina, Diego R.; Bringa, Eduardo M.; Urbassek, Herbert M.</p> <p>2015-02-01</p> <p>Despite a number of large-scale molecular dynamics simulations of <span class="hlt">shock</span> <span class="hlt">compressed</span> <span class="hlt">iron</span>, the morphological properties of simulated recovered samples are still unexplored. Key questions remain open in this area, including the role of dislocation motion and deformation twinning in shear stress release. In this study, we present simulations of homogeneous uniaxial <span class="hlt">compression</span> and recovery of large polycrystalline <span class="hlt">iron</span> samples. Our results reveal significant recovery of the body-centered cubic grains with some deformation twinning driven by shear stress, in agreement with experimental results by Wang et al. [Sci. Rep. 3, 1086 (2013)]. The twin fraction agrees reasonably well with a semi-analytical model which assumes a critical shear stress for twinning. On reloading, twins disappear and the material reaches a very low strength value.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/1986RpPhM.......11G','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/1986RpPhM.......11G"><span>Interaction of air <span class="hlt">shock</span> waves and porous <span class="hlt">compressible</span> materials</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Gvozdeva, L. G.; Faresov, Yu. M.; Fokeyev, V. P.</p> <p>1986-05-01</p> <p>Interaction of air <span class="hlt">shock</span> waves and porous <span class="hlt">compressible</span> materials was studied in an experiment with two foam-plastic materials: PPU-3M-1 polyurethane (density 33 kg/cu m) and much more rigid PKhV-1 polyvinyl chloride (density 50 kg/cu m). Tests were performed in a <span class="hlt">shock</span> tube with 0.1x0.1 m square cross-section, a single diaphragm separating its 8 m long low-pressure segment with inspection zone and 1.5 m long high-pressure segment. The instrumentation included an array of piezoelectric pressure transducers and a digital frequency meter for velocity measurements, a Tectronix 451A oscillograph, and IAB-451 shadowgraph, and a ZhFR camera with slit scanning. Air was used as <span class="hlt">compressing</span> gas, its initial pressure being varied from 10(3) Pa to 10(5) Pa, helium and nitrogen were used as propelling gas. The impact velocity of <span class="hlt">shock</span> waves was varied over the N(M) = 2-5 range of the Mach number. The maximum amplitude of the pressure pulse increased as the thickness of the foam layer was increased up to 80 mm and then remained constant with further increases of that thickness, at a level depending on the material and on the intitial conditions. A maximum pressure rise by a factor of approximately 10 was attained, with 1.3 x 10(3) Pa initial pressure and an impact velocity N(M) = 5. Reducing the initial pressure to below (0.1-0.3) x 10(3) Pa, with the impact velocity maintained at N(M) = 5, reduced the pressure rise to a factor below 3. The results are interpreted taking into account elasticity forces in the solid skeleton phase and gas filtration through the pores.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016ApPhL.108a1908X','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016ApPhL.108a1908X"><span>Laser-excited optical emission response of CdTe quantum dot/polymer nanocomposite under <span class="hlt">shock</span> <span class="hlt">compression</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Xiao, Pan; Kang, Zhitao; Bansihev, Alexandr A.; Breidenich, Jennifer; Scripka, David A.; Christensen, James M.; Summers, Christopher J.; Dlott, Dana D.; Thadhani, Naresh N.; Zhou, Min</p> <p>2016-01-01</p> <p>Laser-driven <span class="hlt">shock</span> <span class="hlt">compression</span> experiments and corresponding finite element method simulations are carried out to investigate the blueshift in the optical emission spectra under continuous laser excitation of a dilute composite consisting of 0.15% CdTe quantum dots by weight embedded in polyvinyl alcohol polymer. This material is a potential candidate for use as internal stress sensors. The analyses focus on the time histories of the wavelength blue-shift for <span class="hlt">shock</span> loading with pressures up to 7.3 GPa. The combined measurements and calculations allow a relation between the wavelength blueshift and pressure for the loading conditions to be extracted. It is found that the blueshift first increases with pressure to a maximum and subsequently decreases with pressure. This trend is different from the monotonic increase of blueshift with pressure observed under conditions of quasistatic hydrostatic <span class="hlt">compression</span>. Additionally, the blueshift in the <span class="hlt">shock</span> experiments is much smaller than that in hydrostatic experiments at the same pressure levels. The differences in responses are attributed to the different stress states achieved in the <span class="hlt">shock</span> and hydrostatic experiments and the time dependence of the mechanical response of the polymer in the composite. The findings offer a potential guide for the design and development of materials for internal stress sensors for <span class="hlt">shock</span> conditions.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_4");'>4</a></li> <li><a href="#" onclick='return showDiv("page_5");'>5</a></li> <li class="active"><span>6</span></li> <li><a href="#" onclick='return showDiv("page_7");'>7</a></li> <li><a href="#" onclick='return showDiv("page_8");'>8</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_6 --> <div id="page_7" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_5");'>5</a></li> <li><a href="#" onclick='return showDiv("page_6");'>6</a></li> <li class="active"><span>7</span></li> <li><a href="#" onclick='return showDiv("page_8");'>8</a></li> <li><a href="#" onclick='return showDiv("page_9");'>9</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="121"> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2009JAP...106d3519D','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2009JAP...106d3519D"><span>Hugoniot temperatures and melting of tantalum under <span class="hlt">shock</span> <span class="hlt">compression</span> determined by optical pyrometry</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Dai, Chengda; Hu, Jianbo; Tan, Hua</p> <p>2009-08-01</p> <p>LiF single crystal was used as transparent window (anvil) to tamp the <span class="hlt">shock</span>-induced free surface expansion of Ta specimen, and the Ta/LiF interface temperature was measured under <span class="hlt">shock</span> <span class="hlt">compression</span> using optical pyrometry technique. The <span class="hlt">shock</span> temperatures and/or melting temperatures of Ta up to ˜400 GPa were extracted from the observed interface temperatures based on the Tan-Ahrens' model for one-dimensional heat conduction across metal/window ideal interface in which initial melting and subsequent solidification were considered under <span class="hlt">shock</span> loading. The obtained data within the experimental uncertainties are consistent with the results from high-pressure sound velocity measurements. The temperature of the partial melting on Ta Hugoniot is estimated to be ˜9700 K at 300 GPa, supported by available results from theoretical calculations.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017APS..DFDA30006S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017APS..DFDA30006S"><span>A volume-filtered formulation to capture particle-<span class="hlt">shock</span> interactions in multiphase <span class="hlt">compressible</span> flows</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Shallcross, Gregory; Capecelatro, Jesse</p> <p>2017-11-01</p> <p><span class="hlt">Compressible</span> particle-laden flows are common in engineering systems. Applications include but are not limited to water injection in high-speed jet flows for noise suppression, rocket-plume surface interactions during planetary landing, and explosions during coal mining operations. Numerically, it is challenging to capture these interactions due to the wide range of length and time scales. Additionally, there are many forms of the multiphase <span class="hlt">compressible</span> flow equations with volume fraction effects, some of which are conflicting in nature. The purpose of this presentation is to develop the capability to accurately capture particle-<span class="hlt">shock</span> interactions in systems with a large number of particles from dense to dilute regimes. A thorough derivation of the volume filtered equations is presented. The volume filtered equations are then implemented in a high-order, energy-stable Eulerian-Lagrangian framework. We show this framework is capable of decoupling the fluid mesh from the particle size, enabling arbitrary particle size distributions in the presence of <span class="hlt">shocks</span>. The proposed method is then assessed against particle-laden <span class="hlt">shock</span> tube data. Quantities of interest include fluid-phase pressure profiles and particle spreading rates. The effect of collisions in 2D and 3D are also evaluated.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1342519-shock-compression-release-axis-magnesium-single-crystals-anisotropy-time-dependent-inelastic-response','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1342519-shock-compression-release-axis-magnesium-single-crystals-anisotropy-time-dependent-inelastic-response"><span><span class="hlt">Shock</span> <span class="hlt">compression</span> and release of a-axis magnesium single crystals: Anisotropy and time dependent inelastic response</span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>Renganathan, P.; Winey, J. M.; Gupta, Y. M.</p> <p>2017-01-19</p> <p>Here, to gain insight into inelastic deformation mechanisms for <span class="hlt">shocked</span> hexagonal close-packed (hcp) metals, particularly the role of crystal anisotropy, magnesium (Mg) single crystals were subjected to <span class="hlt">shock</span> <span class="hlt">compression</span> and release along the a-axis to 3.0 and 4.8 GPa elastic impact stresses. Wave profiles measured at several thicknesses, using laser interferometry, show a sharply peaked elastic wave followed by the plastic wave. Additionally, a smooth and featureless release wave is observed following peak <span class="hlt">compression</span>. When compared to wave profiles measured previously for c-axis Mg, the elastic wave amplitudes for a-axis Mg are lower for the same propagation distance, and less attenuation of elastic wave amplitude is observed for a given peak stress. The featureless release wave for a-axis Mg is in marked contrast to the structured features observed for c-axis unloading. Numerical simulations, using a time-dependent anisotropic modeling framework, showed that the wave profiles calculated using prismatic slip or (10more » $$\\bar{1}$$2) twinning, individually, do not match the measured <span class="hlt">compression</span> profiles for a-axis Mg. However, a combination of slip and twinning provides a good overall match to the measured <span class="hlt">compression</span> profiles. In contrast to <span class="hlt">compression</span>,prismatic slip alone provides a reasonable match to the measured release wave profiles; (10$$\\bar{1}$$2) twinning due to its uni-directionality is not activated during release. The experimental results and wave profile simulations for a-axis Mg presented here are quite different from the previously published c-axis results, demonstrating the important role of crystal anisotropy on the time-dependent inelastic deformation of Mg single crystals under <span class="hlt">shock</span> <span class="hlt">compression</span> and release.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/1342519','SCIGOV-STC'); return false;" href="https://www.osti.gov/servlets/purl/1342519"><span><span class="hlt">Shock</span> <span class="hlt">compression</span> and release of a-axis magnesium single crystals: Anisotropy and time dependent inelastic response</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Renganathan, P.; Winey, J. M.; Gupta, Y. M.</p> <p></p> <p>Here, to gain insight into inelastic deformation mechanisms for <span class="hlt">shocked</span> hexagonal close-packed (hcp) metals, particularly the role of crystal anisotropy, magnesium (Mg) single crystals were subjected to <span class="hlt">shock</span> <span class="hlt">compression</span> and release along the a-axis to 3.0 and 4.8 GPa elastic impact stresses. Wave profiles measured at several thicknesses, using laser interferometry, show a sharply peaked elastic wave followed by the plastic wave. Additionally, a smooth and featureless release wave is observed following peak <span class="hlt">compression</span>. When compared to wave profiles measured previously for c-axis Mg, the elastic wave amplitudes for a-axis Mg are lower for the same propagation distance, and less attenuation of elastic wave amplitude is observed for a given peak stress. The featureless release wave for a-axis Mg is in marked contrast to the structured features observed for c-axis unloading. Numerical simulations, using a time-dependent anisotropic modeling framework, showed that the wave profiles calculated using prismatic slip or (10more » $$\\bar{1}$$2) twinning, individually, do not match the measured <span class="hlt">compression</span> profiles for a-axis Mg. However, a combination of slip and twinning provides a good overall match to the measured <span class="hlt">compression</span> profiles. In contrast to <span class="hlt">compression</span>,prismatic slip alone provides a reasonable match to the measured release wave profiles; (10$$\\bar{1}$$2) twinning due to its uni-directionality is not activated during release. The experimental results and wave profile simulations for a-axis Mg presented here are quite different from the previously published c-axis results, demonstrating the important role of crystal anisotropy on the time-dependent inelastic deformation of Mg single crystals under <span class="hlt">shock</span> <span class="hlt">compression</span> and release.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/29714184','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/29714184"><span>Simulations of X-ray diffraction of <span class="hlt">shock-compressed</span> single-crystal tantalum with synchrotron undulator sources.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Tang, M X; Zhang, Y Y; E, J C; Luo, S N</p> <p>2018-05-01</p> <p>Polychromatic synchrotron undulator X-ray sources are useful for ultrafast single-crystal diffraction under <span class="hlt">shock</span> <span class="hlt">compression</span>. Here, simulations of X-ray diffraction of <span class="hlt">shock-compressed</span> single-crystal tantalum with realistic undulator sources are reported, based on large-scale molecular dynamics simulations. Purely elastic deformation, elastic-plastic two-wave structure, and severe plastic deformation under different impact velocities are explored, as well as an edge release case. Transmission-mode diffraction simulations consider crystallographic orientation, loading direction, incident beam direction, X-ray spectrum bandwidth and realistic detector size. Diffraction patterns and reciprocal space nodes are obtained from atomic configurations for different loading (elastic and plastic) and detection conditions, and interpretation of the diffraction patterns is discussed.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2001APS..SHK.E1002F','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2001APS..SHK.E1002F"><span>The History of the APS <span class="hlt">Shock</span> <span class="hlt">Compression</span> of Condensed Matter Topical Group</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Forbes, Jerry W.</p> <p>2001-06-01</p> <p>To provide broader scientific recognition and to advance the science of <span class="hlt">shock-compressed</span> condensed matter, a group of APS members worked within the Society to make this technical field an active part of APS. Individual papers were given at APS meetings starting in the 1950’s and then later whole sessions were organized starting at the 1967 Pasadena meeting. Topical conferences began in 1979 in Pullman, WA where George Duvall and Dennis Hayes were co-chairs. Most all early topical conferences were sanctioned by the APS while those held after 1985 were official APS meetings. In 1984, after consulting with a number of people in the <span class="hlt">shock</span> wave field, Robert Graham circulated a petition to form an APS topical group. He obtained signatures from a balanced cross-section of the community. William Havens, the executive secretary of APS, informed Robert Graham by letter on November 28, 1984 that the APS Council had officially accepted the formation of this topical group at its October 28, 1984 meeting. The first election occurred July 23, 1985 where Robert Graham was elected chairman, William Nellis vice-chairman, and Jerry Forbes secretary/treasurer. The topical group remains viable today by holding a topical conference in odd numbered years and <span class="hlt">shock</span> wave sessions at APS general meetings in even numbered years A major benefit of being an official unit of APS is the allotment of APS fellows every year. The APS <span class="hlt">shock</span> <span class="hlt">compression</span> award established in 1987, has also provided broad recognition of many major scientific accomplishments in this field.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19750061541&hterms=bleeding&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D30%26Ntt%3Dbleeding','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19750061541&hterms=bleeding&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D30%26Ntt%3Dbleeding"><span>Control of <span class="hlt">shock</span>-wave boundary-layer interactions by bleed in supersonic mixed <span class="hlt">compression</span> inlets</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Fukuda, M. K.; Reshotko, E.; Hingst, W. R.</p> <p>1975-01-01</p> <p>An experimental investigation has been conducted to determine the effect of bleed region geometry and bleed rate on <span class="hlt">shock</span> wave-boundary layer interactions in an axisymmetric, mixed-<span class="hlt">compression</span> inlet at a Mach number of 2.5. The full realizable reduction in transformed form factor is obtained by bleeding off about half the incident boundary layer mass flow. Bleeding upstream or downstream of the <span class="hlt">shock</span>-induced pressure rise is preferable to bleeding across the <span class="hlt">shock</span>-induced pressure rise. Slanted holes are more effective than normal holes. Two different bleed hole sizes were tested without detectable difference in performance.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19770011443','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19770011443"><span>Diffraction of a <span class="hlt">shock</span> wave by a <span class="hlt">compression</span> corner; regular and single Mach reflection</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Vijayashankar, V. S.; Kutler, P.; Anderson, D.</p> <p>1976-01-01</p> <p>The two dimensional, time dependent Euler equations which govern the flow field resulting from the injection of a planar <span class="hlt">shock</span> with a <span class="hlt">compression</span> corner are solved with initial conditions that result in either regular reflection or single Mach reflection of the incident planar <span class="hlt">shock</span>. The Euler equations which are hyperbolic are transformed to include the self similarity of the problem. A normalization procedure is employed to align the reflected <span class="hlt">shock</span> and the Mach stem as computational boundaries to implement the <span class="hlt">shock</span> fitting procedure. A special floating fitting scheme is developed in conjunction with the method of characteristics to fit the slip surface. The reflected <span class="hlt">shock</span>, the Mach stem, and the slip surface are all treated as harp discontinuities, thus, resulting in a more accurate description of the inviscid flow field. The resulting numerical solutions are compared with available experimental data and existing first-order, <span class="hlt">shock</span>-capturing numerical solutions.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2013APS..DPPCO6001M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2013APS..DPPCO6001M"><span>Molecular systems under <span class="hlt">shock</span> <span class="hlt">compression</span> into the dense plasma regime: carbon dioxide and hydrocarbon polymers</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Mattsson, Thomas R.; Cochrane, Kyle R.; Root, Seth; Carpenter, John H.</p> <p>2013-10-01</p> <p>Density Functional Theory (DFT) has proven remarkably accurate in predicting properties of matter under <span class="hlt">shock</span> <span class="hlt">compression</span> into the dense plasma regime. Materials where chemistry plays a role are of interest for many applications, including planetary science and inertial confinement fusion (ICF). As examples of systems where chemical reactions are important, and demonstration of the high fidelity possible for these both structurally and chemically complex systems, we will discuss <span class="hlt">shock</span>- and re-<span class="hlt">shock</span> of liquid carbon dioxide (CO2) in the range 100 to 800 GPa and <span class="hlt">shock</span> <span class="hlt">compression</span> of hydrocarbon polymers, including GDP (glow discharge polymer) which is used as an ablator in laser ICF experiments. Experimental results from Sandia's Z machine validate the DFT simulations at extreme conditions and the combination of experiment and DFT provide reliable data for evaluating existing and constructing future wide-range equations of state models for molecular compounds. Sandia National Laboratories is a multi-program laboratory managed and operated by Sandia Corporation, a wholly owned subsidiary of Lockheed Martin Company, for the U.S. Department of Energy's National Nuclear Security Administration under contract DE-AC04-94AL85000.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4841653','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4841653"><span>On the formation of Friedlander waves in a <span class="hlt">compressed</span>-gas-driven <span class="hlt">shock</span> tube</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Tasissa, Abiy F.; Hautefeuille, Martin; Fitek, John H.; Radovitzky, Raúl A.</p> <p>2016-01-01</p> <p><span class="hlt">Compressed</span>-gas-driven <span class="hlt">shock</span> tubes have become popular as a laboratory-scale replacement for field blast tests. The well-known initial structure of the Riemann problem eventually evolves into a <span class="hlt">shock</span> structure thought to resemble a Friedlander wave, although this remains to be demonstrated theoretically. In this paper, we develop a semi-analytical model to predict the key characteristics of pseudo blast waves forming in a <span class="hlt">shock</span> tube: location where the wave first forms, peak over-pressure, decay time and impulse. The approach is based on combining the solutions of the two different types of wave interactions that arise in the <span class="hlt">shock</span> tube after the family of rarefaction waves in the Riemann solution interacts with the closed end of the tube. The results of the analytical model are verified against numerical simulations obtained with a finite volume method. The model furnishes a rational approach to relate <span class="hlt">shock</span> tube parameters to desired blast wave characteristics, and thus constitutes a useful tool for the design of <span class="hlt">shock</span> tubes for blast testing. PMID:27118888</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/17907198','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/17907198"><span>Focal gene misexpression in zebrafish embryos induced by local heat <span class="hlt">shock</span> using a modified soldering <span class="hlt">iron</span>.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Hardy, Melissa E; Ross, Louis V; Chien, Chi-Bin</p> <p>2007-11-01</p> <p>Misexpression of genes in a temporally and spatially controlled fashion is an important tool for assessing gene function during development. Because few tissue-specific promoters have been identified in zebrafish, inducible systems such as the Cre/LoxP and Tet repressor systems are of limited utility. Here we describe a new method of misexpression: local heat <span class="hlt">shock</span> using a modified soldering <span class="hlt">iron</span>. Zebrafish carrying transgenes under the control of a heat <span class="hlt">shock</span> promoter (hsp70) are focally heated with the soldering <span class="hlt">iron</span> to induce gene expression in a small area of the embryo. We have validated this method in three stable transgenic lines and at three developmental timepoints. Local heat <span class="hlt">shock</span> is a fast, easy, and inexpensive method for gene misexpression. Copyright 2007 Wiley-Liss, Inc.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2013JAP...113v3513F','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2013JAP...113v3513F"><span>Predicting the <span class="hlt">shock</span> <span class="hlt">compression</span> response of heterogeneous powder mixtures</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Fredenburg, D. A.; Thadhani, N. N.</p> <p>2013-06-01</p> <p>A model framework for predicting the dynamic <span class="hlt">shock-compression</span> response of heterogeneous powder mixtures using readily obtained measurements from quasi-static tests is presented. Low-strain-rate <span class="hlt">compression</span> data are first analyzed to determine the region of the bulk response over which particle rearrangement does not contribute to compaction. This region is then fit to determine the densification modulus of the mixture, σD, an newly defined parameter describing the resistance of the mixture to yielding. The measured densification modulus, reflective of the diverse yielding phenomena that occur at the meso-scale, is implemented into a rate-independent formulation of the P-α model, which is combined with an isobaric equation of state to predict the low and high stress dynamic <span class="hlt">compression</span> response of heterogeneous powder mixtures. The framework is applied to two metal + metal-oxide (thermite) powder mixtures, and good agreement between the model and experiment is obtained for all mixtures at stresses near and above those required to reach full density. At lower stresses, rate-dependencies of the constituents, and specifically those of the matrix constituent, determine the ability of the model to predict the measured response in the incomplete compaction regime.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/1991JPSJ...60.4119Y','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/1991JPSJ...60.4119Y"><span>Statistical modeling of <span class="hlt">compressible</span> turbulence - <span class="hlt">Shock</span>-wave/turbulence interactions and buoyancy effects</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Yoshizawa, Akira</p> <p>1991-12-01</p> <p>A mass-weighted mean <span class="hlt">compressible</span> turbulence model is presented with the aid of the results from a two-scale DIA. This model aims at dealing with two typical aspects in <span class="hlt">compressible</span> flows: the interaction of a <span class="hlt">shock</span> wave with turbulence in high-speed flows and strong buoyancy effects in thermally-driven flows as in stellar convection and conflagration. The former is taken into account through the effect of turbulent dilatation that is related to the density fluctuation and leads to the enhanced kinetic-energy dissipation. The latter is incorporated through the interaction between the gravitational and density-fluctuation effects.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/22597040-shock-compression-response-highly-reactive-ni+al-multilayered-thin-foils','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/22597040-shock-compression-response-highly-reactive-ni+al-multilayered-thin-foils"><span><span class="hlt">Shock</span> <span class="hlt">compression</span> response of highly reactive Ni + Al multilayered thin foils</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Kelly, Sean C.; Thadhani, Naresh N., E-mail: naresh.thadhani@mse.gatech.edu</p> <p>2016-03-07</p> <p>The <span class="hlt">shock-compression</span> response of Ni + Al multilayered thin foils is investigated using laser-accelerated thin-foil plate-impact experiments over the pressure range of 2 to 11 GPa. The foils contain alternating Ni and Al layers (parallel but not flat) of nominally 50 nm bilayer spacing. The goal is to determine the equation of state and <span class="hlt">shock</span>-induced reactivity of these highly reactive fully dense thin-foil materials. The laser-accelerated thin-foil impact set-up involved combined use of photon-doppler-velocimetry to monitor the acceleration and impact velocity of an aluminum flyer, and VISAR interferometry was used to monitor the back free-surface velocity of the impacted Ni + Al multilayered target. The <span class="hlt">shock</span>-compressionmore » response of the Ni + Al target foils was determined using experimentally measured parameters and impedance matching approach, with error bars identified considering systematic and experimental errors. Meso-scale CTH <span class="hlt">shock</span> simulations were performed using real imported microstructures of the cross-sections of the multilayered Ni + Al foils to compute the Hugoniot response (assuming no reaction) for correlation with their experimentally determined equation of state. It was observed that at particle velocities below ∼150 m/s, the experimentally determined equation of state trend matches the CTH-predicted inert response and is consistent with the observed unreacted state of the recovered Ni + Al target foils from this velocity regime. At higher particle velocities, the experimentally determined equation of state deviates from the CTH-predicted inert response. A complete and self-sustained reaction is also seen in targets recovered from experiments performed at these higher particle velocities. The deviation in the measured equation of state, to higher <span class="hlt">shock</span> speeds and expanded volumes, combined with the observation of complete reaction in the recovered multilayered foils, confirmed via microstructure</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017AIPC.1793j0030K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017AIPC.1793j0030K"><span>Evolutions of elastic-plastic <span class="hlt">shock</span> <span class="hlt">compression</span> waves in different materials</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Kanel, G. I.; Zaretsky, E. B.; Razorenov, S. V.; Savinykh, A. S.; Garkushin, G. V.</p> <p>2017-01-01</p> <p>In the paper, we discuss such unexpected features in the wave evolution in solids as a departure from self-similar development of the wave process which is accompanied with apparent sub-sonic wave propagation, changes of shape of elastic precursor wave as a result of variations in the material structure and the temperature, unexpected peculiarities of reflection of elastic-plastic waves from free surface, effects of internal friction at <span class="hlt">shock</span> <span class="hlt">compression</span> of glasses and some other effects.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/1435819-simulations-ray-diffraction-shock-compressed-single-crystal-tantalum-synchrotron-undulator-sources','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/1435819-simulations-ray-diffraction-shock-compressed-single-crystal-tantalum-synchrotron-undulator-sources"><span>Simulations of X-ray diffraction of <span class="hlt">shock-compressed</span> single-crystal tantalum with synchrotron undulator sources</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Tang, M. X.; Zhang, Y. Y.; E, J. C.</p> <p></p> <p>Polychromatic synchrotron undulator X-ray sources are useful for ultrafast single-crystal diffraction under <span class="hlt">shock</span> <span class="hlt">compression</span>. Here, simulations of X-ray diffraction of <span class="hlt">shock-compressed</span> single-crystal tantalum with realistic undulator sources are reported, based on large-scale molecular dynamics simulations. Purely elastic deformation, elastic–plastic two-wave structure, and severe plastic deformation under different impact velocities are explored, as well as an edge release case. Transmission-mode diffraction simulations consider crystallographic orientation, loading direction, incident beam direction, X-ray spectrum bandwidth and realistic detector size. Diffraction patterns and reciprocal space nodes are obtained from atomic configurations for different loading (elastic and plastic) and detection conditions, and interpretation of themore » diffraction patterns is discussed.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://www.dtic.mil/docs/citations/ADA608086','DTIC-ST'); return false;" href="http://www.dtic.mil/docs/citations/ADA608086"><span>Finite Strain Analysis of <span class="hlt">Shock</span> <span class="hlt">Compression</span> of Brittle Solids Applied to Titanium Diboride</span></a></p> <p><a target="_blank" href="http://www.dtic.mil/">DTIC Science & Technology</a></p> <p></p> <p>2014-07-01</p> <p>dislocation motion [18,19] may take place at high pressures. Multiple investigations have discovered that tita - nium diboride demonstrates a rather unique...mean stress under <span class="hlt">shock</span> <span class="hlt">compression</span>. It has been suggested [5] that pore collapse may be an important source of inelasticity in tita - nium diboride</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/10190963','SCIGOV-STC'); return false;" href="https://www.osti.gov/servlets/purl/10190963"><span>(BARS) -- Bibliographic Retrieval System Sandia <span class="hlt">Shock</span> <span class="hlt">Compression</span> (SSC) database <span class="hlt">Shock</span> Physics Index (SPHINX) database. Volume 1: UNIX version query guide customized application for INGRES</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Herrmann, W.; von Laven, G.M.; Parker, T.</p> <p>1993-09-01</p> <p>The Bibliographic Retrieval System (BARS) is a data base management system specially designed to retrieve bibliographic references. Two databases are available, (i) the Sandia <span class="hlt">Shock</span> <span class="hlt">Compression</span> (SSC) database which contains over 5700 references to the literature related to stress waves in solids and their applications, and (ii) the <span class="hlt">Shock</span> Physics Index (SPHINX) which includes over 8000 further references to stress waves in solids, material properties at intermediate and low rates, ballistic and hypervelocity impact, and explosive or <span class="hlt">shock</span> fabrication methods. There is some overlap in the information in the two data bases.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017PhRvE..96a3204Z','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017PhRvE..96a3204Z"><span>First-principles equation of state and <span class="hlt">shock</span> <span class="hlt">compression</span> predictions of warm dense hydrocarbons</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Zhang, Shuai; Driver, Kevin P.; Soubiran, François; Militzer, Burkhard</p> <p>2017-07-01</p> <p>We use path integral Monte Carlo and density functional molecular dynamics to construct a coherent set of equations of state (EOS) for a series of hydrocarbon materials with various C:H ratios (2:1, 1:1, 2:3, 1:2, and 1:4) over the range of 0.07 -22.4 g cm-3 and 6.7 ×103-1.29 ×108K . The <span class="hlt">shock</span> Hugoniot curve derived for each material displays a single <span class="hlt">compression</span> maximum corresponding to K -shell ionization. For C:H = 1:1, the <span class="hlt">compression</span> maximum occurs at 4.7-fold of the initial density and we show radiation effects significantly increase the <span class="hlt">shock</span> <span class="hlt">compression</span> ratio above 2 Gbar, surpassing relativistic effects. The single-peaked structure of the Hugoniot curves contrasts with previous work on higher-Z plasmas, which exhibit a two-peak structure corresponding to both K - and L -shell ionization. Analysis of the electronic density of states reveals that the change in Hugoniot structure is due to merging of the L -shell eigenstates in carbon, while they remain distinct for higher-Z elements. Finally, we show that the isobaric-isothermal linear mixing rule for carbon and hydrogen EOS is a reasonable approximation with errors better than 1% for stellar-core conditions.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2012AIPC.1426.1573B','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2012AIPC.1426.1573B"><span>Nitro stretch probing of a single molecular layer to monitor <span class="hlt">shock</span> <span class="hlt">compression</span> with picosecond time resolution</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Berg, Christopher; Lagutchev, Alexei; Fu, Yuanxi; Dlott, Dana</p> <p>2012-03-01</p> <p>Ultrafast <span class="hlt">shock</span> <span class="hlt">compression</span> vibrational spectroscopy experiments with molecular monolayers provide atomic-scale time and space resolution, which enables critical testing of reactive molecular simulations. Since the origination of this project, we have greatly improved the ability to detect <span class="hlt">shocked</span> monolayers by nonlinear coherent vibrational spectroscopy with nonresonant suppression. In this study, we show new results on a nitroaromatic monolayer, where the nitro symmetric stretch is probed. A small frequency blue-shift under <span class="hlt">shock</span> conditions compared to measurements with static high pressure shows the <span class="hlt">shock</span> is ~1 GPa. The ability to flash-preheat the monolayer by several hundred K is demonstrated. In order to observe <span class="hlt">shock</span> monolayer chemistry in real time, along with pre-heating, the <span class="hlt">shock</span> pressure needs to be increased and methods to do so are described.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_5");'>5</a></li> <li><a href="#" onclick='return showDiv("page_6");'>6</a></li> <li class="active"><span>7</span></li> <li><a href="#" onclick='return showDiv("page_8");'>8</a></li> <li><a href="#" onclick='return showDiv("page_9");'>9</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_7 --> <div id="page_8" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_6");'>6</a></li> <li><a href="#" onclick='return showDiv("page_7");'>7</a></li> <li class="active"><span>8</span></li> <li><a href="#" onclick='return showDiv("page_9");'>9</a></li> <li><a href="#" onclick='return showDiv("page_10");'>10</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="141"> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017APS..MAR.P2001M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017APS..MAR.P2001M"><span>Ultrafast studies of <span class="hlt">shock</span>-induced melting and phase transitions at LCLS</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>McMahon, Malcolm</p> <p></p> <p>The study of <span class="hlt">shock</span>-induced phase transitions, which is vital to the understanding of material response to rapid pressure changes, dates back to the 1950s, when Bankcroft et al reported a transition in <span class="hlt">iron</span>. Since then, many transitions have been reported in a wide range of materials, but, due to the lack of sufficiently bright x-ray sources, the structural details of these new phases has been notably lacking. While the development of nanosecond in situ x-ray diffraction has meant that lattice-level studies of such phenomena have become possible, including studies of the phase transition reported 60 years ago in <span class="hlt">iron</span>, the quality of the diffraction data from such studies is noticeably poorer than that obtained from statically-<span class="hlt">compressed</span> samples on synchrotrons. The advent of x-ray free electron lasers (XFELs), such as the LCLS, has resulted in an unprecedented improvement in the quality of diffraction data that can be obtained from <span class="hlt">shock-compressed</span> matter. Here I describe the results from three recent experiment at the LCLS that looked at the solid-solid and solid-liquid phase transitions in Sb, Bi and Sc using single 50 fs x-ray exposures. The results provide new insight into the structural changes and melting induced by <span class="hlt">shock</span> <span class="hlt">compression</span>. This work is supported by EPSRC under Grant No. EP/J017051/1. Use of the LCLS, SLAC National Accelerator Laboratory, is supported by the U.S. Department of Energy, Office of Science, Office of Basic Energy Sciences under Contract No. DE-AC02-76SF00515.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016APS..MARE21011A','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016APS..MARE21011A"><span>Reactive decomposition of low density PMDI foam subject to <span class="hlt">shock</span> <span class="hlt">compression</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Alexander, Scott; Reinhart, William; Brundage, Aaron; Peterson, David</p> <p></p> <p>Low density polymethylene diisocyanate (PMDI) foam with a density of 5.4 pounds per cubic foot (0.087 g/cc) was tested to determine the equation of state properties under <span class="hlt">shock</span> <span class="hlt">compression</span> over the pressure range of 0.58 - 3.4 GPa. This pressure range encompasses a region approximately 1.0-1.2 GPa within which the foam undergoes reactive decomposition resulting in significant volume expansion of approximately three times the volume prior to reaction. This volume expansion has a significant effect on the high pressure equation of state. Previous work on similar foam was conducted only up to the region where volume expansion occurs and extrapolation of that data to higher pressure results in a significant error. It is now clear that new models are required to account for the reactive decomposition of this class of foam. The results of plate impact tests will be presented and discussed including details of the unique challenges associated with <span class="hlt">shock</span> <span class="hlt">compression</span> of low density foams. Sandia National Labs is a multi-program lab managed and operated by Sandia Corporation, a wholly owned subsidiary of Lockheed Martin Corp., for the U.S. Dept. of Energy's National Nuclear Security Administration under Contract DE-AC04-94AL85000.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/25177717','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/25177717"><span>Estimation of the <span class="hlt">iron</span> loss in deep-sea permanent magnet motors considering seawater <span class="hlt">compressive</span> stress.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Xu, Yongxiang; Wei, Yanyu; Zou, Jibin; Li, Jianjun; Qi, Wenjuan; Li, Yong</p> <p>2014-01-01</p> <p>Deep-sea permanent magnet motor equipped with fluid compensated pressure-tolerant system is <span class="hlt">compressed</span> by the high pressure fluid both outside and inside. The induced stress distribution in stator core is significantly different from that in land type motor. Its effect on the magnetic properties of stator core is important for deep-sea motor designers but seldom reported. In this paper, the stress distribution in stator core, regarding the seawater <span class="hlt">compressive</span> stress, is calculated by 2D finite element method (FEM). The effect of <span class="hlt">compressive</span> stress on magnetic properties of electrical steel sheet, that is, permeability, BH curves, and BW curves, is also measured. Then, based on the measured magnetic properties and calculated stress distribution, the stator <span class="hlt">iron</span> loss is estimated by stress-electromagnetics-coupling FEM. At last the estimation is verified by experiment. Both the calculated and measured results show that stator <span class="hlt">iron</span> loss increases obviously with the seawater <span class="hlt">compressive</span> stress.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4142183','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4142183"><span>Estimation of the <span class="hlt">Iron</span> Loss in Deep-Sea Permanent Magnet Motors considering Seawater <span class="hlt">Compressive</span> Stress</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Wei, Yanyu; Zou, Jibin; Li, Jianjun; Qi, Wenjuan; Li, Yong</p> <p>2014-01-01</p> <p>Deep-sea permanent magnet motor equipped with fluid compensated pressure-tolerant system is <span class="hlt">compressed</span> by the high pressure fluid both outside and inside. The induced stress distribution in stator core is significantly different from that in land type motor. Its effect on the magnetic properties of stator core is important for deep-sea motor designers but seldom reported. In this paper, the stress distribution in stator core, regarding the seawater <span class="hlt">compressive</span> stress, is calculated by 2D finite element method (FEM). The effect of <span class="hlt">compressive</span> stress on magnetic properties of electrical steel sheet, that is, permeability, BH curves, and BW curves, is also measured. Then, based on the measured magnetic properties and calculated stress distribution, the stator <span class="hlt">iron</span> loss is estimated by stress-electromagnetics-coupling FEM. At last the estimation is verified by experiment. Both the calculated and measured results show that stator <span class="hlt">iron</span> loss increases obviously with the seawater <span class="hlt">compressive</span> stress. PMID:25177717</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1418960-first-principles-equation-state-shock-compression-predictions-warm-dense-hydrocarbons','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1418960-first-principles-equation-state-shock-compression-predictions-warm-dense-hydrocarbons"><span>First-principles equation of state and <span class="hlt">shock</span> <span class="hlt">compression</span> predictions of warm dense hydrocarbons</span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>Zhang, Shuai; Driver, Kevin P.; Soubiran, Francois; ...</p> <p>2017-07-10</p> <p>We use path integral Monte Carlo and density functional molecular dynamics to construct a coherent set of equations of state (EOS) for a series of hydrocarbon materials with various C:H ratios (2:1, 1:1, 2:3, 1:2, and 1:4) over the range of 0.07–22.4gcm –3 and 6.7 × 10 3 – 1.29 × 10 8K. The <span class="hlt">shock</span> Hugoniot curve derived for each material displays a single <span class="hlt">compression</span> maximum corresponding to K-shell ionization. For C:H = 1:1, the <span class="hlt">compression</span> maximum occurs at 4.7-fold of the initial density and we show radiation effects significantly increase the <span class="hlt">shock</span> <span class="hlt">compression</span> ratio above 2 Gbar, surpassing relativisticmore » effects. The single-peaked structure of the Hugoniot curves contrasts with previous work on higher-Z plasmas, which exhibit a two-peak structure corresponding to both K- and L-shell ionization. Analysis of the electronic density of states reveals that the change in Hugoniot structure is due to merging of the L-shell eigenstates in carbon, while they remain distinct for higher-Z elements. Lastly, we show that the isobaric-isothermal linear mixing rule for carbon and hydrogen EOS is a reasonable approximation with errors better than 1% for stellar-core conditions.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2011APS..SHK.J4002A','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2011APS..SHK.J4002A"><span><span class="hlt">Shock</span> <span class="hlt">compression</span> of preheated silicate liquids: 30 years of progress</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Asimow, Paul</p> <p>2011-06-01</p> <p>Tom Ahrens and his students pioneered, beginning around 1981, the technique of determining silicate liquid equations of state for geophysical applications using <span class="hlt">shock</span> <span class="hlt">compression</span> of pre-heated, encapsulated samples. In the last decade, we have ported this technique to the Caltech two-stage light gas gun and extended several pre-heated liquid Hugoniots to over 125 GPa. We now have enough compositions studied to perform several tests of the theory of linear mixing or, assuming linear mixing, to describe any liquid in the five-component CaO-MgO-FeO-Al2O3-SiO2 system. This data allows us to identify liquid compositions likely to be negatively or neutrally buoyant in the lower mantle and to form a preliminary description of the dynamics of partial melting of solid lower mantle or initial crystallization of a deep mantle magma ocean. The most robust and surprising feature of all studied liquids, which places very strong constraints on microscopic models for silicate liquid <span class="hlt">compression</span> behavior, is anomalous increase of the Grüneisen parameter upon <span class="hlt">compression</span>, with remarkably consistent q = dln γ/dlnV = -1.75 +/- 0.25. Thanks to long-term support by the National Science Foundation.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19750023958','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19750023958"><span>Control of <span class="hlt">shock</span> wave-boundary layer interactions by bleed in supersonic mixed <span class="hlt">compression</span> inlets</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Fukuda, M. K.; Hingst, W. G.; Reshotko, E.</p> <p>1975-01-01</p> <p>An experimental investigation was conducted to determine the effect of bleed on a <span class="hlt">shock</span> wave-boundary layer interaction in an axisymmetric mixed-<span class="hlt">compression</span> supersonic inlet. The inlet was designed for a free-stream Mach number of 2.50 with 60-percent supersonic internal area contraction. The experiment was conducted in the NASA Lewis Research Center 10-Foot Supersonic Wind Tunnel. The effects of bleed amount and bleed geometry on the boundary layer after a <span class="hlt">shock</span> wave-boundary layer interaction were studied. The effect of bleed on the transformed form factor is such that the full realizable reduction is obtained by bleeding of a mass flow equal to about one-half of the incident boundary layer mass flow. More bleeding does not yield further reduction. Bleeding upstream or downstream of the <span class="hlt">shock</span>-induced pressure rise is preferable to bleeding across the <span class="hlt">shock</span>-induced pressure rise.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017APS..SHK.B2002Z','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017APS..SHK.B2002Z"><span>Ultrafast <span class="hlt">Shock</span> <span class="hlt">Compression</span> Hugoniot Data of beta-CL-20 and TATB Thin Films</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Zaug, Joseph; Armstrong, Michael; Grivickas, Paulius; Tappan, Alexander; Kohl, Ian; Rodriguez, Mark; Knepper, Robert; Crowhurst, Jonathan; Stavrou, Elissaios; Bastea, Sorin</p> <p>2017-06-01</p> <p>The <span class="hlt">shock</span> induced initiation threshold of two energetic materials, CL-20 and TATB are remarkably different; CL-20 is a relatively <span class="hlt">shock</span> sensitive energetic material and TATB is considered an insensitive high explosive (IHE). Here we report ultrafast laser-based shockwave hydrodynamic data on the 100 ps timescale with 10 ps time resolution to further develop density dependent unreacted <span class="hlt">shock</span> Hugoniot equations of state (UEOS) and to elucidate ultrafast timescale <span class="hlt">shock</span> initiation processes for these two vastly different HEs. Thin film samples were made by vacuum thermal evaporation of the explosive on a deposited aluminum ablator layer. The deposited explosives were characterized by scanning electron microscopy, surface profilometry, and x-ray diffraction. Our preliminary UEOS results (up range of 1.3 - 1.8 km/s) from <span class="hlt">shock</span> <span class="hlt">compressed</span> beta-CL-20 agree reasonably well with extrapolated pseudo-velocities computed from epsilon-CL-20 isothermal diamond-anvil cell EOS measurements. This work was performed under the auspices of the U.S. Department of Energy by Lawrence Livermore National Laboratory under Contract No. DE-AC52-07NA27344. Sandia National Laboratories is a multi-mission laboratory managed and operated by Sandia Corporati.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/1986E%26PSL..76..209R','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/1986E%26PSL..76..209R"><span>Properties of the Guin ungrouped <span class="hlt">iron</span> meteorite - The origin of Guin and of group-IIE <span class="hlt">irons</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Rubin, A. E.; Jerde, E. A.; Zong, P.; Wasson, J. T.; Westcott, J. W.; Mayeda, T. K.; Clayton, R. N.</p> <p>1986-01-01</p> <p>The composition and structure of the Guin ungrouped <span class="hlt">iron</span> meteorite inclusions have been investigated experimentally. The structural characteristics of polished and etched slabs of the meteorite were studied microscopically in reflected light. Modal abundances of troilite nodules and silicate inclusions were determined by weighing paper traces. The bulk composition of the silicate inclusions was calculated by combining modal phase abundances and mineral compositions. It is found that the largest silicate inclusion (2 x 4 cm) consists mostly of a <span class="hlt">shock</span>-melted plagioclase-rich matrix surrounding large, partly melted augite grains. The oxygen isotopic composition of the inclusion is near that of LL chondrites. The inclusion is found to be similar in composition to selected melt pocket glasses in ordinary chondrites produced in situ by preferential melting of plagioclase rock due to <span class="hlt">shock</span> <span class="hlt">compression</span>. It is suggested that the Guin assemblage was formed by impact melting on a chondritic parent body. Silicate inclusions in IIE <span class="hlt">irons</span> share many of the compositional and petrological characteristics of the Guin inclusions, indicating that IIE <span class="hlt">irons</span> also formed by impact-melting of chondritic materials. Black and white photomicrographs of the silicate inclusions are provided.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2010PhRvE..82b6401Z','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2010PhRvE..82b6401Z"><span>Measurements of the equations of state and spectrum of nonideal xenon plasma under <span class="hlt">shock</span> <span class="hlt">compression</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Zheng, J.; Gu, Y. J.; Chen, Z. Y.; Chen, Q. F.</p> <p>2010-08-01</p> <p>Experimental equations of state on generation of nonideal xenon plasma by intense <span class="hlt">shock</span> wave <span class="hlt">compression</span> was presented in the ranges of pressure of 2-16 GPa and temperature of 31-50 kK, and the xenon plasma with the nonideal coupling parameter Γ range from 0.6-2.1 was generated. The <span class="hlt">shock</span> wave was produced using the flyer plate impact and accelerated up to ˜6km/s with a two-stage light gas gun. Gaseous specimens were <span class="hlt">shocked</span> from two initial pressures of 0.80 and 4.72 MPa at room temperature. Time-resolved spectral radiation histories were recorded by using a multiwavelength channel pyrometer. The transient spectra with the wavelength range of 460-700 nm were recorded by using a spectrometer to evaluate the <span class="hlt">shock</span> temperature. <span class="hlt">Shock</span> velocity was measured and particle velocity was determined by the impedance matching methods. The equations of state of xenon plasma and ionization degree have been discussed in terms of the self-consistent fluid variational theory.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/20866920','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/20866920"><span>Measurements of the equations of state and spectrum of nonideal xenon plasma under <span class="hlt">shock</span> <span class="hlt">compression</span>.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Zheng, J; Gu, Y J; Chen, Z Y; Chen, Q F</p> <p>2010-08-01</p> <p>Experimental equations of state on generation of nonideal xenon plasma by intense <span class="hlt">shock</span> wave <span class="hlt">compression</span> was presented in the ranges of pressure of 2-16 GPa and temperature of 31-50 kK, and the xenon plasma with the nonideal coupling parameter Γ range from 0.6-2.1 was generated. The <span class="hlt">shock</span> wave was produced using the flyer plate impact and accelerated up to ∼6 km/s with a two-stage light gas gun. Gaseous specimens were <span class="hlt">shocked</span> from two initial pressures of 0.80 and 4.72 MPa at room temperature. Time-resolved spectral radiation histories were recorded by using a multiwavelength channel pyrometer. The transient spectra with the wavelength range of 460-700 nm were recorded by using a spectrometer to evaluate the <span class="hlt">shock</span> temperature. <span class="hlt">Shock</span> velocity was measured and particle velocity was determined by the impedance matching methods. The equations of state of xenon plasma and ionization degree have been discussed in terms of the self-consistent fluid variational theory.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19730017097','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19730017097"><span>Terminal <span class="hlt">shock</span> position and restart control of a Mach 2.7, two-dimensional, twin duct mixed <span class="hlt">compression</span> inlet</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Cole, G. L.; Neiner, G. H.; Baumbick, R. J.</p> <p>1973-01-01</p> <p>Experimental results of terminal <span class="hlt">shock</span> and restart control system tests of a two-dimensional, twin-duct mixed <span class="hlt">compression</span> inlet are presented. High-response (110-Hz bandwidth) overboard bypass doors were used, both as the variable to control <span class="hlt">shock</span> position and as the means of disturbing the inlet airflow. An inherent instability in inlet <span class="hlt">shock</span> position resulted in noisy feedback signals and thus restricted the terminal <span class="hlt">shock</span> position control performance that was achieved. Proportional-plus-integral type controllers using either throat exit static pressure or <span class="hlt">shock</span> position sensor feedback gave adequate low-frequency control. The inlet restart control system kept the terminal <span class="hlt">shock</span> control loop closed throughout the unstart-restart transient. The capability to restart the inlet was non limited by the inlet instability.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015APS..DPPCO4012H','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015APS..DPPCO4012H"><span>Dynamic <span class="hlt">Shock</span> <span class="hlt">Compression</span> of Copper to Multi-Megabar Pressure</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Haill, T. A.; Furnish, M. D.; Twyeffort, L. L.; Arrington, C. L.; Lemke, R. W.; Knudson, M. D.; Davis, J.-P.</p> <p>2015-11-01</p> <p>Copper is an important material for a variety of <span class="hlt">shock</span> and high energy density applications and experiments. Copper is used as a standard reference material to determine the EOS properties of other materials. The high conductivity of copper makes it useful as an MHD driver layer in high current dynamic materials experiments on Sandia National Laboratories Z machine. Composite aluminum/copper flyer plates increase the dwell time in plate impact experiments by taking advantage of the slower wave speeds in copper. This presentation reports on recent efforts to reinstate a composite Al/Cu flyer capability on Z and to extend the range of equation-of-state <span class="hlt">shock</span> <span class="hlt">compression</span> data through the use of hyper-velocity composite flyers and symmetric planar impact with copper targets. We will present results from multi-dimensional ALEGRA MHD simulations, as well as experimental designs and methods of composite flyer fabrication. Sandia National Laboratories is a multi-program laboratory managed and operated by Sandia Corporation, a wholly owned subsidiary of Lockheed Martin Company, for the U.S. DOE's National Nuclear Security Administration under contract DE-AC04-94AL85000.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018JAP...123m5902L','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018JAP...123m5902L"><span>Time-resolved light emission of a, c, and r-cut sapphires <span class="hlt">shock-compressed</span> to 65 GPa</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Liu, Q. C.; Zhou, X. M.</p> <p>2018-04-01</p> <p>To investigate light emission and dynamic deformation behaviors, sapphire (single crystal Al2O3) samples with three crystallographic orientations (a, c, and r-cut) were <span class="hlt">shock-compressed</span> by the planar impact method, with final stress ranges from 47 to 65 GPa. Emission radiance and velocity versus time profiles were simultaneously measured with a fast pyrometer and a Doppler pin system in each experiment. Wave profile results show anisotropic elastic-plastic transitions, which confirm the literature observations. Under final <span class="hlt">shock</span> stress of about 52 GPa, lower emission intensity is observed in the r-cut sample, in agreement with the previous report in the literature. When final <span class="hlt">shock</span> stress increases to 57 GPa and 65 GPa, spectral radiance histories of the r-cut show two stages of distinct features. In the first stage, the emission intensity of r-cut is lower than those of the other two, which agrees with the previous report in the literature. In the second stage, spectral radiance of r-cut increases with time at much higher rate and it finally peaks over those of the a and c-cut. These observations (conversion of intensified emission in the r-cut) may indicate activation of a second slip system and formation of shear bands which are discussed with the resolved shear stress calculations for the slip systems in each of the three cuts under <span class="hlt">shock</span> <span class="hlt">compression</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018HPR....38....1W','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018HPR....38....1W"><span>Electrical resistivity of fluid methane multiply <span class="hlt">shock</span> <span class="hlt">compressed</span> to 147 GPa</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Wang, Yi-Gao; Liu, Fu-Sheng; Liu, Qi-Jun; Wang, Wen-Peng</p> <p>2018-01-01</p> <p><span class="hlt">Shock</span> wave experiments were carried out to measure the electrical resistivity of fluid methane. The pressure range of 89-147 GPa and the temperature range from 1800 to 2600 K were achieved with a two-stage light-gas gun. We obtained a minimum electrical resistivity value of 4.5 × 10-2 Ω cm at pressure and temperature of 147 GPa and 2600 K, which is two orders of magnitude higher than that of hydrogen under similar conditions. The data are interpreted in terms of a continuous transition from insulator to semiconductor state. One possibility reason is chemical decomposition of methane in the <span class="hlt">shock</span> <span class="hlt">compression</span> process. Along density and temperature increase with Hugoniot pressure, dissociation of fluid methane increases continuously to form a H2-rich fluid.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018JAP...123p5901L','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018JAP...123p5901L"><span>Birefringence and incipient plastic deformation in elastically overdriven [100] CaF2 under <span class="hlt">shock</span> <span class="hlt">compression</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Li, Y.; Zhou, X. M.; Cai, Y.; Liu, C. L.; Luo, S. N.</p> <p>2018-04-01</p> <p>[100] CaF2 single crystals are <span class="hlt">shock-compressed</span> via symmetric planar impact, and the flyer plate-target interface velocity histories are measured with a laser displacement interferometry. The <span class="hlt">shock</span> loading is slightly above the Hugoniot elastic limit to investigate incipient plasticity and its kinetics, and its effects on optical properties and deformation inhomogeneity. Fringe patterns demonstrate different features in modulation of fringe amplitude, including birefringence and complicated modulations. The birefringence is attributed to local lattice rotation accompanying incipient plasticity. Spatially resolved measurements show inhomogeneity in deformation, birefringence, and fringe pattern evolutions, most likely caused by the inhomogeneity associated with lattice rotation and dislocation slip. Transiently overdriven elastic states are observed, and the incubation time for incipient plasticity decreases inversely with increasing overdrive by the elastic <span class="hlt">shock</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/23432260','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/23432260"><span>X-ray scattering measurements of strong ion-ion correlations in <span class="hlt">shock-compressed</span> aluminum.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Ma, T; Döppner, T; Falcone, R W; Fletcher, L; Fortmann, C; Gericke, D O; Landen, O L; Lee, H J; Pak, A; Vorberger, J; Wünsch, K; Glenzer, S H</p> <p>2013-02-08</p> <p>The strong ion-ion correlation peak characteristic of warm dense matter (WDM) is observed for the first time using simultaneous angularly, temporally, and spectrally resolved x-ray scattering measurements in laser-driven <span class="hlt">shock-compressed</span> aluminum. Laser-produced molybdenum x-ray line emission at an energy of 17.9 keV is employed to probe aluminum <span class="hlt">compressed</span> to a density of ρ>8 g/cm(3). We observe a well pronounced peak in the static structure factor at a wave number of k=4.0 Å(-1). The measurements of the magnitude and position of this correlation peak are precise enough to test different theoretical models for the ion structure and show that only models taking the complex interaction in WDM into account agree with the data. This also demonstrates a new highly accurate diagnostic to directly measure the state of <span class="hlt">compression</span> of warm dense matter.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/20366206','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/20366206"><span>Measurements of ionic structure in <span class="hlt">shock</span> <span class="hlt">compressed</span> lithium hydride from ultrafast x-ray Thomson scattering.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Kritcher, A L; Neumayer, P; Brown, C R D; Davis, P; Döppner, T; Falcone, R W; Gericke, D O; Gregori, G; Holst, B; Landen, O L; Lee, H J; Morse, E C; Pelka, A; Redmer, R; Roth, M; Vorberger, J; Wünsch, K; Glenzer, S H</p> <p>2009-12-11</p> <p>We present the first ultrafast temporally, spectrally, and angularly resolved x-ray scattering measurements from <span class="hlt">shock-compressed</span> matter. The experimental spectra yield the absolute elastic and inelastic scattering intensities from the measured density of free electrons. Laser-<span class="hlt">compressed</span> lithium-hydride samples are well characterized by inelastic Compton and plasmon scattering of a K-alpha x-ray probe providing independent measurements of temperature and density. The data show excellent agreement with the total intensity and structure when using the two-species form factor and accounting for the screening of ion-ion interactions.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2000AIPC..505..601B','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2000AIPC..505..601B"><span>Failure waves in glass and ceramics under <span class="hlt">shock</span> <span class="hlt">compression</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Brar, N. S.</p> <p>2000-04-01</p> <p>The response of various types of glasses (fused silica, borosilicates, soda-lime, and lead filled) to <span class="hlt">shock</span> wave loading, especially the failure of glass behind the <span class="hlt">shock</span> wave through the "so called" failure wave or front, has been the subject of intense research among a number of investigators. The variations in material properties across this front include complete loss of tensile (spall) strength, loss in shear strength, reduction in acoustic impedance and opacity to light. Both the Stress and velocity history from VISAR measurements have shown that the failure front propagates at a speed of 1.5 to 2.5 mm/s, depending on the peak <span class="hlt">shock</span> stress. The shear strength [τ=1/2(σ1-σ2)] behind the failure front, determined using embedded transverse gauges, is found to decrease to about 1 GPa for soda-lime, borosilicate, and filled glasses. Optical (high-speed photography) observations also confirm formation of this failure front. There is a general agreement among various researchers on these failure observations. However, three proposed mechanisms for the formation of failure front are based on totally different formulations. The first, due to Clifton, is based on the hypothesis of densification of glass under <span class="hlt">shock</span> <span class="hlt">compression</span>. Densification is followed by shear failure around inhomogeneities resulting in a phase boundary between the comminuted and the intact material. The second, proposed by Grady, involves the transfer of elastic shear strain energy to dilatant strain energy as a result of severe micro-cracking originating from impact. The third, by Espinosa and Brar, proposes that the front is created through shear micro-cracks, which nucleate and propagate from the impact face; as originally suggested by Kanel. This later mechanism is supported by the observed loss of shear strength of glass by Clifton et al. at <span class="hlt">shock</span> stress above the threshold level. Espinosa has incorporated this mechanism in multiple-plane model and simulations predict the increase in lateral</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20110013216','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20110013216"><span>Uncertainty Assessments of 2D and Axisymmetric Hypersonic <span class="hlt">Shock</span> Wave - Turbulent Boundary Layer Interaction Simulations at <span class="hlt">Compression</span> Corners</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Gnoffo, Peter A.; Berry, Scott A.; VanNorman, John W.</p> <p>2011-01-01</p> <p>This paper is one of a series of five papers in a special session organized by the NASA Fundamental Aeronautics Program that addresses uncertainty assessments for CFD simulations in hypersonic flow. Simulations of a <span class="hlt">shock</span> emanating from a <span class="hlt">compression</span> corner and interacting with a fully developed turbulent boundary layer are evaluated herein. Mission relevant conditions at Mach 7 and Mach 14 are defined for a pre-<span class="hlt">compression</span> ramp of a scramjet powered vehicle. Three <span class="hlt">compression</span> angles are defined, the smallest to avoid separation losses and the largest to force a separated flow engaging more complicated flow physics. The Baldwin-Lomax and the Cebeci-Smith algebraic models, the one-equation Spalart-Allmaras model with the Catrix-Aupoix <span class="hlt">compressibility</span> modification and two-equation models including Menter SST, Wilcox k-omega 98, and Wilcox k-omega 06 turbulence models are evaluated. Each model is fully defined herein to preclude any ambiguity regarding model implementation. Comparisons are made to existing experimental data and Van Driest theory to provide preliminary assessment of model form uncertainty. A set of coarse grained uncertainty metrics are defined to capture essential differences among turbulence models. Except for the inability of algebraic models to converge for some separated flows there is no clearly superior model as judged by these metrics. A preliminary metric for the numerical component of uncertainty in <span class="hlt">shock</span>-turbulent-boundary-layer interactions at <span class="hlt">compression</span> corners sufficiently steep to cause separation is defined as 55%. This value is a median of differences with experimental data averaged for peak pressure and heating and for extent of separation captured in new, grid-converged solutions presented here. This value is consistent with existing results in a literature review of hypersonic <span class="hlt">shock</span>-turbulent-boundary-layer interactions by Roy and Blottner and with more recent computations of MacLean.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_6");'>6</a></li> <li><a href="#" onclick='return showDiv("page_7");'>7</a></li> <li class="active"><span>8</span></li> <li><a href="#" onclick='return showDiv("page_9");'>9</a></li> <li><a href="#" onclick='return showDiv("page_10");'>10</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_8 --> <div id="page_9" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_7");'>7</a></li> <li><a href="#" onclick='return showDiv("page_8");'>8</a></li> <li class="active"><span>9</span></li> <li><a href="#" onclick='return showDiv("page_10");'>10</a></li> <li><a href="#" onclick='return showDiv("page_11");'>11</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="161"> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/28128621','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/28128621"><span>Ultrafast X-Ray Diffraction Studies of the Phase Transitions and Equation of State of Scandium <span class="hlt">Shock</span> <span class="hlt">Compressed</span> to 82 GPa.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Briggs, R; Gorman, M G; Coleman, A L; McWilliams, R S; McBride, E E; McGonegle, D; Wark, J S; Peacock, L; Rothman, S; Macleod, S G; Bolme, C A; Gleason, A E; Collins, G W; Eggert, J H; Fratanduono, D E; Smith, R F; Galtier, E; Granados, E; Lee, H J; Nagler, B; Nam, I; Xing, Z; McMahon, M I</p> <p>2017-01-13</p> <p>Using x-ray diffraction at the Linac Coherent Light Source x-ray free-electron laser, we have determined simultaneously and self-consistently the phase transitions and equation of state (EOS) of the lightest transition metal, scandium, under <span class="hlt">shock</span> <span class="hlt">compression</span>. On <span class="hlt">compression</span> scandium undergoes a structural phase transition between 32 and 35 GPa to the same bcc structure seen at high temperatures at ambient pressures, and then a further transition at 46 GPa to the incommensurate host-guest polymorph found above 21 GPa in static <span class="hlt">compression</span> at room temperature. <span class="hlt">Shock</span> melting of the host-guest phase is observed between 53 and 72 GPa with the disappearance of Bragg scattering and the growth of a broad asymmetric diffraction peak from the high-density liquid.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016APS..DPPC10006S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016APS..DPPC10006S"><span>Simulations of Converging <span class="hlt">Shock</span> Collisions for <span class="hlt">Shock</span> Ignition</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Sauppe, Joshua; Dodd, Evan; Loomis, Eric</p> <p>2016-10-01</p> <p><span class="hlt">Shock</span> ignition (SI) has been proposed as an alternative to achieving high gain in inertial confinement fusion (ICF) targets. A central hot spot below the ignition threshold is created by an initial <span class="hlt">compression</span> pulse, and a second laser pulse drives a strong converging <span class="hlt">shock</span> into the fuel. The collision between the rebounding <span class="hlt">shock</span> from the <span class="hlt">compression</span> pulse and the converging <span class="hlt">shock</span> results in amplification of the converging <span class="hlt">shock</span> and increases the hot spot pressure above the ignition threshold. We investigate <span class="hlt">shock</span> collision in SI drive schemes for cylindrical targets with a polystyrene foam interior using radiation-hydrodynamics simulations with the RAGE code. The configuration is similar to previous targets fielded on the Omega laser. The CH interior results in a lower convergence ratio and the cylindrical geometry facilitates visualization of the <span class="hlt">shock</span> transit using an axial X-ray backlighter, both of which are important for comparison to potential experimental measurements. One-dimensional simulations are used to determine <span class="hlt">shock</span> timing, and the effects of low mode asymmetries in 2D computations are also quantified. LA-UR-16-24773.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018JAP...123q5903H','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018JAP...123q5903H"><span><span class="hlt">Shock</span> <span class="hlt">compression</span> behavior of a mixture of cubic and hexagonal boron nitride</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Hu, Xiaojun; Yang, Gang; Zhao, Bin; Li, Peiyun; Yang, Jun; Leng, Chunwei; Liu, Hanyu; Huang, Haijun; Fei, Yingwei</p> <p>2018-05-01</p> <p>We report Hugoniot measurements on a mixture of cubic boron nitride (cBN) and hexagonal boron nitride (hBN, ˜10% in weight) to investigate the <span class="hlt">shock</span> <span class="hlt">compression</span> behavior of BN at Hugoniot stresses up to 110 GPa. We observed a discontinuity at ˜77 GPa along the Hugoniot and interpreted it as the manifestation of the <span class="hlt">shock</span>-induced phase transition of hBN to cBN. The experimental stress at 77-110 GPa shows significant deviation from the hydrodynamic Hugoniot of cBN calculated using the Mie-Grüneisen model coupled with the reported 300 K-isotherms of cBN. Our investigation reveals that material strength in cBN increases with the experimental stress at least up to 110 GPa. The material strength might be preserved at higher stress if we consider the previously reported high stress data.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015APS..SHK.W1027R','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015APS..SHK.W1027R"><span>Synchrotron hard X-ray imaging of <span class="hlt">shock-compressed</span> metal powders</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Rutherford, Michael E.; Chapman, David J.; Collinson, Mark A.; Jones, David R.; Music, Jasmina; Stafford, Samuel J. P.; Tear, Gareth R.; White, Thomas G.; Winters, John B. R.; Drakopoulos, Michael; Eakins, Daniel E.</p> <p>2015-06-01</p> <p>This poster will present the application of a new, high-energy (50 to 250 keV) synchrotron X-ray radiography technique to the study of <span class="hlt">shock-compressed</span> granular materials. Following plate-impact loading, transmission radiography was used to quantitatively observe the compaction and release processes in a range of high-Z metal powders (e.g. Fe, Ni, Cu). By comparing the predictions of 3D numerical models initialized from X-ray tomograms-captured prior to loading-with experimental results, this research represents a new approach to refining mesoscopic compaction models. The authors gratefully acknowledge the ongoing support of Imperial College London, EPSRC, STFC and the Diamond Light Source, and AWE Plc.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/1999APS..SHK..H401S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/1999APS..SHK..H401S"><span>Failure Waves in Glass and Ceramics under <span class="hlt">Shock</span> <span class="hlt">Compression</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Singh Brar, N.</p> <p>1999-06-01</p> <p>The response of various types of glasses (fused silica, borosilicates, soda-lime, and lead filled) to <span class="hlt">shock</span> wave loading, especially the failure of glass behind the <span class="hlt">shock</span> wave through the ``so called" failure wave or front has been the subject of intense research among a number of investigators. The variations in material properties across this front include complete loss of tensile (spall) strength, loss in shear strength, reduction in acoustic impedance, and opacity to light. Both the Stress and velocity history from VISAR measurements have shown that the failure front propagates at a speed of 1.5 to 2.5 mm/s, depending on the peak <span class="hlt">shock</span> stress level. The shear strength [τ = 1/2(σ_x-σ_y)] behind the failure front, determined using embedded transverse gauges, is found to decrease to about 2 GPa for soda-lime, borosilicate, and filled glasses. The optical (high-speed photography) observations also confirm the formation of failure front. There is a general agreement among various researchers on these observations. However, three proposed mechanisms for the formation of failure front are based on totally different formulations. The first, due to Clifton is based on the process of nucleation of local densification due to <span class="hlt">shock</span> <span class="hlt">compression</span> followed by shear failure around inhomogeneities resulting in phase boundary between the comminuted from the intact material. The second, proposed by Grady involves the transfer of elastic shear strain energy to dilatant strain energy as a result of severe microcracking originating from impact face. The third, by Espinosa and Brar proposes that the front is created through shear microcracks, which nucleate and propagate from the impact face, as originally suggested by Kanel. This mechanism is incorporated in multiple-plane model and simulations predict the increase in lateral stress and an observed reduction in spall strength behind the failure front. Failure front studies, in terms of loss of shear strength, have been recently</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018PhRvB..97l5106W','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018PhRvB..97l5106W"><span><span class="hlt">Shock</span> <span class="hlt">compression</span> of strongly correlated oxides: A liquid-regime equation of state for cerium(IV) oxide</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Weck, Philippe F.; Cochrane, Kyle R.; Root, Seth; Lane, J. Matthew D.; Shulenburger, Luke; Carpenter, John H.; Sjostrom, Travis; Mattsson, Thomas R.; Vogler, Tracy J.</p> <p>2018-03-01</p> <p>The <span class="hlt">shock</span> Hugoniot for full-density and porous CeO2 was investigated in the liquid regime using ab initio molecular dynamics (AIMD) simulations with Erpenbeck's approach based on the Rankine-Hugoniot jump conditions. The phase space was sampled by carrying out NVT simulations for isotherms between 6000 and 100 000 K and densities ranging from ρ =2.5 to 20 g /cm3 . The impact of on-site Coulomb interaction corrections +U on the equation of state (EOS) obtained from AIMD simulations was assessed by direct comparison with results from standard density functional theory simulations. Classical molecular dynamics (CMD) simulations were also performed to model atomic-scale <span class="hlt">shock</span> <span class="hlt">compression</span> of larger porous CeO2 models. Results from AIMD and CMD <span class="hlt">compression</span> simulations compare favorably with Z-machine <span class="hlt">shock</span> data to 525 GPa and gas-gun data to 109 GPa for porous CeO2 samples. Using results from AIMD simulations, an accurate liquid-regime Mie-Grüneisen EOS was built for CeO2. In addition, a revised multiphase SESAME-type EOS was constrained using AIMD results and experimental data generated in this work. This study demonstrates the necessity of acquiring data in the porous regime to increase the reliability of existing analytical EOS models.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1361149-ultrafast-ray-diffraction-studies-phase-transitions-equation-state-scandium-shock-compressed-nbsp-gpa','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1361149-ultrafast-ray-diffraction-studies-phase-transitions-equation-state-scandium-shock-compressed-nbsp-gpa"><span>Ultrafast X-Ray Diffraction Studies of the Phase Transitions and Equation of State of Scandium <span class="hlt">Shock</span> <span class="hlt">Compressed</span> to 82 GPa</span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>Briggs, R.; Gorman, M. G.; Coleman, A. L.; ...</p> <p>2017-01-09</p> <p>Using x-ray diffraction at the Linac Coherent Light Source x-ray free-electron laser, we have determined simultaneously and self-consistently the phase transitions and equation of state (EOS) of the lightest transition metal, scandium, under <span class="hlt">shock</span> <span class="hlt">compression</span>. On <span class="hlt">compression</span> scandium undergoes a structural phase transition between 32 and 35 GPa to the same bcc structure seen at high temperatures at ambient pressures, and then a further transition at 46 GPa to the incommensurate host-guest polymorph found above 21 GPa in static <span class="hlt">compression</span> at room temperature. Furthermore, <span class="hlt">shock</span> melting of the host-guest phase is observed between 53 and 72 GPa with the disappearancemore » of Bragg scattering and the growth of a broad asymmetric diffraction peak from the high-density liquid.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/1136193-release-path-temperatures-shock-compressed-tin-from-dynamic-reflectance-radiance-measurements','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/1136193-release-path-temperatures-shock-compressed-tin-from-dynamic-reflectance-radiance-measurements"><span>Release Path Temperatures of <span class="hlt">Shock-Compressed</span> Tin from Dynamic Reflectance and Radiance Measurements</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>La Lone, B. M.; Stevens, G. D.; Turley, W. D.</p> <p>2013-08-01</p> <p>Dynamic reflectance and radiance measurements were conducted for tin samples <span class="hlt">shock</span> <span class="hlt">compressed</span> to 35 GPa and released to 15 GPa using high explosives. We determined the reflectance of the tin samples glued to lithium fluoride windows using an integrating sphere with an internal xenon flashlamp as an illumination source. The dynamic reflectance (R) was determined at near normal incidence in four spectral bands with coverage in visible and near-infrared spectra. Uncertainties in R/R0 are < 2%, and uncertainties in absolute reflectance are < 5%. In complementary experiments, thermal radiance from the tin/glue/lithium fluoride interface was recorded with similar <span class="hlt">shock</span> stressmore » and spectral coverage as the reflectance measurements. The two sets of experiments were combined to obtain the temperature history of the tin surface with an uncertainty of < 2%. The stress at the interface was determined from photonic Doppler velocimetry and combined with the temperatures to obtain temperature-stress release paths for tin. We discuss the relationship between the experimental release paths and release isentropes that begin on the principal <span class="hlt">shock</span> Hugoniot.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/24115435','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/24115435"><span>Femtosecond visualization of lattice dynamics in <span class="hlt">shock-compressed</span> matter.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Milathianaki, D; Boutet, S; Williams, G J; Higginbotham, A; Ratner, D; Gleason, A E; Messerschmidt, M; Seibert, M M; Swift, D C; Hering, P; Robinson, J; White, W E; Wark, J S</p> <p>2013-10-11</p> <p>The ultrafast evolution of microstructure is key to understanding high-pressure and strain-rate phenomena. However, the visualization of lattice dynamics at scales commensurate with those of atomistic simulations has been challenging. Here, we report femtosecond x-ray diffraction measurements unveiling the response of copper to laser <span class="hlt">shock-compression</span> at peak normal elastic stresses of ~73 gigapascals (GPa) and strain rates of 10(9) per second. We capture the evolution of the lattice from a one-dimensional (1D) elastic to a 3D plastically relaxed state within a few tens of picoseconds, after reaching shear stresses of 18 GPa. Our in situ high-precision measurement of material strength at spatial (<1 micrometer) and temporal (<50 picoseconds) scales provides a direct comparison with multimillion-atom molecular dynamics simulations.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2012AGUFMMR23B2415H','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2012AGUFMMR23B2415H"><span>The Effect of Wavelength-Dependent Emissivity on the Melting Temperatures of <span class="hlt">Iron</span> From <span class="hlt">Shock</span> Wave Measurements</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Heinz, D. L.; Mark, H.</p> <p>2012-12-01</p> <p>The high-pressure melting curve of <span class="hlt">iron</span> at the conditions of the outer core is anchored by the <span class="hlt">shock</span> wave measurements of Bass et. al. 1987. They used spectral radiometric techniques, looking at <span class="hlt">shocked</span> <span class="hlt">iron</span> films or foils through a transparent anvil. They assumed that the emissivity of the <span class="hlt">iron</span> was independent of wavelength. The wavelength dependence of the emissivity of fcc and bcc <span class="hlt">iron</span> was measured by Taylor, 1952. Both structures have a change in emissivity of 20% over 200nm in the visible, although the absolute magnitude of the emissivity is different. In the measurement of temperature using spectral radiometry, the absolute value of the emissivity does not effect the temperature measurement. In <span class="hlt">iron</span> the 3d-bands straddle the Fermi Energy in any close packed structure (Boness and Brown, 1990). The electrons at the Fermi Energy can easily be promoted into the empty states of the conduction band, and thus are the basis of the electronic contribution to the heat capacity. It is these same electrons in the 3d-bands that also control the emissivity. With increasing wavelength, more electrons are promoted into the conduction band, which means the emissivity is higher at shorter wavelengths than at longer wavelengths. We reanalyzed the <span class="hlt">shock</span> wave data of Bass et. al. using the wavelength dependent emissivity. The corrected melting temperature of <span class="hlt">iron</span> at 243 GPa is 5900 +/-500 K compared to Bass et. al.'s determination of 6700 +/- 400 K. This is just slightly higher then the estimate (based upon the assumption of the heat capacity being equal to 5R) of Brown and McQueen, 1986 of 5000-5700 K, and in good agreement with theoretical calculations of Alfe, 2010. Alfe, D., 2010, Rev. Min. and Geochem., 71, 337-354. Bass, J. D., B. Svendsen, and T. J. Ahrens, 1987, M. H. Manghnani and Y. Syono, Terra Scientific Publishing Co. / American Geophysical Union, Washington, D. C., 393-402. Boness, D. A., and J. M. Brown, 1990, JGR, 95, 21,721-30. Brown, J. M. and R. G. Mc</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/22499254-simulations-situ-ray-diffraction-from-uniaxially-compressed-highly-textured-polycrystalline-targets','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/22499254-simulations-situ-ray-diffraction-from-uniaxially-compressed-highly-textured-polycrystalline-targets"><span>Simulations of in situ x-ray diffraction from uniaxially <span class="hlt">compressed</span> highly textured polycrystalline targets</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>McGonegle, David, E-mail: d.mcgonegle1@physics.ox.ac.uk; Wark, Justin S.; Higginbotham, Andrew</p> <p>2015-08-14</p> <p>A growing number of <span class="hlt">shock</span> <span class="hlt">compression</span> experiments, especially those involving laser <span class="hlt">compression</span>, are taking advantage of in situ x-ray diffraction as a tool to interrogate structure and microstructure evolution. Although these experiments are becoming increasingly sophisticated, there has been little work on exploiting the textured nature of polycrystalline targets to gain information on sample response. Here, we describe how to generate simulated x-ray diffraction patterns from materials with an arbitrary texture function subject to a general deformation gradient. We will present simulations of Debye-Scherrer x-ray diffraction from highly textured polycrystalline targets that have been subjected to uniaxial <span class="hlt">compression</span>, as maymore » occur under planar <span class="hlt">shock</span> conditions. In particular, we study samples with a fibre texture, and find that the azimuthal dependence of the diffraction patterns contains information that, in principle, affords discrimination between a number of similar <span class="hlt">shock</span>-deformation mechanisms. For certain cases, we compare our method with results obtained by taking the Fourier transform of the atomic positions calculated by classical molecular dynamics simulations. Illustrative results are presented for the <span class="hlt">shock</span>-induced α–ϵ phase transition in <span class="hlt">iron</span>, the α–ω transition in titanium and deformation due to twinning in tantalum that is initially preferentially textured along [001] and [011]. The simulations are relevant to experiments that can now be performed using 4th generation light sources, where single-shot x-ray diffraction patterns from crystals <span class="hlt">compressed</span> via laser-ablation can be obtained on timescales shorter than a phonon period.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1414361-simulations-situ-ray-diffraction-from-uniaxially-compressed-highly-textured-polycrystalline-targets','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1414361-simulations-situ-ray-diffraction-from-uniaxially-compressed-highly-textured-polycrystalline-targets"><span>Simulations of in situ x-ray diffraction from uniaxially <span class="hlt">compressed</span> highly textured polycrystalline targets</span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>McGonegle, David; Milathianaki, Despina; Remington, Bruce A.; ...</p> <p>2015-08-11</p> <p>A growing number of <span class="hlt">shock</span> <span class="hlt">compression</span> experiments, especially those involving laser <span class="hlt">compression</span>, are taking advantage of in situ x-ray diffraction as a tool to interrogate structure and microstructure evolution. Although these experiments are becoming increasingly sophisticated, there has been little work on exploiting the textured nature of polycrystalline targets to gain information on sample response. Here, we describe how to generate simulated x-ray diffraction patterns from materials with an arbitrary texture function subject to a general deformation gradient. We will present simulations of Debye-Scherrer x-ray diffraction from highly textured polycrystalline targets that have been subjected to uniaxial <span class="hlt">compression</span>, as maymore » occur under planar <span class="hlt">shock</span> conditions. In particular, we study samples with a fibre texture, and find that the azimuthal dependence of the diffraction patterns contains information that, in principle, affords discrimination between a number of similar <span class="hlt">shock</span>-deformation mechanisms. For certain cases, we compare our method with results obtained by taking the Fourier transform of the atomic positions calculated by classical molecular dynamics simulations. Illustrative results are presented for the <span class="hlt">shock</span>-induced α–ϵ phase transition in <span class="hlt">iron</span>, the α–ω transition in titanium and deformation due to twinning in tantalum that is initially preferentially textured along [001] and [011]. In conclusion, the simulations are relevant to experiments that can now be performed using 4th generation light sources, where single-shot x-ray diffraction patterns from crystals <span class="hlt">compressed</span> via laser-ablation can be obtained on timescales shorter than a phonon period.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20070023401','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20070023401"><span>Nonstandard Analysis and <span class="hlt">Shock</span> Wave Jump Conditions in a One-Dimensional <span class="hlt">Compressible</span> Gas</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Baty, Roy S.; Farassat, Fereidoun; Hargreaves, John</p> <p>2007-01-01</p> <p>Nonstandard analysis is a relatively new area of mathematics in which infinitesimal numbers can be defined and manipulated rigorously like real numbers. This report presents a fairly comprehensive tutorial on nonstandard analysis for physicists and engineers with many examples applicable to generalized functions. To demonstrate the power of the subject, the problem of <span class="hlt">shock</span> wave jump conditions is studied for a one-dimensional <span class="hlt">compressible</span> gas. It is assumed that the <span class="hlt">shock</span> thickness occurs on an infinitesimal interval and the jump functions in the thermodynamic and fluid dynamic parameters occur smoothly across this interval. To use conservations laws, smooth pre-distributions of the Dirac delta measure are applied whose supports are contained within the <span class="hlt">shock</span> thickness. Furthermore, smooth pre-distributions of the Heaviside function are applied which vary from zero to one across the <span class="hlt">shock</span> wave. It is shown that if the equations of motion are expressed in nonconservative form then the relationships between the jump functions for the flow parameters may be found unambiguously. The analysis yields the classical Rankine-Hugoniot jump conditions for an inviscid <span class="hlt">shock</span> wave. Moreover, non-monotonic entropy jump conditions are obtained for both inviscid and viscous flows. The report shows that products of generalized functions may be defined consistently using nonstandard analysis; however, physically meaningful products of generalized functions must be determined from the physics of the problem and not the mathematical form of the governing equations.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2008JAP...103j3537Y','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2008JAP...103j3537Y"><span>Dynamic shear strength of S2 glass fiber reinforced polymer composites under <span class="hlt">shock</span> <span class="hlt">compression</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Yuan, Fuping; Tsai, Liren; Prakash, Vikas; Dandekar, Dattatraya P.; Rajendran, A. M.</p> <p>2008-05-01</p> <p>In the present paper, a series of plate impact <span class="hlt">shock</span>-reshock and <span class="hlt">shock</span>-release experiments were conducted to study the critical shear strength of a S2 glass fiber reinforced polymer (GRP) composite under <span class="hlt">shock</span> <span class="hlt">compression</span> levels ranging from 0.8 to 1.8 GPa. The GRP was fabricated at ARL, Aberdeen, using S2 glass woven roving in a Cycom 4102 polyester resin matrix. The experiments were conducted by using an 82.5 mm bore single-stage gas gun at Case Western Reserve University. In order to conduct <span class="hlt">shock</span>-reshock and <span class="hlt">shock</span>-release experiments a dual flyer plate assembly was utilized. The <span class="hlt">shock</span>-reshock experiments were conducted by using a projectile faced with GRP and backed with a relatively high <span class="hlt">shock</span> impedance Al 6061-T6 plate; while for the <span class="hlt">shock</span>-release experiments the GRP was backed by a relatively lower impedance polymethyl methacrylate backup flyer plate. A multibeam velocity interferometer was used to measure the particle velocity profile at the rear surface of the target plate. By using self-consistent technique procedure described by Asay and Chabbildas [<span class="hlt">Shock</span> Waves and High-Strain-Rate Phenomena, in Metals, edited by M. M. Myers and L. E. Murr (Plenum, New York, 1981), pp. 417-431], the critical shear strength of the GRP (2τc) was determined for impact stresses in the range of 0.8 to 1.8 GPa. The results show that the critical shear strength of the GRP is increased from 0.108 GPa to 0.682 GPa when the impact stress is increased from 0.8 to 1.8 GPa. The increase in critical shear strength may be attributed to rate-dependence and/or pressure dependent yield behavior of the GRP.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017AIPC.1793l0011B','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017AIPC.1793l0011B"><span><span class="hlt">Shock</span> <span class="hlt">compression</span> of simulated adobe</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Braithwaite, C. H.; Church, P. D.; Gould, P. J.; Stewart, B.; Jardine, A. P.</p> <p>2017-01-01</p> <p>A series of plate impact experiments were conducted to investigate the <span class="hlt">shock</span> response of a simulant for adobe, a traditional form of building material widely used around the world. Air dried bricks were sourced from the London brick company, dry machined and impacted at a range of velocities in a single stage gas gun. The <span class="hlt">shock</span> Hugoniot was determined (Us =2.26up+0.37) as well as release information. The material was found to behave in a manner which was similar to that of loose sand and considerably less stiff than a weak porous sandstone. The effect of any cementing of the grains was examined by <span class="hlt">shocking</span> powdered samples contained within a cell arrangement.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015APS..SHK.L6003B','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015APS..SHK.L6003B"><span><span class="hlt">Shock</span> <span class="hlt">Compression</span> of Simulated Adobe</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Braithwaite, C. H.; Church, P. D.; Gould, P. J.; Stewart, B.; Jardine, A. P.</p> <p>2015-06-01</p> <p>A series of plate impact experiments were conducted to investigate the <span class="hlt">shock</span> response of a simulant for adobe, a traditional form of building material widely used around the world. Air dried bricks were sourced from the London brick company, dry machined and impacted at a range of velocities in a single stage gas gun. The <span class="hlt">shock</span> Hugoniot was determined (Us = 2.26up + 0.33) as well as release information. The material was found to behave in a manner which was similar to that of loose sand and considerably less stiff than a weak porous sandstone. The effect of any cementing of the grains was examined by <span class="hlt">shocking</span> powdered samples contained within a cell arrangement. The research was funded by DSTL through a WSTC contract.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/16863163','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/16863163"><span>Ultrafast dynamics of self-assembled monolayers under <span class="hlt">shock</span> <span class="hlt">compression</span>: effects of molecular and substrate structure.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Lagutchev, Alexei S; Patterson, James E; Huang, Wentao; Dlott, Dana D</p> <p>2005-03-24</p> <p>Laser-driven approximately 1 GPa <span class="hlt">shock</span> waves are used to dynamically <span class="hlt">compress</span> self-assembled monolayers (SAMs) consisting of octadecanethiol (ODT) on Au and Ag, and pentanedecanethiol (PDT) and benzyl mercaptan (BMT) on Au. The SAM response to <4 ps <span class="hlt">shock</span> loading and approximately 25 ps <span class="hlt">shock</span> unloading is monitored by vibrational sum-frequency generation spectroscopy (SFG), which is sensitive to the instantaneous tilt angle of the SAM terminal group relative to the surface normal. Arrival of the <span class="hlt">shock</span> front causes SFG signal loss in all SAMs with a material time constant <3.5 ps. Thermal desorption and <span class="hlt">shock</span> recovery experiments show that SAMs remain adsorbed on the substrate, so signal loss is attributed to <span class="hlt">shock</span> tilting of the methyl or phenyl groups to angles near 90 degrees. When the <span class="hlt">shock</span> unloads, PDT/Au returns elastically to its native structure whereas ODT/Au does not. ODT evidences a complicated viscoelastic response that arises from at least two conformers, one that remains kinetically trapped in a large-tilt-angle conformation for times >250 ps and one that relaxes in approximately 30 ps to a nearly upright conformation. Although the <span class="hlt">shock</span> responses of PDT/Au, ODT/Ag, and BMT/Au are primarily elastic, a small portion of the molecules, 10-20%, evidence viscoelastic response, either becoming kinetically trapped in large-tilt states or by relaxing in approximately 30 ps back to the native structure. The implications of the observed large-amplitude monolayer dynamics for lubrication under extreme conditions of high strain rates are discussed briefly.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2013ChPhL..30f6401Z','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2013ChPhL..30f6401Z"><span><span class="hlt">Shock</span> <span class="hlt">Compression</span> of the New 47Zr45Ti5Al3V Alloys up to 200 GPa</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Zhang, Pin-Liang; Gong, Zi-Zheng; Ji, Guang-Fu; Wang, Qing-Song; Song, Zhen-Fei; Cao, Yan; Wang, Xiang</p> <p>2013-06-01</p> <p><span class="hlt">Shock</span> <span class="hlt">compression</span> experiments on a new kind of 47Zr45Ti5Al3V alloys at pressures between 28 and 200 GPa are performed using a two-stage light gas gun. The Hugoniot data are obtained by combining the impedance-match method and the electrical probe technique. The relationship between the <span class="hlt">shock</span> wave velocity Us and particle velocity up can be described linearly by Us = 4.324(±0.035) + 1.177(±0.012)up. No obvious evidence of phase transition is found in the <span class="hlt">shock</span> <span class="hlt">compression</span> pressure range. The calculated Us - up relationship obtained from the additive principle is different from the experimental data, indicating that the α → β phase transition occurs below 28 GPa. The Grüneisen parameter γ obtained from the experimental data can be expressed by γ = 1.277(ρ0/ρ). The zero-pressure bulk modulus B0s = 97.96 GPa and its pressure derivative B'0s = 3.68. The P—V—T equation of state for 47Zr45Ti5Al3V is given using the Vinet equation of state to describe the cold curve and the Debye model for the thermal contributions.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/25430279','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/25430279"><span>A magnetic particle time-of-flight (MagPTOF) diagnostic for measurements of <span class="hlt">shock</span>- and <span class="hlt">compression</span>-bang time at the NIF (invited).</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Rinderknecht, H G; Sio, H; Frenje, J A; Magoon, J; Agliata, A; Shoup, M; Ayers, S; Bailey, C G; Gatu Johnson, M; Zylstra, A B; Sinenian, N; Rosenberg, M J; Li, C K; Sèguin, F H; Petrasso, R D; Rygg, J R; Kimbrough, J R; Mackinnon, A; Bell, P; Bionta, R; Clancy, T; Zacharias, R; House, A; Döppner, T; Park, H S; LePape, S; Landen, O; Meezan, N; Robey, H; Glebov, V U; Hohenberger, M; Stoeckl, C; Sangster, T C; Li, C; Parat, J; Olson, R; Kline, J; Kilkenny, J</p> <p>2014-11-01</p> <p>A magnetic particle time-of-flight (MagPTOF) diagnostic has been designed to measure <span class="hlt">shock</span>- and <span class="hlt">compression</span>-bang time using D(3)He-fusion protons and DD-fusion neutrons, respectively, at the National Ignition Facility (NIF). This capability, in combination with <span class="hlt">shock</span>-burn weighted areal density measurements, will significantly constrain the modeling of the implosion dynamics. This design is an upgrade to the existing particle time-of-flight (pTOF) diagnostic, which records bang times using DD or DT neutrons with an accuracy better than ±70 ps [H. G. Rinderknecht et al., Rev. Sci. Instrum. 83, 10D902 (2012)]. The inclusion of a deflecting magnet will increase D(3)He-proton signal-to-background by a factor of 1000, allowing for the first time simultaneous measurements of <span class="hlt">shock</span>- and <span class="hlt">compression</span>-bang times in D(3)He-filled surrogate implosions at the NIF.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017APS..SHK.F4001W','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017APS..SHK.F4001W"><span>Measuring twinning and slip in <span class="hlt">shock-compressed</span> Ta from in-situ x-ray diffraction</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Wehrenberg, Christopher; McGonegle, David; Sliwa, Marcin; Suggit, Matt; Wark, Justin; Lee, Hae Ja; Nagler, Bob; Tavella, Franz; Remington, Bruce; Rudd, Rob; Lazicki, Amy; Park, Hye-Sook; Swift, Damian; Zepeda-Ruiz, Louis; Higginbotham, Andrew; Bolme, Cindy</p> <p>2017-06-01</p> <p>A fundamental understanding of high-pressure and high-strain-rate deformation rests on grasping the underlying microstructural processes, such as twinning and dislocation generation and transport (slip), yet simulations and ex-post-facto recovery experiments provide conflicting answers to these basic issues. Here, we report direct, in-situ observation of twinning and slip in <span class="hlt">shock</span> <span class="hlt">compressed</span> Ta using in-situ x-ray diffraction. A series of <span class="hlt">shock</span> experiments were performed on the Matter in Extreme Conditions end station at LCLS. Direct laser ablation was used to drive a <span class="hlt">shock</span>, ranging in pressure from 10-300 GPa, into a Ta sample with an initial (110) fiber texture. The subsequent changes in texture were observed in-situ by examining the azimuthal distribution of the diffraction intensity and found to match twinning and lattice rotation. Measurements of the twin fraction and lattice rotation were used to calculate the equivalent plastic strain from twinning and slip. This work was performed under the auspices of the U.S. Department of Energy by Lawrence Livermore National Laboratory under Contract No. DE-AC52-07NA27344.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_7");'>7</a></li> <li><a href="#" onclick='return showDiv("page_8");'>8</a></li> <li class="active"><span>9</span></li> <li><a href="#" onclick='return showDiv("page_10");'>10</a></li> <li><a href="#" onclick='return showDiv("page_11");'>11</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_9 --> <div id="page_10" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_8");'>8</a></li> <li><a href="#" onclick='return showDiv("page_9");'>9</a></li> <li class="active"><span>10</span></li> <li><a href="#" onclick='return showDiv("page_11");'>11</a></li> <li><a href="#" onclick='return showDiv("page_12");'>12</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="181"> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2008PhPl...15f2703Y','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2008PhPl...15f2703Y"><span>Extended x-ray absorption fine structure measurements of quasi-isentropically <span class="hlt">compressed</span> vanadium targets on the OMEGA laser</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Yaakobi, B.; Boehly, T. R.; Sangster, T. C.; Meyerhofer, D. D.; Remington, B. A.; Allen, P. G.; Pollaine, S. M.; Lorenzana, H. E.; Lorenz, K. T.; Hawreliak, J. A.</p> <p>2008-06-01</p> <p>The use of in situ extended x-ray absorption fine structure (EXAFS) for characterizing nanosecond laser-<span class="hlt">shocked</span> vanadium, titanium, and <span class="hlt">iron</span> has recently been demonstrated. These measurements are extended to laser-driven, quasi-isentropic <span class="hlt">compression</span> experiments (ICE). The radiation source (backlighter) for EXAFS in all of these experiments is obtained by imploding a spherical target on the OMEGA laser [T. R. Boehly et al., Rev. Sci. Instrum. 66, 508 (1995)]. Isentropic <span class="hlt">compression</span> (where the entropy is kept constant) enables to reach high <span class="hlt">compressions</span> at relatively low temperatures. The absorption spectra are used to determine the temperature and <span class="hlt">compression</span> in a vanadium sample quasi-isentropically <span class="hlt">compressed</span> to pressures of up to ˜0.75Mbar. The ability to measure the temperature and <span class="hlt">compression</span> directly is unique to EXAFS. The drive pressure is calibrated by substituting aluminum for the vanadium and interferometrically measuring the velocity of the back target surface by the velocity interferometer system for any reflector (VISAR). The experimental results obtained by EXAFS and VISAR agree with each other and with the simulations of a hydrodynamic code. The role of a shield to protect the sample from impact heating is studied. It is shown that the shield produces an initial weak <span class="hlt">shock</span> that is followed by a quasi-isentropic <span class="hlt">compression</span> at a relatively low temperature. The role of radiation heating from the imploding target as well as from the laser-absorption region is studied. The results show that in laser-driven ICE, as compared with laser-driven <span class="hlt">shocks</span>, comparable <span class="hlt">compressions</span> can be achieved at lower temperatures. The EXAFS results show important details not seen in the VISAR results.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19830025959','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19830025959"><span>Numerical solutions of Navier-Stokes equations for <span class="hlt">compressible</span> turbulent two/three dimensional flows in terminal <span class="hlt">shock</span> region of an inlet/diffuser</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Liu, N. S.; Shamroth, S. J.; Mcdonald, H.</p> <p>1983-01-01</p> <p>The multidimensional ensemble averaged <span class="hlt">compressible</span> time dependent Navier Stokes equations in conjunction with mixing length turbulence model and <span class="hlt">shock</span> capturing technique were used to study the terminal <span class="hlt">shock</span> type of flows in various flight regimes occurring in a diffuser/inlet model. The numerical scheme for solving the governing equations is based on a linearized block implicit approach and the following high Reynolds number calculations were carried out: (1) 2 D, steady, subsonic; (2) 2 D, steady, transonic with normal <span class="hlt">shock</span>; (3) 2 D, steady, supersonic with terminal <span class="hlt">shock</span>; (4) 2 D, transient process of <span class="hlt">shock</span> development and (5) 3 D, steady, transonic with normal <span class="hlt">shock</span>. The numerical results obtained for the 2 D and 3 D transonic <span class="hlt">shocked</span> flows were compared with corresponding experimental data; the calculated wall static pressure distributions agree well with the measured data.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/22308932-magnetic-particle-time-flight-magptof-diagnostic-measurements-shock-compression-bang-time-nif-invited','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/22308932-magnetic-particle-time-flight-magptof-diagnostic-measurements-shock-compression-bang-time-nif-invited"><span>A magnetic particle time-of-flight (MagPTOF) diagnostic for measurements of <span class="hlt">shock</span>- and <span class="hlt">compression</span>-bang time at the NIF (invited)</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Rinderknecht, H. G., E-mail: hgr@mit.edu; Sio, H.; Frenje, J. A.</p> <p></p> <p>A magnetic particle time-of-flight (MagPTOF) diagnostic has been designed to measure <span class="hlt">shock</span>- and <span class="hlt">compression</span>-bang time using D{sup 3}He-fusion protons and DD-fusion neutrons, respectively, at the National Ignition Facility (NIF). This capability, in combination with <span class="hlt">shock</span>-burn weighted areal density measurements, will significantly constrain the modeling of the implosion dynamics. This design is an upgrade to the existing particle time-of-flight (pTOF) diagnostic, which records bang times using DD or DT neutrons with an accuracy better than ±70 ps [H. G. Rinderknecht et al., Rev. Sci. Instrum. 83, 10D902 (2012)]. The inclusion of a deflecting magnet will increase D{sup 3}He-proton signal-to-background by amore » factor of 1000, allowing for the first time simultaneous measurements of <span class="hlt">shock</span>- and <span class="hlt">compression</span>-bang times in D{sup 3}He-filled surrogate implosions at the NIF.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016AGUFM.P53D..03J','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016AGUFM.P53D..03J"><span>Scaling impact and <span class="hlt">shock-compression</span> response for porous materials: Application to planetary formation</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Jeanloz, R.</p> <p>2016-12-01</p> <p>A thermodynamic model based on the Mie-Grüneisen equation of state does a good job of describing the response of porous materials to impact, so can provide insights into the accretion and cohesion of planetesimals too small to be significantly held together by gravity (e.g., tens of km or less in average diameter). The model identifies an offset in Hugoniot pressure (ΔPH) due to porosity that is found to be in agreement with experimental <span class="hlt">shock-compression</span> measurements for samples having a wide range of initial porosities. Assuming the Grüneisen parameter (γ) is proportional to volume (γ/V = constant), the relative offset in Hugoniot pressure as a function of initial porosity (φ = 1 - V0/V0por) and <span class="hlt">compression</span> (η = 1 - V/V0) is ΔPH/PH = γ0 φ/[2(1 - φ) - γ0 (φ + η(1 - φ))] where subscripts 0 and por represent zero-pressure (non-porous) conditions and a porous sample, respectively. This additional thermal pressure at a given volume is due to the extra internal energy and corresponding temperature increase associated with collapsing pores (Fig. 1: near-identical curves for φ = 0.001 and 0.01). This result can be interpreted as indicating that upon collapse individual pores create hot spots with temperatures of order 103-104K above the background, suggesting that impact into an initially porous target can result in cohesion due to partial melting and vaporization. Moreover, the waste heat associated with pore closure far exceeds the dissipation in <span class="hlt">shock</span> loading of non-porous material, reflecting the ability of a porous target to absorb and dissipate impact energy. The Mie-Grüneisen model along with analysis of waste heat thus provides a scaling for planetesimal impact that might explain how rock and regolith accrete into a gravitationally bound planet. Fig. 1. Porosity-induced anomaly in Hugoniot temperature per unit of porosity, shown as a function of <span class="hlt">compression</span> for samples with initial porosity φ = 0.001 (green), 0.01 (blue) and 0.1 (gold) assuming</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017APS..DPPYO6010M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017APS..DPPYO6010M"><span>The Simultaneous Combination of Phase Contrast Imaging with In Situ X-ray diffraction from <span class="hlt">Shock</span> <span class="hlt">Compressed</span> Matter</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>McBride, Emma Elizabeth; Seiboth, Frank; Cooper, Leora; Frost, Mungo; Goede, Sebastian; Harmand, Marion; Levitan, Abe; McGonegle, David; Miyanishi, Kohei; Ozaki, Norimasa; Roedel, Melanie; Sun, Peihao; Wark, Justin; Hastings, Jerry; Glenzer, Siegfried; Fletcher, Luke</p> <p>2017-10-01</p> <p>Here, we present the simultaneous combination of phase contrast imaging (PCI) techniques with in situ X-ray diffraction to investigate multiple-wave features in laser-driven <span class="hlt">shock-compressed</span> germanium. Experiments were conducted at the Matter at Extreme Conditions end station at the LCLS, and measurements were made perpendicular to the <span class="hlt">shock</span> propagation direction. PCI allows one to take femtosecond snapshots of magnified real-space images of <span class="hlt">shock</span> waves as they progress though matter. X-ray diffraction perpendicular to the <span class="hlt">shock</span> propagation direction provides the opportunity to isolate and identify different waves and determine the crystal structure unambiguously. Here, we combine these two powerful techniques simultaneously, by using the same Be lens setup to focus the fundamental beam at 8.2 keV to a size of 1.5 mm on target for PCI and the 3rd harmonic at 24.6 keV to a spot size of 2 um on target for diffraction.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018ShWav..28...51A','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018ShWav..28...51A"><span>Dynamic loads on human and animal surrogates at different test locations in <span class="hlt">compressed</span>-gas-driven <span class="hlt">shock</span> tubes</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Alay, E.; Skotak, M.; Misistia, A.; Chandra, N.</p> <p>2018-01-01</p> <p>Dynamic loads on specimens in live-fire conditions as well as at different locations within and outside <span class="hlt">compressed</span>-gas-driven <span class="hlt">shock</span> tubes are determined by both static and total blast overpressure-time pressure pulses. The biomechanical loading on the specimen is determined by surface pressures that combine the effects of static, dynamic, and reflected pressures and specimen geometry. Surface pressure is both space and time dependent; it varies as a function of size, shape, and external contour of the specimens. In this work, we used two sets of specimens: (1) anthropometric dummy head and (2) a surrogate rodent headform instrumented with pressure sensors and subjected them to blast waves in the interior and at the exit of the <span class="hlt">shock</span> tube. We demonstrate in this work that while inside the <span class="hlt">shock</span> tube the biomechanical loading as determined by various pressure measures closely aligns with live-fire data and <span class="hlt">shock</span> wave theory, significant deviations are found when tests are performed outside.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19930081326','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19930081326"><span>The <span class="hlt">Compressibility</span> Burble</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Stack, John</p> <p>1935-01-01</p> <p>Simultaneous air-flow photographs and pressure-distribution measurements have been made of the NACA 4412 airfoil at high speeds in order to determine the physical nature of the <span class="hlt">compressibility</span> burble. The flow photographs were obtained by the Schlieren method and the pressures were simultaneously measured for 54 stations on the 5-inch-chord wing by means of a multiple-tube photographic manometer. Pressure-measurement results and typical Schlieren photographs are presented. The general nature of the phenomenon called the "<span class="hlt">compressibility</span> burble" is shown by these experiments. The source of the increased drag is the <span class="hlt">compression</span> <span class="hlt">shock</span> that occurs, the excess drag being due to the conversion of a considerable amount of the air-stream kinetic energy into heat at the <span class="hlt">compression</span> <span class="hlt">shock</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017M%26PS...52.2375M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017M%26PS...52.2375M"><span><span class="hlt">Shock</span>-darkening in ordinary chondrites: Determination of the pressure-temperature conditions by <span class="hlt">shock</span> physics mesoscale modeling</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Moreau, J.; Kohout, T.; Wünnemann, K.</p> <p>2017-11-01</p> <p>We determined the <span class="hlt">shock</span>-darkening pressure range in ordinary chondrites using the iSALE <span class="hlt">shock</span> physics code. We simulated planar <span class="hlt">shock</span> waves on a mesoscale in a sample layer at different nominal pressures. <span class="hlt">Iron</span> and troilite grains were resolved in a porous olivine matrix in the sample layer. We used equations of state (Tillotson EoS and ANEOS) and basic strength and thermal properties to describe the material phases. We used Lagrangian tracers to record the peak <span class="hlt">shock</span> pressures in each material unit. The post-<span class="hlt">shock</span> temperatures (and the fractions of the tracers experiencing temperatures above the melting point) for each material were estimated after the passage of the <span class="hlt">shock</span> wave and after the reflections of the <span class="hlt">shock</span> at grain boundaries in the heterogeneous materials. The results showed that <span class="hlt">shock</span>-darkening, associated with troilite melt and the onset of olivine melt, happened between 40 and 50 GPa with 52 GPa being the pressure at which all tracers in the troilite material reach the melting point. We demonstrate the difficulties of <span class="hlt">shock</span> heating in <span class="hlt">iron</span> and also the importance of porosity. Material impedances, grain shapes, and the porosity models available in the iSALE code are discussed. We also discuss possible not-<span class="hlt">shock</span>-related triggers for <span class="hlt">iron</span> melt.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015APS..DPPCO4003B','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015APS..DPPCO4003B"><span>Probing Hotspot Conditions in Spherically <span class="hlt">Shock</span> <span class="hlt">Compressed</span> Matter</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Bachmann, Benjamin; Nilsen, J.; Kritcher, A. L.; Swift, D.; Rygg, J. R.; Collins, G. W.; Divol, L.; Falcone, R. W.; Gaffney, J.; Glenzer, S. H.; Hatarik, R.; Hawreliak, J.; Khan, S.; Kraus, D.; Landen, O. L.; Masters, N.; Nagel, S. R.; Pardini, T.; Zimmerman, G.; Doeppner, T.</p> <p>2015-11-01</p> <p>We present results of an approach to experimentally determine the conditions in the center of a CD2 sphere that has been <span class="hlt">compressed</span> to petapascal pressures by spherically converging <span class="hlt">shocks</span>. By measuring the hotspot size using penumbral imaging, hotspot temperature using two-color spectroscopy, the neutron yield from DD nuclear reactions and the x-ray burn width, we infer average hotspot densities of 43 g/cm3 at 1.6 keV temperature. These conditions correspond to pressures of 4.4 petapascal (44 Gbar) in an ideal gas and 3.5 petapascal from independently performed rad.-hydro. simulations. The experimentally determined neutron yield, temperature and density constrain the EOS in a regime that exceeds previously reported pressures obtained in carbon EOS measurements by three orders of magnitude. The results show a path for constraining the EOS of matter at conditions that have been inaccessible with state-of-the-art experimental EOS techniques. This work was performed under the auspices of the U.S. DOE by LLNL under Contract DE-AC52-07NA27344 and LDRD Grant 13-ERD-073</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/1998EL.....41..495H','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/1998EL.....41..495H"><span>Experimental observation of the shift and width of the aluminium K absorption edge in laser <span class="hlt">shock-compressed</span> plasmas</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Hall, T. A.; Al-Kuzee, J.; Benuzzi, A.; Koenig, M.; Krishnan, J.; Grandjouan, N.; Batani, D.; Bossi, S.; Nicolella, S.</p> <p>1998-03-01</p> <p>Experimental measurements of the shift and width of the aluminium K-absorption edge in laser <span class="hlt">shock-compressed</span> plasma is presented. The spectrometer used in these experiments allows an accurate wavelength calibration and fiduciary and hence provides precise measurements of both the shift and the width of the absorption edge. Results have been obtained for <span class="hlt">compressions</span> up to approximately ×2 and temperatures up to about 1.5 eV. The values of shift and width are compared with a new model with which there is very good agreement.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19720022153','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19720022153"><span>Digital-computer normal <span class="hlt">shock</span> position and restart control of a Mach 2.5 axisymmetric mixed-<span class="hlt">compression</span> inlet</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Neiner, G. H.; Cole, G. L.; Arpasi, D. J.</p> <p>1972-01-01</p> <p>Digital computer control of a mixed-<span class="hlt">compression</span> inlet is discussed. The inlet was terminated with a choked orifice at the compressor face station to dynamically simulate a turbojet engine. Inlet diffuser exit airflow disturbances were used. A digital version of a previously tested analog control system was used for both normal <span class="hlt">shock</span> and restart control. Digital computer algorithms were derived using z-transform and finite difference methods. Using a sample rate of 1000 samples per second, the digital normal <span class="hlt">shock</span> and restart controls essentially duplicated the inlet analog computer control results. At a sample rate of 100 samples per second, the control system performed adequately but was less stable.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017PhRvB..95v4104Z','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017PhRvB..95v4104Z"><span><span class="hlt">Shock</span>-adiabatic to quasi-isentropic <span class="hlt">compression</span> of warm dense helium up to 150 GPa</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Zheng, J.; Chen, Q. F.; Gu, Y. J.; Li, J. T.; Li, Z. G.; Li, C. J.; Chen, Z. Y.</p> <p>2017-06-01</p> <p>Multiple reverberation <span class="hlt">compression</span> can achieve higher pressure, higher temperature, but lower entropy. It is available to provide an important validation for the elaborate and wider planetary models and simulate the inertial confinement fusion capsule implosion process. In the work, we have developed the thermodynamic and optical properties of helium from <span class="hlt">shock</span>-adiabatic to quasi-isentropic <span class="hlt">compression</span> by means of a multiple reverberation technique. By this technique, the initial dense gaseous helium was <span class="hlt">compressed</span> to high pressure and high temperature and entered the warm dense matter (WDM) region. The experimental equation of state (EOS) of WDM helium in the pressure-density-temperature (P-ρ -T) range of 1 -150 GPa , 0.1 -1.1 g c m-3 , and 4600-24 000 K were measured. The optical radiations emanating from the WDM helium were recorded, and the particle velocity profiles detecting from the sample/window interface were obtained successfully up to 10 times <span class="hlt">compression</span>. The optical radiation results imply that dense He has become rather opaque after the 2nd <span class="hlt">compression</span> with a density of about 0.3 g c m-3 and a temperature of about 1 eV. The opaque states of helium under multiple <span class="hlt">compression</span> were analyzed by the particle velocity measurements. The multiple <span class="hlt">compression</span> technique could efficiently enhanced the density and the <span class="hlt">compressibility</span>, and our multiple <span class="hlt">compression</span> ratios (ηi=ρi/ρ0,i =1 -10 ) of helium are greatly improved from 3.5 to 43 based on initial precompressed density (ρ0) . For the relative <span class="hlt">compression</span> ratio (ηi'=ρi/ρi -1) , it increases with pressure in the lower density regime and reversely decreases in the higher density regime, and a turning point occurs at the 3rd and 4th <span class="hlt">compression</span> states under the different loading conditions. This nonmonotonic evolution of the <span class="hlt">compression</span> is controlled by two factors, where the excitation of internal degrees of freedom results in the increasing <span class="hlt">compressibility</span> and the repulsive interactions between the</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017ExFl...58...64L','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017ExFl...58...64L"><span>MacCormack's technique-based pressure reconstruction approach for PIV data in <span class="hlt">compressible</span> flows with <span class="hlt">shocks</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Liu, Shun; Xu, Jinglei; Yu, Kaikai</p> <p>2017-06-01</p> <p>This paper proposes an improved approach for extraction of pressure fields from velocity data, such as obtained by particle image velocimetry (PIV), especially for steady <span class="hlt">compressible</span> flows with strong <span class="hlt">shocks</span>. The principle of this approach is derived from Navier-Stokes equations, assuming adiabatic condition and neglecting viscosity of flow field boundaries measured by PIV. The computing method is based on MacCormack's technique in computational fluid dynamics. Thus, this approach is called the MacCormack method. Moreover, the MacCormack method is compared with several approaches proposed in previous literature, including the isentropic method, the spatial integration and the Poisson method. The effects of velocity error level and PIV spatial resolution on these approaches are also quantified by using artificial velocity data containing <span class="hlt">shock</span> waves. The results demonstrate that the MacCormack method has higher reconstruction accuracy than other approaches, and its advantages become more remarkable with <span class="hlt">shock</span> strengthening. Furthermore, the performance of the MacCormack method is also validated by using synthetic PIV images with an oblique <span class="hlt">shock</span> wave, confirming the feasibility and advantage of this approach in real PIV experiments. This work is highly significant for the studies on aerospace engineering, especially the outer flow fields of supersonic aircraft and the internal flow fields of ramjets.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017APS..SHK.J8006J','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017APS..SHK.J8006J"><span>Molecular dynamics study of <span class="hlt">shock</span> <span class="hlt">compression</span> in porous silica glass</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Jones, Keith; Lane, J. Matthew D.; Vogler, Tracy J.</p> <p>2017-06-01</p> <p>The <span class="hlt">shock</span> response of porous amorphous silica is investigated using classical molecular dynamics, over a range of porosity ranging from fully dense (2.21 g/cc) down to 0.14 g/cc. We observe an enhanced densification in the Hugoniot response at initial porosities above 50 %, and the effect increases with increasing porosity. In the lowest initial densities, after an initial <span class="hlt">compression</span> response, the systems expand with increased pressure. These results show good agreement with experiments. Mechanisms leading to enhanced densification will be explored, which appear to differ from mechanisms observed in similar studies in silicon. Sandia National Laboratories is a multi mission laboratory managed and operated by Sandia Corporation, a wholly owned subsidiary of Lockheed Martin Corporation, for the U.S. Department of Energy's National Nuclear Security Administration under contract DE-AC04-94AL85000.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/22181498','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/22181498"><span>Converging <span class="hlt">shocks</span> in elastic-plastic solids.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Ortega, A López; Lombardini, M; Hill, D J</p> <p>2011-11-01</p> <p>We present an approximate description of the behavior of an elastic-plastic material processed by a cylindrically or spherically symmetric converging <span class="hlt">shock</span>, following Whitham's <span class="hlt">shock</span> dynamics theory. Originally applied with success to various gas dynamics problems, this theory is presently derived for solid media, in both elastic and plastic regimes. The exact solutions of the <span class="hlt">shock</span> dynamics equations obtained reproduce well the results obtained by high-resolution numerical simulations. The examined constitutive laws share a <span class="hlt">compressible</span> neo-Hookean structure for the internal energy e=e(s)(I(1))+e(h)(ρ,ς), where e(s) accounts for shear through the first invariant of the Cauchy-Green tensor, and e(h) represents the hydrostatic contribution as a function of the density ρ and entropy ς. In the strong-<span class="hlt">shock</span> limit, reached as the <span class="hlt">shock</span> approaches the axis or origin r=0, we show that <span class="hlt">compression</span> effects are dominant over shear deformations. For an isothermal constitutive law, i.e., e(h)=e(h)(ρ), with a power-law dependence e(h) is proportional to ρ(α), <span class="hlt">shock</span> dynamics predicts that for a converging <span class="hlt">shock</span> located at r=R(t) at time t, the Mach number increases as M is proportional to [log(1/R)](α), independently of the space index s, where s=2 in cylindrical geometry and 3 in spherical geometry. An alternative isothermal constitutive law with p(ρ) of the arctanh type, which enforces a finite density in the strong-<span class="hlt">shock</span> limit, leads to M is proportional to R(-(s-1)) for strong <span class="hlt">shocks</span>. A nonisothermal constitutive law, whose hydrostatic part e(h) is that of an ideal gas, is also tested, recovering the strong-<span class="hlt">shock</span> limit M is proportional to R(-(s-1)/n(γ)) originally derived by Whitham for perfect gases, where γ is inherently related to the maximum <span class="hlt">compression</span> ratio that the material can reach, (γ+1)/(γ-1). From these strong-<span class="hlt">shock</span> limits, we also estimate analytically the density, radial velocity, pressure, and sound speed immediately behind the <span class="hlt">shock</span>. While the</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/1036318-laboratory-shock-experiments-basalt-iron-sulfate-mixes-gpa-relevance-martian-reolith-component-present-shergotties','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/1036318-laboratory-shock-experiments-basalt-iron-sulfate-mixes-gpa-relevance-martian-reolith-component-present-shergotties"><span>Laboratory <span class="hlt">Shock</span> Experiments on Basalt - <span class="hlt">Iron</span> Sulfate Mixes at ~ 40 - 50 GPa and their Relevance to the Martian Reolith Component Present in Shergotties</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Rao, M N; Nyquist, L E; Ross, D K</p> <p>2012-03-14</p> <p>Basaltic shergottites such as Shergotty, Zagami and EET79001 contain impact melt glass pockets that are rich in Martian atmospheric gases and are known as gas-rich impact-melt (GRIM) glasses. These glasses show evidence for the presence of a Martian regolith component based on Sm and Kr isotopic studies. The GRIM glasses are sometimes embedded with clusters of innumerable micron-sized <span class="hlt">iron</span>-sulfide blebs associated with minor amounts of <span class="hlt">iron</span> sulfate particles. These sulfide blebs are secondary in origin and are not related to the primary igneous sulfides occurring in Martian meteorites. The material comprising these glasses arises from the highly oxidizing Martian surfacemore » and sulfur is unlikely to occur as sulfide in the Martian regoilith. Instead, sulfur is shown to occur as sulfate based on APXS and Mossbauer results obtained by the Opportunity and Spirit rovers at Meridiani and Gusev. We have earlier suggested that the micron-sized <span class="hlt">iron</span> sulfide globules in GRIM glasses were likely produced by <span class="hlt">shock</span>-reduction of <span class="hlt">iron</span> sulfate occurring in the regolith at the time when the GRIM glasses were produced by the meteoroid impact that launched the Martian meteorites into space. As a result of high energy deposition by <span class="hlt">shock</span> (~ 40-60 GPa), the <span class="hlt">iron</span> sulfate bearing phases are likely to melt along with other regolith components and will get reduced to immiscible sulfide fluid under reducing conditions. On quenching, this generates a dispersion of micron-scale sulfide blebs. The reducing agents in our case are likely to be H 2 and CO which were <span class="hlt">shock</span>-implanted from the Martian atmosphere into these glasses along with the noble gases. We conducted lab simulation experiments in the Lindhurst Laboratory of Experimental Geophysics at Caltech and the Experimental Impact Laboratory at JSC to test whether <span class="hlt">iron</span> sulfide globules can be produced by impact-driven reduction of <span class="hlt">iron</span> sulfate by subjecting Columbia River Basalt (CRB) and ferric sulfate mixtures to <span class="hlt">shock</span> pressures</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/1982AIPC...78..657S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/1982AIPC...78..657S"><span>Sandia 25-meter <span class="hlt">compressed</span> helium/air gun</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Setchell, R. E.</p> <p>1982-04-01</p> <p>For nearly twenty years the Sandia 25-meter <span class="hlt">compressed</span> gas gun has been an important tool for studying condensed materials subjected to transient <span class="hlt">shock</span> <span class="hlt">compression</span>. Major system modifications are now in progress to provide new control, instrumentation, and data acquisition capabilities. These features will ensure that the facility can continue as an effective means of investigating a variety of physical and chemical processes in <span class="hlt">shock-compressed</span> solids.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015SPIE.9543E..1ZF','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015SPIE.9543E..1ZF"><span>Improving friction performance of cast <span class="hlt">iron</span> by laser <span class="hlt">shock</span> peening</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Feng, Xu; Zhou, Jianzhong; Huang, Shu; Sheng, Jie; Mei, Yufen; Zhou, Hongda</p> <p>2015-05-01</p> <p>According to different purpose, some high or low friction coefficient of the material surface is required. In this study, micro-dent texture was fabricated on cast <span class="hlt">iron</span> specimens by a set of laser <span class="hlt">shock</span> peening (LSP) experiments under different laser energy, with different patterns of micro dimples in terms of the depth over diameter. The mechanism of LSP was discussed and surface morphology of the micro dimples were investigated by utilizing a Keyence KS-1100 3D optical surface profilometer. The tests under the conditions of dry and lubricating sliding friction were accomplished on the UMT-2 apparatus. The performance of treated samples during friction and wear tests were characterized and analyzed. Based on theoretical analysis and experimental study, friction performance of textured and untextured samples were studied and compared. Morphological characteristics were observed by scanning electron microscope (SEM) and compared after friction tests under dry condition. The results showed that friction coefficient of textured samples were obvious changed than smooth samples. It can be seen that LSP is an effective way to improve the friction performance of cast <span class="hlt">iron</span> by fabricating high quality micro dimples on its surface, no matter what kind of engineering application mentioned in this paper.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018JCoPh.362..131O','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018JCoPh.362..131O"><span>A simple, robust and efficient high-order accurate <span class="hlt">shock</span>-capturing scheme for <span class="hlt">compressible</span> flows: Towards minimalism</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Ohwada, Taku; Shibata, Yuki; Kato, Takuma; Nakamura, Taichi</p> <p>2018-06-01</p> <p>Developed is a high-order accurate <span class="hlt">shock</span>-capturing scheme for the <span class="hlt">compressible</span> Euler/Navier-Stokes equations; the formal accuracy is 5th order in space and 4th order in time. The performance and efficiency of the scheme are validated in various numerical tests. The main ingredients of the scheme are nothing special; they are variants of the standard numerical flux, MUSCL, the usual Lagrange's polynomial and the conventional Runge-Kutta method. The scheme can compute a boundary layer accurately with a rational resolution and capture a stationary contact discontinuity sharply without inner points. And yet it is endowed with high resistance against <span class="hlt">shock</span> anomalies (carbuncle phenomenon, post-<span class="hlt">shock</span> oscillations, etc.). A good balance between high robustness and low dissipation is achieved by blending three types of numerical fluxes according to physical situation in an intuitively easy-to-understand way. The performance of the scheme is largely comparable to that of WENO5-Rusanov, while its computational cost is 30-40% less than of that of the advanced scheme.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/29573675','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/29573675"><span>Short-term effects of nanoscale Zero-Valent <span class="hlt">Iron</span> (nZVI) and hydraulic <span class="hlt">shock</span> during high-rate anammox wastewater treatment.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Xu, Jia-Jia; Zhang, Zheng-Zhe; Ji, Zheng-Quan; Zhu, Ying-Hong; Qi, Si-Yu; Tang, Chong-Jian; Jin, Ren-Cun</p> <p>2018-06-01</p> <p>The stability and resilience of an anaerobic ammonium oxidation (anammox) system under transient nanoscale Zero-Valent <span class="hlt">Iron</span> (nZVI) (50, 75 and 100 mg L -1 ), hydraulic <span class="hlt">shock</span> (2-fold increase in flow rate) and their combination were studied in an up-flow anaerobic sludge blanket reactor. The response to the <span class="hlt">shock</span> loads can be divided into three phases i.e. <span class="hlt">shock</span>, inertial and recovery periods. The effects of the <span class="hlt">shock</span> loads were directly proportional to the <span class="hlt">shock</span> intensity. The effluent quality was gradually deteriorated after exposure to high nZVI level (100 mg L -1 ) for 2 h. The higher effluent sensitivity index and response caused by unit intensity of <span class="hlt">shock</span> was observed under hydraulic and combined <span class="hlt">shocks</span>. Notably, the specific anammox activity and the content of heme c were considerably reduced during the <span class="hlt">shock</span> phase and the maximum loss rates were about 30.5% and 24.8%, respectively. Nevertheless, the extracellular polymeric substance amount in the <span class="hlt">shock</span> phase was enhanced in varying degrees and variation tendency was disparate at all the tested <span class="hlt">shock</span> loads. These results suggested that robustness of the anammox system was dependent on the magnitude <span class="hlt">shocks</span> applied and the reactor resistance can be improved by reducing hydraulic retention time with the increase of nZVI concentration under these circumstances. Copyright © 2018 Elsevier Ltd. All rights reserved.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_8");'>8</a></li> <li><a href="#" onclick='return showDiv("page_9");'>9</a></li> <li class="active"><span>10</span></li> <li><a href="#" onclick='return showDiv("page_11");'>11</a></li> <li><a href="#" onclick='return showDiv("page_12");'>12</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_10 --> <div id="page_11" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_9");'>9</a></li> <li><a href="#" onclick='return showDiv("page_10");'>10</a></li> <li class="active"><span>11</span></li> <li><a href="#" onclick='return showDiv("page_12");'>12</a></li> <li><a href="#" onclick='return showDiv("page_13");'>13</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="201"> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20120001831','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20120001831"><span>Laboratory <span class="hlt">Shock</span> Experiments on Basalt - <span class="hlt">Iron</span> Sulfate Mixes at Approximately 40-50 GPa and Their Relevance to the Martian Regolith Component Present in Shergottites</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Rao, M. N.; Nyquist, L. E.; Ross, D. K.; Asimow, P. D.; See, T.; Sutton, S.; Cardernas, F.; Montes, R.; Cintala, M.</p> <p>2012-01-01</p> <p>Basaltic shergottites such as Shergotty, Zagami and EET79001 contain impact melt glass pockets that are rich in Martian atmospheric gases [1] and are known as gas-rich impact-melt (GRIM) glasses. These glasses show evidence for the presence of a Martian regolith component based on Sm and Kr isotopic studies [2]. The GRIM glasses are sometimes embedded with clusters of innumerable micron-sized <span class="hlt">iron</span>-sulfide blebs associated with minor amounts of <span class="hlt">iron</span> sulfate particles [3, 4]. These sulfide blebs are secondary in origin and are not related to the primary igneous sulfides occurring in Martian meteorites. The material comprising these glasses arises from the highly oxidizing Martian surface and sulfur is unlikely to occur as sulfide in the Martian regoilith. Instead, sulfur is shown to occur as sulfate based on APXS and Mossbauer results obtained by the Opportunity and Spirit rovers at Meridiani and Gusev [5]. We have earlier suggested that the micron-sized <span class="hlt">iron</span> sulfide globules in GRIM glasses were likely produced by <span class="hlt">shock</span>-reduction of <span class="hlt">iron</span> sulfate occurring in the regolith at the time when the GRIM glasses were produced by the meteoroid impact that launched the Martian meteorites into space [6]. As a result of high energy deposition by <span class="hlt">shock</span> (approx. 40-60 GPa), the <span class="hlt">iron</span> sulfate bearing phases are likely to melt along with other regolith components and will get reduced to immiscible sulfide fluid under reducing conditions. On quenching, this generates a dispersion of micron-scale sulfide blebs. The reducing agents in our case are likely to be H2 and CO which were <span class="hlt">shock</span>-implanted from the Martian atmosphere into these glasses along with the noble gases. We conducted lab simulation experiments in the Lindhurst Laboratory of Experimental Geophysics at Caltech and the Experimental Impact Laboratory at JSC to test whether <span class="hlt">iron</span> sulfide globules can be produced by impact-driven reduction of <span class="hlt">iron</span> sulfate by subjecting Columbia River Basalt (CRB) and ferric sulfate mixtures to</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016APS..DPPBO4010W','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016APS..DPPBO4010W"><span>A platform for detecting material melting from <span class="hlt">shock</span> <span class="hlt">compression</span> using the NIF x-ray diffraction diagnostic TARDIS</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Wehrenberg, Christopher; Kraus, Richard; Braun, Dave; Rygg, Ryan; Coppari, Federica; Lazicki, Amy; McNaney, James; Eggert, Jon</p> <p>2016-10-01</p> <p>A series of experiments were performed on NIF to develop a platform to detect material melting during <span class="hlt">shock</span> <span class="hlt">compression</span> using x-ray diffraction. The unique pulse shaping on NIF can be utilized to directly-drive a steady <span class="hlt">shock</span> into an ablator and material sample while simultaneously creating an x-ray source to probe the material state. Sharp diffraction lines are observed when the material is in the solid state, while broad diffuse lines are seen when in the liquid state, providing an unambiguous signal for <span class="hlt">shock</span> driven melting. Several shots were performed in which a <span class="hlt">shock</span> of 50-80 GPa was driven into a Pb sample while a Ge foil was used as an x-ray source probe. Laser conditions were varied to create a suitable x-ray source that provides a short, bright burst of He-alpha emission from the Ge while maintaining a low background level on the image plates contained in the TARDIS diagnostic. This work was performed under the auspices of the U.S. Department of Energy by Lawrence Livermore National Laboratory under Contract No. DE-AC52-07NA27344.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2012APS..MARZ43002V','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2012APS..MARZ43002V"><span><span class="hlt">Shocks</span> in fragile matter</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Vitelli, Vincenzo</p> <p>2012-02-01</p> <p>Non-linear sound is an extreme phenomenon typically observed in solids after violent explosions. But granular media are different. Right when they unjam, these fragile and disordered solids exhibit vanishing elastic moduli and sound speed, so that even tiny mechanical perturbations form supersonic <span class="hlt">shocks</span>. Here, we perform simulations in which two-dimensional jammed granular packings are continuously <span class="hlt">compressed</span>, and demonstrate that the resulting excitations are strongly nonlinear <span class="hlt">shocks</span>, rather than linear waves. We capture the full dependence of the <span class="hlt">shock</span> speed on pressure and <span class="hlt">compression</span> speed by a surprisingly simple analytical model. We also treat shear <span class="hlt">shocks</span> within a simplified viscoelastic model of nearly-isostatic random networks comprised of harmonic springs. In this case, anharmonicity does not originate locally from nonlinear interactions between particles, as in granular media; instead, it emerges from the global architecture of the network. As a result, the diverging width of the shear <span class="hlt">shocks</span> bears a nonlinear signature of the diverging isostatic length associated with the loss of rigidity in these floppy networks.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4251450','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4251450"><span>A Parametric Approach to Shape Field-Relevant Blast Wave Profiles in <span class="hlt">Compressed</span>-Gas-Driven <span class="hlt">Shock</span> Tube</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Sundaramurthy, Aravind; Chandra, Namas</p> <p>2014-01-01</p> <p> compared with the profiles obtained from the <span class="hlt">shock</span> tube. To conclude, our experimental results demonstrate that a <span class="hlt">compressed</span>-gas <span class="hlt">shock</span> tube when designed and operated carefully can replicate the blast time profiles of field explosions accurately. Such a faithful replication is an essential first step when studying the effects of blast induced neurotrauma using animal models. PMID:25520701</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/22476142-grain-size-dependence-dynamic-mechanical-behavior-az31b-magnesium-alloy-sheet-under-compressive-shock-loading','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/22476142-grain-size-dependence-dynamic-mechanical-behavior-az31b-magnesium-alloy-sheet-under-compressive-shock-loading"><span>Grain size dependence of dynamic mechanical behavior of AZ31B magnesium alloy sheet under <span class="hlt">compressive</span> <span class="hlt">shock</span> loading</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Asgari, H., E-mail: hamed.asgari@usask.ca; Odeshi, A.G.; Szpunar, J.A.</p> <p>2015-08-15</p> <p>The effects of grain size on the dynamic deformation behavior of rolled AZ31B alloy at high strain rates were investigated. Rolled AZ31B alloy samples with grain sizes of 6, 18 and 37 μm, were subjected to <span class="hlt">shock</span> loading tests using Split Hopkinson Pressure Bar at room temperature and at a strain rate of 1100 s{sup −} {sup 1}. It was found that a double-peak basal texture formed in the <span class="hlt">shock</span> loaded samples. The strength and ductility of the alloy under the high strain-rate <span class="hlt">compressive</span> loading increased with decreasing grain size. However, twinning fraction and strain hardening rate were found tomore » decrease with decreasing grain size. In addition, orientation imaging microscopy showed a higher contribution of double and contraction twins in the deformation process of the coarse-grained samples. Using transmission electron microscopy, pyramidal dislocations were detected in the <span class="hlt">shock</span> loaded sample, proving the activation of pyramidal slip system under dynamic impact loading. - Highlights: • A double-peak basal texture developed in all <span class="hlt">shock</span> loaded samples. • Both strength and ductility increased with decreasing grain size. • Twinning fraction and strain hardening rate decreased with decreasing grain size. • ‘g.b’ analysis confirmed the presence of dislocations in <span class="hlt">shock</span> loaded alloy.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19900016618','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19900016618"><span>Interactive calculation procedures for mixed <span class="hlt">compression</span> inlets</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Reshotko, Eli</p> <p>1983-01-01</p> <p>The proper design of engine nacelle installations for supersonic aircraft depends on a sophisticated understanding of the interactions between the boundary layers and the bounding external flows. The successful operation of mixed external-internal <span class="hlt">compression</span> inlets depends significantly on the ability to closely control the operation of the internal <span class="hlt">compression</span> portion of the inlet. This portion of the inlet is one where <span class="hlt">compression</span> is achieved by multiple reflection of oblique <span class="hlt">shock</span> waves and weak <span class="hlt">compression</span> waves in a converging internal flow passage. However weak these <span class="hlt">shocks</span> and waves may seem gas-dynamically, they are of sufficient strength to separate a laminar boundary layer and generally even strong enough for separation or incipient separation of the turbulent boundary layers. An understanding was developed of the viscous-inviscid interactions and of the <span class="hlt">shock</span> wave boundary layer interactions and reflections.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/22410200-sound-velocity-tantalum-under-shock-compression-range','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/22410200-sound-velocity-tantalum-under-shock-compression-range"><span>Sound velocity of tantalum under <span class="hlt">shock</span> <span class="hlt">compression</span> in the 18–142 GPa range</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Xi, Feng, E-mail: xifeng@caep.cn; Jin, Ke; Cai, Lingcang, E-mail: cai-lingcang@aliyun.com</p> <p>2015-05-14</p> <p>Dynamic <span class="hlt">compression</span> experiments of tantalum (Ta) within a <span class="hlt">shock</span> pressure range from 18–142 GPa were conducted driven by explosive, a two-stage light gas gun, and a powder gun, respectively. The time-resolved Ta/LiF (lithium fluoride) interface velocity profiles were recorded with a displacement interferometer system for any reflector. Sound velocities of Ta were obtained from the peak state time duration measurements with the step-sample technique and the direct-reverse impact technique. The uncertainty of measured sound velocities were analyzed carefully, which suggests that the symmetrical impact method with step-samples is more accurate for sound velocity measurement, and the most important parameter in thismore » type experiment is the accurate sample/window particle velocity profile, especially the accurate peak state time duration. From these carefully analyzed sound velocity data, no evidence of a phase transition was found up to the <span class="hlt">shock</span> melting pressure of Ta.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20110013043','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20110013043"><span><span class="hlt">Compressible</span> Flow Toolbox</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Melcher, Kevin J.</p> <p>2006-01-01</p> <p>The <span class="hlt">Compressible</span> Flow Toolbox is primarily a MATLAB-language implementation of a set of algorithms that solve approximately 280 linear and nonlinear classical equations for <span class="hlt">compressible</span> flow. The toolbox is useful for analysis of one-dimensional steady flow with either constant entropy, friction, heat transfer, or Mach number greater than 1. The toolbox also contains algorithms for comparing and validating the equation-solving algorithms against solutions previously published in open literature. The classical equations solved by the <span class="hlt">Compressible</span> Flow Toolbox are as follows: The isentropic-flow equations, The Fanno flow equations (pertaining to flow of an ideal gas in a pipe with friction), The Rayleigh flow equations (pertaining to frictionless flow of an ideal gas, with heat transfer, in a pipe of constant cross section), The normal-<span class="hlt">shock</span> equations, The oblique-<span class="hlt">shock</span> equations, and The expansion equations.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2014GeoRL..41.4554Z','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2014GeoRL..41.4554Z"><span><span class="hlt">Shock</span> <span class="hlt">compression</span> of Fe-Ni-Si system to 280 GPa: Implications for the composition of the Earth's outer core</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Zhang, Youjun; Sekine, Toshimori; He, Hongliang; Yu, Yin; Liu, Fusheng; Zhang, Mingjian</p> <p>2014-07-01</p> <p>The <span class="hlt">shock</span> Hugoniot of an Fe-9 wt %Ni-10 wt %Si system as a model of the Earth's core has been measured up to ~280 GPa using a two-stage light-gas gun. The samples had an average density of 6.853 (±0.036) g/cm3. The relationship between <span class="hlt">shock</span> velocity (Us) and particle velocity (up) can be described by Us (km/s) = 3.95 (±0.15) + 1.53 (±0.05) up (km/s). The calculated Hugoniot temperatures and the melting curve indicate that the model composition melts above a <span class="hlt">shock</span> pressure of ~168 GPa, which is significantly lower than the <span class="hlt">shock</span>-melting pressure of <span class="hlt">iron</span> (~225 GPa). A comparison of the pressure-density (P-ρ) profiles between the model composition and the preliminary reference Earth model gives a silicon content close to 10 wt %, necessary to compensate the density deficit in the Earth's outer core from seismological observations, if silicon is present as a major light element in the Fe-Ni core system.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2006AIPC..845.1139Y','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2006AIPC..845.1139Y"><span>Initiation of Detonation in Multiple <span class="hlt">Shock-Compressed</span> Liquid Explosives</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Yoshinaka, A. C.; Zhang, F.; Petel, O. E.; Higgins, A. J.</p> <p>2006-07-01</p> <p>Initiation and resulting propagation of detonation via multiple <span class="hlt">shock</span> reverberations between two high impedance plates has been investigated in amine-sensitized nitromethane. Experiments were designed so that the first reflected <span class="hlt">shock</span> strength was below the critical value for initiation found previously. Luminosity combined with a distinct pressure hump indicated onset of reaction and successful initiation after double or triple <span class="hlt">shock</span> reflection off the bottom plate. Final temperature estimates for double or triple <span class="hlt">shock</span> reflection immediately before initiation lie between 700-720 K, consistent with those found previously for both incident and singly reflected <span class="hlt">shock</span> initiation.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017GeoRL..44.8712C','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017GeoRL..44.8712C"><span>Dayside response of the magnetosphere to a small <span class="hlt">shock</span> <span class="hlt">compression</span>: Van Allen Probes, Magnetospheric MultiScale, and GOES-13</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Cattell, C.; Breneman, A.; Colpitts, C.; Dombeck, J.; Thaller, S.; Tian, S.; Wygant, J.; Fennell, J.; Hudson, M. K.; Ergun, Robert; Russell, C. T.; Torbert, Roy; Lindqvist, Per-Arne; Burch, J.</p> <p>2017-09-01</p> <p>Observations from Magnetospheric MultiScale ( 8 <fi>Re</fi>) and Van Allen Probes ( 5 and 4 <fi>Re</fi>) show that the initial dayside response to a small interplanetary <span class="hlt">shock</span> is a double-peaked dawnward electric field, which is distinctly different from the usual bipolar (dawnward and then duskward) signature reported for large <span class="hlt">shocks</span>. The associated <fi>E</fi> × <fi>B</fi> flow is radially inward. The <span class="hlt">shock</span> <span class="hlt">compressed</span> the magnetopause to inside 8 <fi>Re</fi>, as observed by Magnetospheric MultiScale (MMS), with a speed that is comparable to the <fi>E</fi> × <fi>B</fi> flow. The magnetopause speed and the <fi>E</fi> × <fi>B</fi> speeds were significantly less than the propagation speed of the pulse from MMS to the Van Allen Probes and GOES-13, which is consistent with the MHD fast mode. There were increased fluxes of energetic electrons up to several MeV. Signatures of drift echoes and response to ULF waves also were seen. These observations demonstrate that even very weak <span class="hlt">shocks</span> can have significant impact on the radiation belts.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20120018047','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20120018047"><span>Quasi One-Dimensional Unsteady Modeling of External <span class="hlt">Compression</span> Supersonic Inlets</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Kopasakis, George; Connolly, Joseph W.; Kratz, Jonathan</p> <p>2012-01-01</p> <p>The AeroServoElasticity task under the NASA Supersonics Project is developing dynamic models of the propulsion system and the vehicle in order to conduct research for integrated vehicle dynamic performance. As part of this effort, a nonlinear quasi 1-dimensional model of an axisymmetric external <span class="hlt">compression</span> supersonic inlet is being developed. The model utilizes <span class="hlt">compressible</span> flow computational fluid dynamics to model the internal inlet segment as well as the external inlet portion between the cowl lip and normal <span class="hlt">shock</span>, and <span class="hlt">compressible</span> flow relations with flow propagation delay to model the oblique <span class="hlt">shocks</span> upstream of the normal <span class="hlt">shock</span>. The external <span class="hlt">compression</span> portion between the cowl-lip and the normal <span class="hlt">shock</span> is also modeled with leaking fluxes crossing the sonic boundary, with a moving CFD domain at the normal <span class="hlt">shock</span> boundary. This model has been verified in steady state against tunnel inlet test data and it s a first attempt towards developing a more comprehensive model for inlet dynamics.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015MS%26E...81a2069A','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015MS%26E...81a2069A"><span>Thermal <span class="hlt">shock</span> removal of defective glass-enamel coating from cast-<span class="hlt">iron</span> products</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Aleutdinov, A. D.; Ghyngazov, S. A.; Mylnikova, T. S.; Luchnikov, P. A.</p> <p>2015-04-01</p> <p>A setup for light beam exposure has been developed. The setup was used to consider the technology of thermal <span class="hlt">shock</span> destruction of the coating by pulsed-periodic exposure to powerful focused light from the xenon arc lamp DKsShRB-10000. It is shown that this type of exposure can effectively remove the glass-enamel coating from <span class="hlt">iron</span> products. The optimal mode of setup operation to efficiently remove the defective glass-enamel coating is found: the diameter of the focused light beams is 2.5-3.5 cm; the lamp arc pulse current is 350-450 A; pulse duration is (0.5-1) s and pulse repetition frequency is (0.15-0.5) s-1.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/1986dyex.coll..155G','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/1986dyex.coll..155G"><span>Normal <span class="hlt">shock</span> wave reflection on porous <span class="hlt">compressible</span> material</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Gvozdeva, L. G.; Faresov, Iu. M.; Brossard, J.; Charpentier, N.</p> <p></p> <p>The present experimental investigation of the interaction of plane <span class="hlt">shock</span> waves in air and a rigid wall coated with flat layers of expanded polymers was conducted in a standard <span class="hlt">shock</span> tube and a diaphragm with an initial test section pressure of 100,000 Pa. The Mach number of the incident <span class="hlt">shock</span> wave was varied from 1.1 to 2.7; the peak pressures measured on the wall behind polyurethane at various incident wave Mach numbers are compared with calculated values, with the ideal model of propagation, and with the reflection of <span class="hlt">shock</span> waves in a porous material that is understood as a homogeneous mixture. The effect of elasticity and permeability of the porous material structure on the rigid wall's pressure pulse parameters is qualitatively studied.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015APS..DPPYI2006K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015APS..DPPYI2006K"><span>Nanometer-scale characterization of laser-driven plasmas, <span class="hlt">compression</span>, <span class="hlt">shocks</span> and phase transitions, by coherent small angle x-ray scattering</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Kluge, Thomas</p> <p>2015-11-01</p> <p>Combining ultra-intense short-pulse and high-energy long-pulse lasers, with brilliant coherent hard X-ray FELs, such as the Helmholtz International Beamline for Extreme Fields (HIBEF) under construction at the HED Instrument of European XFEL, or MEC at LCLS, holds the promise to revolutionize our understanding of many High Energy Density Physics phenomena. Examples include the relativistic electron generation, transport, and bulk plasma response, and ionization dynamics and heating in relativistic laser-matter interactions, or the dynamics of laser-driven <span class="hlt">shocks</span>, quasi-isentropic <span class="hlt">compression</span>, and the kinetics of phase transitions at high pressure. A particularly promising new technique is the use of coherent X-ray diffraction to characterize electron density correlations, and by resonant scattering to characterize the distribution of specific charge-state ions, either on the ultrafast time scale of the laser interaction, or associated with hydrodynamic motion. As well one can image slight density changes arising from phase transitions inside of <span class="hlt">shock-compressed</span> high pressure matter. The feasibility of coherent diffraction techniques in laser-driven matter will be discussed. including recent results from demonstration experiments at MEC. Among other things, very sharp density changes from laser-driven <span class="hlt">compression</span> are observed, having an effective step width of 10 nm or smaller. This compares to a resolution of several hundred nm achievedpreviously with phase contrast imaging. and on behalf of HIBEF User Consortium, for the Helmholtz International Beamline for Extreme Fields at the European XFEL.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2008AGUFMMR32B..04A','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2008AGUFMMR32B..04A"><span><span class="hlt">Shock</span> <span class="hlt">compression</span> of liquid silicates to 125 GPa: the anorthite-diopside join</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Asimow, P. D.; Ahrens, T. J.</p> <p>2008-12-01</p> <p><span class="hlt">Shock</span> <span class="hlt">compression</span> of pre-heated liquid silicates provides, at present, the only method for direct measurement of the equation of state of such liquids at lower mantle pressures. At previous AGU meetings we have reported the extension of the pre-heated Hugoniot of the anorthite-diopside eutectic composition Di64An36, initially at 1673 K, to 110 GPa, along with a determination of the density dependence of the Grüneisen parameter of this liquid composition. We have now completed this work by: (1) extending the Di64An36 data to 127 GPa; (2) measuring the diopside (CaMgSi2O6) end-member composition, initially at 1773 K, to 114 GPa; and (3) measuring the anorthite (CaAl2Si2O8) end-member composition, initially at 1923 K, to 125 GPa. For internal consistency we have also re-reduced all of the experiments reported by Rigden et al. (1984, 1988, 1989) as well as some unpublished data from that era, using the latest initial melt densities (Lange, 1997) and hot Mo equation of state (Asimow et al., 2008). We are now in a position to assess the <span class="hlt">compression</span> behavior of each of these liquids and the model of linear mixing along the compositional join to all pressures relevant to the terrestrial mantle. The total data set for the Di64An36 and diopside compositions can be fit within error by straight line Hugoniots in particle velocity vs. <span class="hlt">shock</span> velocity. This suggests that a 3rd order equation of state is adequate to describe <span class="hlt">compression</span> of these liquids over large pressure ranges. Anorthite, on the other hand, clearly requires a more complex model, such as we require for MgSiO3 and Mg2SiO4 liquids (Mosenfelder, Asimow, and Ahrens; this meeting); we examine the 4th-order Birch-Murnaghan and Ghiorso equations of state as well as an explicit speciation model that accounts for continuous coordination change of Si and Al. The complexity of anorthite liquid <span class="hlt">compression</span> causes an apparent failure of linear mixing, suggesting that calibration of a predictive model of the equation of</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/1234625','SCIGOV-STC'); return false;" href="https://www.osti.gov/servlets/purl/1234625"><span>Stabilization of high-<span class="hlt">compression</span>, indirect-drive inertial confinement fusion implosions using a 4-<span class="hlt">shock</span> adiabat-shaped drive</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>MacPhee, A. G.; Peterson, J. L.; Casey, D. T.</p> <p></p> <p>Hydrodynamic instabilities and poor fuel <span class="hlt">compression</span> are major factors for capsule performance degradation in ignition experiments on the National Ignition Facility. Using a recently developed laser drive profile with a decaying first <span class="hlt">shock</span> to tune the ablative Richtmyer-Meshkov (ARM) instability and subsequent in-flight Rayleigh-Taylor growth, we have demonstrated reduced growth compared to the standard ignition pulse whilst maintaining conditions for a low fuel adiabat needed for increased <span class="hlt">compression</span>. Here, using in-flight x-ray radiography of pre-machined modulations, the first growth measurements using this new ARM-tuned drive have demonstrated instability growth reduction of ~4× compared to the original design at a convergencemore » ratio of ~2. Corresponding simulations give a fuel adiabat of ~1.6, similar to the original goal and consistent with ignition requirements.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1234625-stabilization-high-compression-indirect-drive-inertial-confinement-fusion-implosions-using-shock-adiabat-shaped-drive','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1234625-stabilization-high-compression-indirect-drive-inertial-confinement-fusion-implosions-using-shock-adiabat-shaped-drive"><span>Stabilization of high-<span class="hlt">compression</span>, indirect-drive inertial confinement fusion implosions using a 4-<span class="hlt">shock</span> adiabat-shaped drive</span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>MacPhee, A. G.; Peterson, J. L.; Casey, D. T.; ...</p> <p>2015-08-01</p> <p>Hydrodynamic instabilities and poor fuel <span class="hlt">compression</span> are major factors for capsule performance degradation in ignition experiments on the National Ignition Facility. Using a recently developed laser drive profile with a decaying first <span class="hlt">shock</span> to tune the ablative Richtmyer-Meshkov (ARM) instability and subsequent in-flight Rayleigh-Taylor growth, we have demonstrated reduced growth compared to the standard ignition pulse whilst maintaining conditions for a low fuel adiabat needed for increased <span class="hlt">compression</span>. Here, using in-flight x-ray radiography of pre-machined modulations, the first growth measurements using this new ARM-tuned drive have demonstrated instability growth reduction of ~4× compared to the original design at a convergencemore » ratio of ~2. Corresponding simulations give a fuel adiabat of ~1.6, similar to the original goal and consistent with ignition requirements.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19970013371&hterms=mechanical+rocks&qs=N%3D0%26Ntk%3DAll%26Ntx%3Dmode%2Bmatchall%26Ntt%3Dmechanical%2Brocks','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19970013371&hterms=mechanical+rocks&qs=N%3D0%26Ntk%3DAll%26Ntx%3Dmode%2Bmatchall%26Ntt%3Dmechanical%2Brocks"><span>Mechanical Properties of <span class="hlt">Shock</span>-Damaged Rocks</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>He, Hongliang; Ahrens, T. J.</p> <p>1994-01-01</p> <p>Stress-strain tests were performed both on <span class="hlt">shock</span>-damaged gabbro and limestone. The effective Young's modulus decreases with increasing initial damage parameter value, and an apparent work-softening process occurs prior to failure. To further characterize <span class="hlt">shock</span>-induced microcracks, the longitudinal elastic wave velocity behavior of <span class="hlt">shock</span>-damaged gabbro in the direction of <span class="hlt">compression</span> up to failure was measured using an acoustic transmission technique under uniaxial loading. A dramatic increase in velocity was observed for the static <span class="hlt">compressive</span> stress range of 0-50 MPa. Above that stress range, the velocity behavior of lightly damaged (D(sub 0) less than 0.1) gabbro is almost equal to unshocked gabbro. The failure strength of heavily-damaged (D(sub 0) greater than 0.1) gabbro is approx. 100-150 MPa, much lower than that of lightly damaged and unshocked gabbros (approx. 230-260 MPa). Following Nur's theory, the crack shape distribution was analyzed. The <span class="hlt">shock</span>-induced cracks in gabbro appear to be largely thin penny-shaped cracks with c/a values below 5 x 10(exp -4). Moreover, the applicability of Ashby and Sammis's theory relating failure strength and damage parameter of <span class="hlt">shock</span>-damaged rocks was examined and was found to yield a good estimate of the relation of <span class="hlt">shock</span>-induced deficit in elastic modulus with the deficit in <span class="hlt">compressive</span> strength.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018JAP...123r5902G','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018JAP...123r5902G"><span>Quasi-isentropic <span class="hlt">compression</span> using <span class="hlt">compressed</span> water flow generated by underwater electrical explosion of a wire array</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Gurovich, V.; Virozub, A.; Rososhek, A.; Bland, S.; Spielman, R. B.; Krasik, Ya. E.</p> <p>2018-05-01</p> <p>A major experimental research area in material equation-of-state today involves the use of off-Hugoniot measurements rather than <span class="hlt">shock</span> experiments that give only Hugoniot data. There is a wide range of applications using quasi-isentropic <span class="hlt">compression</span> of matter including the direct measurement of the complete isentrope of materials in a single experiment and minimizing the heating of flyer plates for high-velocity <span class="hlt">shock</span> measurements. We propose a novel approach to generating quasi-isentropic <span class="hlt">compression</span> of matter. Using analytical modeling and hydrodynamic simulations, we show that a working fluid composed of <span class="hlt">compressed</span> water, generated by an underwater electrical explosion of a planar wire array, might be used to efficiently drive the quasi-isentropic <span class="hlt">compression</span> of a copper target to pressures ˜2 × 1011 Pa without any complex target designs.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_9");'>9</a></li> <li><a href="#" onclick='return showDiv("page_10");'>10</a></li> <li class="active"><span>11</span></li> <li><a href="#" onclick='return showDiv("page_12");'>12</a></li> <li><a href="#" onclick='return showDiv("page_13");'>13</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_11 --> <div id="page_12" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_10");'>10</a></li> <li><a href="#" onclick='return showDiv("page_11");'>11</a></li> <li class="active"><span>12</span></li> <li><a href="#" onclick='return showDiv("page_13");'>13</a></li> <li><a href="#" onclick='return showDiv("page_14");'>14</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="221"> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015JCoPh.280..489H','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015JCoPh.280..489H"><span>A new limiting procedure for discontinuous Galerkin methods applied to <span class="hlt">compressible</span> multiphase flows with <span class="hlt">shocks</span> and interfaces</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Henry de Frahan, Marc T.; Varadan, Sreenivas; Johnsen, Eric</p> <p>2015-01-01</p> <p>Although the Discontinuous Galerkin (DG) method has seen widespread use for <span class="hlt">compressible</span> flow problems in a single fluid with constant material properties, it has yet to be implemented in a consistent fashion for <span class="hlt">compressible</span> multiphase flows with <span class="hlt">shocks</span> and interfaces. Specifically, it is challenging to design a scheme that meets the following requirements: conservation, high-order accuracy in smooth regions and non-oscillatory behavior at discontinuities (in particular, material interfaces). Following the interface-capturing approach of Abgrall [1], we model flows of multiple fluid components or phases using a single equation of state with variable material properties; discontinuities in these properties correspond to interfaces. To represent <span class="hlt">compressible</span> phenomena in solids, liquids, and gases, we present our analysis for equations of state belonging to the Mie-Grüneisen family. Within the DG framework, we propose a conservative, high-order accurate, and non-oscillatory limiting procedure, verified with simple multifluid and multiphase problems. We show analytically that two key elements are required to prevent spurious pressure oscillations at interfaces and maintain conservation: (i) the transport equation(s) describing the material properties must be solved in a non-conservative weak form, and (ii) the suitable variables must be limited (density, momentum, pressure, and appropriate properties entering the equation of state), coupled with a consistent reconstruction of the energy. Further, we introduce a physics-based discontinuity sensor to apply limiting in a solution-adaptive fashion. We verify this approach with one- and two-dimensional problems with <span class="hlt">shocks</span> and interfaces, including high pressure and density ratios, for fluids obeying different equations of state to illustrate the robustness and versatility of the method. The algorithm is implemented on parallel graphics processing units (GPU) to achieve high speedup.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20130010181','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20130010181"><span>Exhaust Nozzle Plume and <span class="hlt">Shock</span> Wave Interaction</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Castner, Raymond S.; Elmiligui, Alaa; Cliff, Susan</p> <p>2013-01-01</p> <p>Fundamental research for sonic boom reduction is needed to quantify the interaction of <span class="hlt">shock</span> waves generated from the aircraft wing or tail surfaces with the exhaust plume. Both the nozzle exhaust plume shape and the tail <span class="hlt">shock</span> shape may be affected by an interaction that may alter the vehicle sonic boom signature. The plume and <span class="hlt">shock</span> interaction was studied using Computational Fluid Dynamics simulation on two types of convergent-divergent nozzles and a simple wedge <span class="hlt">shock</span> generator. The nozzle plume effects on the lower wedge <span class="hlt">compression</span> region are evaluated for two- and three-dimensional nozzle plumes. Results show that the <span class="hlt">compression</span> from the wedge deflects the nozzle plume and <span class="hlt">shocks</span> form on the deflected lower plume boundary. The sonic boom pressure signature of the wedge is modified by the presence of the plume, and the computational predictions show significant (8 to 15 percent) changes in <span class="hlt">shock</span> amplitude.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2003AGUFM.B52B1034W','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2003AGUFM.B52B1034W"><span>Bugbuster: Survivability of Living Bacteria Upon <span class="hlt">Shock</span> <span class="hlt">Compression</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Willis, M. J.; Ahrens, T. J.; Bertani, L. E.; Nash, C. Z.</p> <p>2003-12-01</p> <p>Survivability of bacteria during impact events has implications both for the transport of life between planets and development of organisms on Hadean Earth and other planets during the period of heavy bombardment which ended 3.5 Gyr before the present [1]. We envision that life existed within internal rock surfaces immersed in the early ocean. We performed <span class="hlt">shock</span> recovery experiments on live E. coli bacteria to determine survival rate vs. <span class="hlt">shock</span> pressure. Samples of 2x107 cells were suspended in ˜10-5 l of a buffer solution (TE: a 10:1 solution of Tris and EDTA), sealed into stainless steel chambers that are impacted by 1.5 mm thick flyer plates at 670-760 m s-1 using a 20 mm gun. Recovered liquid was mixed with a nutrient broth (LB: growth medium containing tryptone, yeast extract and NaCl) and spread on a Petrie dish containing agar (a polysaccharide growth medium extracted from marine algae Rhodophyceae). Recovered samples were cultured for ˜16 hours at 37° C. In addition, sample bacteria studied under an optical microscope with DAPI fluorescent stain to verify presence of bacteria in <span class="hlt">shock</span> recovered samples. Initial and reverberated <span class="hlt">shock</span> pressures in H2O varied from 0.2 to 2.0 and 2.4 to 14.9 GPa respectively. We modeled the bacteria cell walls with stilbene, ρ 0=1.16 g cm-3, US=2.866+1.588uP and the cell interiors as water. Upon initial loading the net strain imposed on E. coli that just caused non-survival for 10-6 s duration stress was 2.8. If this strain is characteristic of that tolerable by E. coli, we predict that <span class="hlt">shock</span> stresses of 25 MPa, 25 kPa and 25 Pa are sustainable upon <span class="hlt">shock</span> loading by 0.1 ms, 0.1 s and 100 s <span class="hlt">shock</span> duration pulses. Such <span class="hlt">shock</span> durations are induced by 2.5 m, 2.5 km and 2,500 km diameter silicate impactors. References: [1] Maher K.A. & Stevenson D.J., Nature, 331, pp.612-614, 1988</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2005ChPhL..22..747L','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2005ChPhL..22..747L"><span>Shear Viscosity of Aluminium under <span class="hlt">Shock</span> <span class="hlt">Compression</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Liu, Fu-Sheng; Yang, Mei-Xia; Liu, Qi-Wen; Chen, Jun-Xiang; Jing, Fu-Qian</p> <p>2005-03-01</p> <p>Based on the Newtonian viscous fluid model and the analytic perturbation theory of Miller and Ahrens for the oscillatory damping of a sinusoidal <span class="hlt">shock</span> front, a flyer-impact technique is developed to investigate the effective viscosity of <span class="hlt">shocked</span> aluminium. The shear viscosity coefficient is determined to be about 5000 poises at 42 GPa with strain rate of 1.27×106 s-1, which is a reasonable estimation compared with the results of other measurement methods.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2010cosp...38.2101K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2010cosp...38.2101K"><span>Extended fusion yield integral using pathway idea in case of <span class="hlt">Shock-compressed</span> heated plasma</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Kumar, Dilip; Haubold, Hans</p> <p></p> <p>The extended non-resonant thermonuclear reaction rate probability integral obtained in Haubold and Kumar [Haubold, H.J. and Kumar, D.: 2008, Extension of thermonuclear functions through the pathway model including Maxwell-Boltzmann and Tsallis distributions, Astroparticle Physics, 29, 70-76] is used to evaluate the fusion energy by itegrating it over temperature. The closed form representation of the extended reaction rate integral via Meijer's G-function is expressed as a solution of a homogeneous differential equation. A physical model of Guderley[Guderley G. :1942, Starke kugelige und zylindrische Verdichtungsstsse in der Nhe des Kugelmittelpunktes bzw. der Zylinderachse, Luftfahrtforschung, 19, 302] has been considered for the laser driven hydrodynamical process in a <span class="hlt">compressed</span> fusion plasma and heated strong spherical <span class="hlt">shock</span> wave. The fusion yield integral obtained in the paper is compared with the standard fusion yield ob-tained by Haubold and John [Haubold, H.J. and John, R.W.:1981, Analytical representation of the thermonuclear reaction rate and fusion energy production in a spherical plasma <span class="hlt">shock</span> wave, Plasma Physics, 5, 399-411]. The pathway parameter used in this paper is given an interpretation in terms of moments.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/22490022-stabilization-high-compression-indirect-drive-inertial-confinement-fusion-implosions-using-shock-adiabat-shaped-drive','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/22490022-stabilization-high-compression-indirect-drive-inertial-confinement-fusion-implosions-using-shock-adiabat-shaped-drive"><span>Stabilization of high-<span class="hlt">compression</span>, indirect-drive inertial confinement fusion implosions using a 4-<span class="hlt">shock</span> adiabat-shaped drive</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>MacPhee, A. G.; Peterson, J. L.; Casey, D. T.</p> <p></p> <p>Hydrodynamic instabilities and poor fuel <span class="hlt">compression</span> are major factors for capsule performance degradation in ignition experiments on the National Ignition Facility. Using a recently developed laser drive profile with a decaying first <span class="hlt">shock</span> to tune the ablative Richtmyer-Meshkov (ARM) instability and subsequent in-flight Rayleigh-Taylor growth, we have demonstrated reduced growth compared to the standard ignition pulse whilst maintaining conditions for a low fuel adiabat needed for increased <span class="hlt">compression</span>. Using in-flight x-ray radiography of pre-machined modulations, the first growth measurements using this new ARM-tuned drive have demonstrated instability growth reduction of ∼4× compared to the original design at a convergence ratiomore » of ∼2. Corresponding simulations give a fuel adiabat of ∼1.6, similar to the original goal and consistent with ignition requirements.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015JAP...117k5902P','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015JAP...117k5902P"><span>Molecular dynamics simulations of <span class="hlt">shock</span> <span class="hlt">compressed</span> heterogeneous materials. II. The graphite/diamond transition case for astrophysics applications</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Pineau, N.; Soulard, L.; Colombet, L.; Carrard, T.; Pellé, A.; Gillet, Ph.; Clérouin, J.</p> <p>2015-03-01</p> <p>We present a series of molecular dynamics simulations of the <span class="hlt">shock</span> <span class="hlt">compression</span> of copper matrices containing a single graphite inclusion: these model systems can be related to some specific carbon-rich rocks which, after a meteoritic impact, are found to contain small fractions of nanodiamonds embedded in graphite in the vicinity of high impedance minerals. We show that the graphite to diamond transformation occurs readily for nanometer-sized graphite inclusions, via a <span class="hlt">shock</span> accumulation process, provided the pressure threshold of the bulk graphite/diamond transition is overcome, independently of the shape or size of the inclusion. Although high diamond yields (˜80%) are found after a few picoseconds in all cases, the transition is non-isotropic and depends substantially on the relative orientation of the graphite stack with respect to the <span class="hlt">shock</span> propagation, leading to distinct nucleation processes and size-distributions of the diamond grains. A substantial regraphitization process occurs upon release and only inclusions with favorable orientations likely lead to the preservation of a fraction of this diamond phase. These results agree qualitatively well with the recent experimental observations of meteoritic impact samples.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2006APS..DFD.AN012R','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2006APS..DFD.AN012R"><span>Experimental Study of <span class="hlt">Shock</span>-Induced <span class="hlt">Compression</span> and Vortex Generation in the <span class="hlt">Shock</span>-Bubble Interaction</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Ranjan, Devesh; Motl, Bradley; Niederhaus, John; Oakley, Jason; Anderson, Mark; Bonazza, Riccardo; Greenough, Jeffrey</p> <p>2006-11-01</p> <p>Results are presented from experiments studying the interaction of a planar <span class="hlt">shock</span> wave of strength 1.4 <M < 3.0 with a spherical soap bubble composed of helium. Experiments are performed in a 9.2-m-long vertical <span class="hlt">shock</span> tube with a square internal cross-section, 0.254 m on a side, equipped with a pneumatically driven retracting bubble injector. The absence of a bubble holder during <span class="hlt">shock</span> wave passage allows for a cleaner initial condition while avoiding complications associated with holder/<span class="hlt">shock</span> interaction. As the planar <span class="hlt">shock</span> passes over the bubble, the intense vortical and nonlinear acoustic phenomena characterized initially by Haas and Sturtevant (J. Fluid. Mech., 1987) are observed, including vortex ring formation, intense mixing, and growth of turbulence-like features. Flow visualizations are obtained using planar laser diagnostics rather than integral measures. The origin and growth of distinctive counter-rotating secondary vortical features are observed in high Mach number experiments. A number of features of the <span class="hlt">shock</span> bubble interaction are investigated and parameterized with the incident M and the initial density difference. These include the axial and lateral extents of the bubble, the translational velocity of the bubble and associated vortex rings, and the circulation of the vortex rings.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://www.dtic.mil/docs/citations/AD0842761','DTIC-ST'); return false;" href="http://www.dtic.mil/docs/citations/AD0842761"><span>Strain Gage Measurements of Aft Nacelle <span class="hlt">Shock</span> Absorbers.</span></a></p> <p><a target="_blank" href="http://www.dtic.mil/">DTIC Science & Technology</a></p> <p></p> <p></p> <p>ENGINE NACELLES, <span class="hlt">SHOCK</span> ABSORBERS ), (* <span class="hlt">SHOCK</span> ABSORBERS , STRESSES), SURFACE TO SURFACE MISSILES, LAUNCHING, STRAIN GAGES, <span class="hlt">COMPRESSIVE</span> PROPERTIES, CALIBRATION, STRAIN(MECHANICS), FAILURE, GROUND SUPPORT EQUIPMENT.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2003RScI...74.1929K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2003RScI...74.1929K"><span>Multiple film plane diagnostic for <span class="hlt">shocked</span> lattice measurements (invited)</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Kalantar, Daniel H.; Bringa, E.; Caturla, M.; Colvin, J.; Lorenz, K. T.; Kumar, M.; Stölken, J.; Allen, A. M.; Rosolankova, K.; Wark, J. S.; Meyers, M. A.; Schneider, M.; Boehly, T. R.</p> <p>2003-03-01</p> <p>Laser-based <span class="hlt">shock</span> experiments have been conducted in thin Si and Cu crystals at pressures above the Hugoniot elastic limit. In these experiments, static film and x-ray streak cameras recorded x rays diffracted from lattice planes both parallel and perpendicular to the <span class="hlt">shock</span> direction. These data showed uniaxial <span class="hlt">compression</span> of Si(100) along the <span class="hlt">shock</span> direction and three-dimensional <span class="hlt">compression</span> of Cu(100). In the case of the Si diffraction, there was a multiple wave structure observed, which may be due to a one-dimensional phase transition or a time variation in the <span class="hlt">shock</span> pressure. A new film-based detector has been developed for these in situ dynamic diffraction experiments. This large-angle detector consists of three film cassettes that are positioned to record x rays diffracted from a <span class="hlt">shocked</span> crystal anywhere within a full π steradian. It records x rays that are diffracted from multiple lattice planes both parallel and at oblique angles with respect to the <span class="hlt">shock</span> direction. It is a time-integrating measurement, but time-resolved data may be recorded using a short duration laser pulse to create the diffraction source x rays. This new instrument has been fielded at the OMEGA and Janus lasers to study single-crystal materials <span class="hlt">shock</span> <span class="hlt">compressed</span> by direct laser irradiation. In these experiments, a multiple wave structure was observed on many different lattice planes in Si. These data provide information on the structure under <span class="hlt">compression</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2013PhPl...20e6315P','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2013PhPl...20e6315P"><span>Radiative <span class="hlt">shocks</span> produced from spherical cryogenic implosions at the National Ignition Facilitya)</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Pak, A.; Divol, L.; Gregori, G.; Weber, S.; Atherton, J.; Bennedetti, R.; Bradley, D. K.; Callahan, D.; Casey, D. T.; Dewald, E.; Döppner, T.; Edwards, M. J.; Frenje, J. A.; Glenn, S.; Grim, G. P.; Hicks, D.; Hsing, W. W.; Izumi, N.; Jones, O. S.; Johnson, M. G.; Khan, S. F.; Kilkenny, J. D.; Kline, J. L.; Kyrala, G. A.; Lindl, J.; Landen, O. L.; Le Pape, S.; Ma, T.; MacPhee, A.; MacGowan, B. J.; MacKinnon, A. J.; Masse, L.; Meezan, N. B.; Moody, J. D.; Olson, R. E.; Ralph, J. E.; Robey, H. F.; Park, H.-S.; Remington, B. A.; Ross, J. S.; Tommasini, R.; Town, R. P. J.; Smalyuk, V.; Glenzer, S. H.; Moses, E. I.</p> <p>2013-05-01</p> <p>Spherically expanding radiative <span class="hlt">shock</span> waves have been observed from inertially confined implosion experiments at the National Ignition Facility. In these experiments, a spherical fusion target, initially 2 mm in diameter, is <span class="hlt">compressed</span> via the pressure induced from the ablation of the outer target surface. At the peak <span class="hlt">compression</span> of the capsule, x-ray and nuclear diagnostics indicate the formation of a central core, with a radius and ion temperature of ˜20 μm and ˜ 2 keV, respectively. This central core is surrounded by a cooler <span class="hlt">compressed</span> shell of deuterium-tritium fuel that has an outer radius of ˜40 μm and a density of >500 g/cm3. Using inputs from multiple diagnostics, the peak pressure of the <span class="hlt">compressed</span> core has been inferred to be of order 100 Gbar for the implosions discussed here. The <span class="hlt">shock</span> front, initially located at the interface between the high pressure <span class="hlt">compressed</span> fuel shell and surrounding in-falling low pressure ablator plasma, begins to propagate outwards after peak <span class="hlt">compression</span> has been reached. Approximately 200 ps after peak <span class="hlt">compression</span>, a ring of x-ray emission created by the limb-brightening of a spherical shell of <span class="hlt">shock</span>-heated matter is observed to appear at a radius of ˜100 μm. Hydrodynamic simulations, which model the experiment and include radiation transport, indicate that the sudden appearance of this emission occurs as the post-<span class="hlt">shock</span> material temperature increases and upstream density decreases, over a scale length of ˜10 μm, as the <span class="hlt">shock</span> propagates into the lower density (˜1 g/cc), hot (˜250 eV) plasma that exists at the ablation front. The expansion of the <span class="hlt">shock</span>-heated matter is temporally and spatially resolved and indicates a <span class="hlt">shock</span> expansion velocity of ˜300 km/s in the laboratory frame. The magnitude and temporal evolution of the luminosity produced from the <span class="hlt">shock</span>-heated matter was measured at photon energies between 5.9 and 12.4 keV. The observed radial <span class="hlt">shock</span> expansion, as well as the magnitude and temporal evolution of</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/952569-al-absorption-spectroscopy-shock-wave-heating-compression-laser-driven-planar-foil','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/952569-al-absorption-spectroscopy-shock-wave-heating-compression-laser-driven-planar-foil"><span>Al 1s-2p Absorption Spectroscopy of <span class="hlt">Shock</span>-Wave Heating and <span class="hlt">Compression</span> in Laser-Driven Planar Foil</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Sawada, H.; Regan, S.P.; Radha, P.B.</p> <p></p> <p>Time-resolved Al 1s-2p absorption spectroscopy is used to diagnose direct-drive, <span class="hlt">shock</span>-wave heating and <span class="hlt">compression</span> of planar targets having nearly Fermi-degenerate plasma conditions (Te ~ 10–40 eV, rho ~ 3–11 g/cm^3) on the OMEGA Laser System [T. R. Boehly et al., Opt. Commun. 133, 495 (1997)]. A planar plastic foil with a buried Al tracer layer was irradiated with peak intensities of 10^14–10^15 W/cm^2 and probed with the pseudocontinuum M-band emission from a point-source Sm backlighter in the range of 1.4–1.7 keV. The laser ablation process launches 10–70 Mbar <span class="hlt">shock</span> waves into the CH/Al/CH target. The Al 1s-2p absorption spectra weremore » analyzed using the atomic physic code PRISMSPECT to infer Te and rho in the Al layer, assuming uniform plasma conditions during <span class="hlt">shock</span>-wave heating, and to determine when the heat front penetrated the Al layer. The drive foils were simulated with the one-dimensional hydrodynamics code LILAC using a flux-limited (f =0.06 and f =0.1) and nonlocal thermal-transport model [V. N. Goncharov et al., Phys. Plasmas 13, 012702 (2006)]. The predictions of simulated <span class="hlt">shock</span>-wave heating and the timing of heat-front penetration are compared to the observations. The experimental results for a wide variety of laser-drive conditions and buried depths have shown that the LILAC predictions using f = 0.06 and the nonlocal model accurately model the <span class="hlt">shock</span>-wave heating and timing of the heat-front penetration while the <span class="hlt">shock</span> is transiting the target. The observed discrepancy between the measured and simulated <span class="hlt">shock</span>-wave heating at late times of the drive can be explained by the reduced radiative heating due to lateral heat flow in the corona.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2012PhRvL.108e8001G','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2012PhRvL.108e8001G"><span><span class="hlt">Shocks</span> near Jamming</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Gómez, Leopoldo R.; Turner, Ari M.; van Hecke, Martin; Vitelli, Vincenzo</p> <p>2012-02-01</p> <p>Nonlinear sound is an extreme phenomenon typically observed in solids after violent explosions. But granular media are different. Right when they jam, these fragile and disordered solids exhibit a vanishing rigidity and sound speed, so that even tiny mechanical perturbations form supersonic <span class="hlt">shocks</span>. Here, we perform simulations in which two-dimensional jammed granular packings are dynamically <span class="hlt">compressed</span> and demonstrate that the elementary excitations are strongly nonlinear <span class="hlt">shocks</span>, rather than ordinary phonons. We capture the full dependence of the <span class="hlt">shock</span> speed on pressure and impact intensity by a surprisingly simple analytical model.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2013APS..SHK.J3002T','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2013APS..SHK.J3002T"><span>Experiments on a Miniature Hypervelocity <span class="hlt">Shock</span> Tube</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Tasker, Douglas; Johnson, Carl; Murphy, Michael; Lieber, Mark; MIMS Team</p> <p>2013-06-01</p> <p>A miniature explosively-driven <span class="hlt">shock</span> tube, based on the Voitenko compressor design, has been designed to produce <span class="hlt">shock</span> speeds in light gases in excess of 80 km/s. Voitenko compressors over 1 meter in diameter have been reported but here experiments on miniature <span class="hlt">shock</span> tubes with ~1-mm bore diameters are described. In this design a 12-mm diameter explosive pellet drives a metal plate into a hemispherical gas <span class="hlt">compression</span> chamber. Downstream from the piston a mica diaphragm separates the gas from an evacuated <span class="hlt">shock</span> tube which is confined by a massive polymethylmethacrylate (PMMA) block. The diaphragm eventually ruptures under the applied pressure loading and the <span class="hlt">compressed</span> gases escape into the evacuated <span class="hlt">shock</span> tube at hyper velocities. The progress of gas <span class="hlt">shocks</span> in the tube and bow <span class="hlt">shocks</span> in the PMMA are monitored with an ultra-high-speed imaging system, the <span class="hlt">Shock</span> Wave Image Framing Technique (SWIFT). The resulting time-resolved images yield two-dimensional visualizations of <span class="hlt">shock</span> geometry and progression. By measuring both the gas and bow <span class="hlt">shocks</span>, accurate and unequivocal measurements of <span class="hlt">shock</span> position history are obtained. The experimental results were compared with those of hydrocode modeling to optimize the design. The first experiments were suboptimum in that the velocities were ~16 km/s. Progress with these experiments will be reported.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19850004196','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19850004196"><span>Dynamic <span class="hlt">compression</span> and volatile release of carbonates</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Tyburczy, J. A.; Ahrens, T. J.</p> <p>1984-01-01</p> <p>Particle velocity profiles upon <span class="hlt">shock</span> <span class="hlt">compression</span> and isentropic releases were measured for polycrystalline calcite. The Solenhofen limestone release paths lie, close to the Hugoniot. Calcite 3 to 2 transition, upon release, was observed, but rarefaction <span class="hlt">shocks</span> were not detected. The equation of state is used to predict the fraction of material devolatilized upon isentropic release as a function of <span class="hlt">shock</span> pressure. The effect of ambient partial pressure of CO2 on the calculations is demonstrated and considered in models of atmospheric evolution by impact induced mineral devolatilization. The radiative characteristics of <span class="hlt">shocked</span> calcite indicate that localization of thermal energy occurs under <span class="hlt">shock</span> <span class="hlt">compression</span>. <span class="hlt">Shock</span> entropy calculations result in a minimum estimate of 90% devolatilization upon complete release from 10 GPa. Isentropic release paths from calculated continuum Hugoniot temperatures cross into the CaO (solid) + CO2 (vapor) field at improbably low pressures. It is found that release paths from measured <span class="hlt">shock</span> temperatures cross into the melt plus vapor field at pressures greater than .5 GPa, which suggests that devolatilization is initiated at the shear banding sites.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018JAP...123d5105Z','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018JAP...123d5105Z"><span>Effect of grain boundaries on <span class="hlt">shock</span>-induced phase transformation in <span class="hlt">iron</span> bicrystals</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Zhang, Xueyang; Wang, Kun; Zhu, Wenjun; Chen, Jun; Cai, Mengqiu; Xiao, Shifang; Deng, Huiqiu; Hu, Wangyu</p> <p>2018-01-01</p> <p>Non-equilibrium molecular-dynamic simulations with a modified analytic embedded-atom model potential have been performed to investigate the effect of three kinds of grain boundaries (GBs) on the martensitic transformation in <span class="hlt">iron</span> bicrystals with three different GBs under <span class="hlt">shock</span> loadings. Our results show that the phase transition was influenced by the GBs. All three GBs provide a nucleation site for the α → ɛ transformation in samples <span class="hlt">shock</span>-loaded with up = 0.5 km/s, and in particular, the elastic wave can induce the phase transformation at Σ3 ⟨110⟩ twist GB, which indicates that the phase transformation can occur at Σ3 ⟨110⟩ twist GB with a much lower pressure. The effect of GBs on the stress assisted transformation (SAT) mechanisms is discussed. All variants nucleating at the vicinity of these GBs meet the maximum strain work (MSW) criterion. Moreover, all of the variants with the MSW nucleate at Σ5 ⟨001⟩ twist GB and Σ3 ⟨110⟩ tilt GB, but only part of them nucleate at Σ3 ⟨110⟩ twist GB. This is because the coincident planes between both sides of the GB would affect the slip process, which is the second stage of the martensitic transformation and influences the selection of variant. We also find that the martensitic transformation at the front end of the bicrystals would give rise to stress attenuation in samples <span class="hlt">shock</span>-loaded with up = 0.6 km/s, which makes the GBs seem to be unfavorable to the martensitic transformation. Our findings have the potential to affect the interface engineering and material design under high pressure conditions.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19960011642','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19960011642"><span>Floating <span class="hlt">shock</span> fitting via Lagrangian adaptive meshes</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Vanrosendale, John</p> <p>1995-01-01</p> <p>In recent work we have formulated a new approach to <span class="hlt">compressible</span> flow simulation, combining the advantages of <span class="hlt">shock</span>-fitting and <span class="hlt">shock</span>-capturing. Using a cell-centered on Roe scheme discretization on unstructured meshes, we warp the mesh while marching to steady state, so that mesh edges align with <span class="hlt">shocks</span> and other discontinuities. This new algorithm, the <span class="hlt">Shock</span>-fitting Lagrangian Adaptive Method (SLAM), is, in effect, a reliable <span class="hlt">shock</span>-capturing algorithm which yields <span class="hlt">shock</span>-fitted accuracy at convergence.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/21405926','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/21405926"><span>Burnett-Cattaneo continuum theory for <span class="hlt">shock</span> waves.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Holian, Brad Lee; Mareschal, Michel; Ravelo, Ramon</p> <p>2011-02-01</p> <p>We model strong <span class="hlt">shock</span>-wave propagation, both in the ideal gas and in the dense Lennard-Jones fluid, using a refinement of earlier work, which accounts for the cold <span class="hlt">compression</span> in the early stages of the <span class="hlt">shock</span> rise by a nonlinear, Burnett-like, strain-rate dependence of the thermal conductivity, and relaxation of kinetic-temperature components on the hot, <span class="hlt">compressed</span> side of the <span class="hlt">shock</span> front. The relaxation of the disequilibrium among the three components of the kinetic temperature, namely, the difference between the component in the direction of a planar <span class="hlt">shock</span> wave and those in the transverse directions, particularly in the region near the <span class="hlt">shock</span> front, is accomplished at a much more quantitative level by a rigorous application of the Cattaneo-Maxwell relaxation equation to a reference solution, namely, the steady <span class="hlt">shock</span>-wave solution of linear Navier-Stokes-Fourier theory, along with the nonlinear Burnett heat-flux term. Our new continuum theory is in nearly quantitative agreement with nonequilibrium molecular-dynamics simulations under strong <span class="hlt">shock</span>-wave conditions, using relaxation parameters obtained from the reference solution. ©2011 American Physical Society</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/27071341','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/27071341"><span>Inelastic response of silicon to <span class="hlt">shock</span> <span class="hlt">compression</span>.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Higginbotham, A; Stubley, P G; Comley, A J; Eggert, J H; Foster, J M; Kalantar, D H; McGonegle, D; Patel, S; Peacock, L J; Rothman, S D; Smith, R F; Suggit, M J; Wark, J S</p> <p>2016-04-13</p> <p>The elastic and inelastic response of [001] oriented silicon to laser <span class="hlt">compression</span> has been a topic of considerable discussion for well over a decade, yet there has been little progress in understanding the basic behaviour of this apparently simple material. We present experimental x-ray diffraction data showing complex elastic strain profiles in laser <span class="hlt">compressed</span> samples on nanosecond timescales. We also present molecular dynamics and elasticity code modelling which suggests that a pressure induced phase transition is the cause of the previously reported 'anomalous' elastic waves. Moreover, this interpretation allows for measurement of the kinetic timescales for transition. This model is also discussed in the wider context of reported deformation of silicon to rapid <span class="hlt">compression</span> in the literature.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1367964-magnetostructural-transition-kinetics-shocked-iron','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1367964-magnetostructural-transition-kinetics-shocked-iron"><span>Magnetostructural Transition Kinetics in <span class="hlt">Shocked</span> <span class="hlt">Iron</span></span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>Surh, Michael P.; Benedict, Lorin X.; Sadigh, Babak</p> <p>2016-08-15</p> <p>Here, a generalized Heisenberg model is implemented to study the effect of thermal magnetic disorder on kinetics of the Fe α–ε transition. The barrier to bulk martensitic displacement remains large in α-Fe <span class="hlt">shocked</span> well past the phase line but is much reduced in the [001] α–ε boundary. The first result is consistent with observed overdriving to metastable α, while the second suggests structural instability, as implied by observation of a [001] <span class="hlt">shock</span> transformation front without plastic relaxation. Reconciling both behaviors may require concurrent treatment of magnetic and structural order.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_10");'>10</a></li> <li><a href="#" onclick='return showDiv("page_11");'>11</a></li> <li class="active"><span>12</span></li> <li><a href="#" onclick='return showDiv("page_13");'>13</a></li> <li><a href="#" onclick='return showDiv("page_14");'>14</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_12 --> <div id="page_13" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_11");'>11</a></li> <li><a href="#" onclick='return showDiv("page_12");'>12</a></li> <li class="active"><span>13</span></li> <li><a href="#" onclick='return showDiv("page_14");'>14</a></li> <li><a href="#" onclick='return showDiv("page_15");'>15</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="241"> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1242000-lattice-level-observation-elastic-plastic-relaxation-process-subnanosecond-resolution-shock-compressed-ta-using-time-resolved-situ-laue-diffraction','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1242000-lattice-level-observation-elastic-plastic-relaxation-process-subnanosecond-resolution-shock-compressed-ta-using-time-resolved-situ-laue-diffraction"><span>Lattice-level observation of the elastic-to-plastic relaxation process with subnanosecond resolution in <span class="hlt">shock-compressed</span> Ta using time-resolved in situ Laue diffraction</span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>Wehrenberg, C. E.; Comley, A. J.; Barton, N. R.; ...</p> <p>2015-09-29</p> <p>We report direct lattice level measurements of plastic relaxation kinetics through time-resolved, in-situ Laue diffraction of <span class="hlt">shock-compressed</span> single-crystal [001] Ta at pressures of 27-210 GPa. For a 50 GPa <span class="hlt">shock</span>, a range of shear strains is observed extending up to the uniaxial limit for early data points (<0.6 ns) and the average shear strain relaxes to a near steady state over ~1 ns. For 80 and 125 GPa <span class="hlt">shocks</span>, the measured shear strains are fully relaxed already at 200 ps, consistent with rapid relaxation associated with the predicted threshold for homogeneous nucleation of dislocations occurring at <span class="hlt">shock</span> pressure ~65 GPa.more » The relaxation rate and shear stresses are used to estimate the dislocation density and these quantities are compared to the Livermore Multiscale Strength model as well as various molecular dynamics simulations.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015AGUFMMR12A..06A','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015AGUFMMR12A..06A"><span>Sound Speed of Liquid <span class="hlt">Iron</span> Along the Outer Core Isentrope: New Pre-heated Ramp <span class="hlt">Compression</span> Experiments</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Asimow, P. D.; Nguyen, J.; Akin, M. C.; Fatýanov, O. V.</p> <p>2015-12-01</p> <p>Detailed elasticity data on liquid Fe and candidate molten core alloys should offer new constraints on the under-constrained problem of Earth's core composition. Density, sound speed, and the gradient in sound speed with pressure are each potentially distinct experimental constraints and are each well-known for Earth. The gradient in sound speed, though, has not been used because sound speed depends on both T and P, such that data must be collected or reconstructed along the correct, nearly adiabatic, thermal profile. Reconstruction requires the Grüneisen γ, which is composition-dependent, and data over a large P-T space to allow extrapolation. Both static and dynamic <span class="hlt">compression</span> methods could be used, but the conditions (140 - 330 GPa and 4000 - 6000 K) are very challenging for static methods and standard <span class="hlt">shock</span> <span class="hlt">compression</span> only samples the outer core P-T profile at a single P. Instead we are applying quasi-isentropic dynamic ramp <span class="hlt">compression</span>, using pre-heating of the target and impedance of the leading edge of a graded-density impactor (GDI) to select a probable outer core isentrope. The target material is melted and raised to a point on the outer core isentrope by the initial <span class="hlt">shock</span>, then quasi-isentropically ramped to a maximum P by increasing <span class="hlt">shock</span> impedance of trailing GDI layers. Particle velocity is monitored by photonic doppler velocimetry (PDV) at two step thicknesses at the interface of Fe or Fe-alloy target and MgO windows. The difference in arrival time of each particle velocity at the two steps directly gives the Lagrangian sound speed vs. particle velocity, which is integrated to obtain Pand density. At the writing of this abstract, we have completed one shot of this type. We successfully heated a two-step Fe target in a Mo capsule with MgO windows to 1350 °C, maintaining sufficient alignment and reflectivity to collect PDV signal returns. We characterized the velocity correction factor for PDV observation through MgO windows, and have confirmed</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1334538-complete-equation-state-shocked-liquid-nitrogen-analytical-developments','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1334538-complete-equation-state-shocked-liquid-nitrogen-analytical-developments"><span>Complete equation of state for <span class="hlt">shocked</span> liquid nitrogen: Analytical developments</span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>Winey, J. M.; Gupta, Y. M.</p> <p>2016-08-02</p> <p>The thermodynamic response of liquid nitrogen has been studied extensively, in part, due to the long-standing interest in the high pressure and high temperature dissociation of <span class="hlt">shocked</span> molecular nitrogen. Previous equation of state (EOS) developments regarding <span class="hlt">shocked</span> liquid nitrogen have focused mainly on the use of intermolecular pair potentials in atomistic calculations. Here, we present EOS developments for liquid nitrogen, incorporating analytical models, for use in continuum calculations of the <span class="hlt">shock</span> <span class="hlt">compression</span> response. The analytical models, together with available Hugoniot data, were used to extrapolate a low pressure reference EOS for molecular nitrogen [Span, et al., J. Phys. Chem. Ref.more » Data 29, 1361 (2000)] to high pressures and high temperatures. Using the EOS presented here, the calculated pressures and temperatures for single <span class="hlt">shock</span>, double <span class="hlt">shock</span>, and multiple <span class="hlt">shock</span> <span class="hlt">compression</span> of liquid nitrogen provide a good match to the measured results over a broad range of P-T space. Our calculations provide the first comparison of EOS developments with recently-measured P-T states under multiple <span class="hlt">shock</span> <span class="hlt">compression</span>. The present EOS developments are general and are expected to be useful for other liquids that have low pressure reference EOS information available.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2000AIPC..505..993T','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2000AIPC..505..993T"><span>Measurements of spatially resolved velocity variations in <span class="hlt">shock</span> <span class="hlt">compressed</span> heterogeneous materials using a line-imaging velocity interferometer</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Trott, Wayne M.; Knudson, Marcus D.; Chhabildas, Lalit C.; Asay, James R.</p> <p>2000-04-01</p> <p>Relatively straightforward changes in the design of a conventional optically recording velocity interferometer system (ORVIS) can be used to produce a line-imaging instrument that allows adjustment of spatial resolution over a wide range. As a result, line-imaging ORVIS can be tailored to various specific applications involving dynamic deformation of heterogeneous materials as required by their characteristic length scales (ranging from a few μm for ferroelectric ceramics to a few mm for concrete). A line-imaging system has been successfully interfaced to a <span class="hlt">compressed</span> gas gun driver and fielded on numerous tests in combination with simultaneous dual delay-leg, "push-pull" VISAR measurements. These tests include <span class="hlt">shock</span> loading of glass-reinforced polyester composites, foam reverberation experiments (measurements at the free surface of a thin aluminum plate impacted by foam), and measurements of dispersive velocity in a <span class="hlt">shock</span>-loaded explosive simulant (sugar). Results are presented that illustrate the capability for recording detailed spatially resolved material response.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018MNRAS.477..816L','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018MNRAS.477..816L"><span>Radiation- and pair-loaded <span class="hlt">shocks</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Lyutikov, Maxim</p> <p>2018-06-01</p> <p>We consider the structure of mildly relativistic <span class="hlt">shocks</span> in dense media, taking into account the radiation and pair loading, and diffusive radiation energy transfer within the flow. For increasing <span class="hlt">shock</span> velocity (increasing post-<span class="hlt">shock</span> temperature), the first important effect is the efficient energy redistribution by radiation within the <span class="hlt">shock</span> that leads to the appearance of an isothermal jump, whereby the flow reaches the final state through a discontinuous isothermal transition. The isothermal jump, on scales much smaller than the photon diffusion length, consists of a weak <span class="hlt">shock</span> and a quick relaxation to the isothermal conditions. Highly radiation-dominated <span class="hlt">shocks</span> do not form isothermal jump. Pair production can mildly increase the overall <span class="hlt">shock</span> <span class="hlt">compression</span> ratio to ≈10 (4 for matter-dominated <span class="hlt">shocks</span> and 7 of the radiation-dominated <span class="hlt">shocks</span>).</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1259515-inelastic-response-silicon-shock-compression','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1259515-inelastic-response-silicon-shock-compression"><span>Inelastic response of silicon to <span class="hlt">shock</span> <span class="hlt">compression</span></span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>Higginbotham, Andrew; Stubley, P. G.; Comley, A. J.; ...</p> <p>2016-04-13</p> <p>The elastic and inelastic response of [001] oriented silicon to laser <span class="hlt">compression</span> has been a topic of considerable discussion for well over a decade, yet there has been little progress in understanding the basic behaviour of this apparently simple material. We present experimental x-ray diffraction data showing complex elastic strain profiles in laser <span class="hlt">compressed</span> samples on nanosecond timescales. We also present molecular dynamics and elasticity code modelling which suggests that a pressure induced phase transition is the cause of the previously reported ‘anomalous’ elastic waves. Moreover, this interpretation allows for measurement of the kinetic timescales for transition. Lastly, this modelmore » is also discussed in the wider context of reported deformation of silicon to rapid <span class="hlt">compression</span> in the literature.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4829838','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4829838"><span>Inelastic response of silicon to <span class="hlt">shock</span> <span class="hlt">compression</span></span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Higginbotham, A.; Stubley, P. G.; Comley, A. J.; Eggert, J. H.; Foster, J. M.; Kalantar, D. H.; McGonegle, D.; Patel, S.; Peacock, L. J.; Rothman, S. D.; Smith, R. F.; Suggit, M. J.; Wark, J. S.</p> <p>2016-01-01</p> <p>The elastic and inelastic response of [001] oriented silicon to laser <span class="hlt">compression</span> has been a topic of considerable discussion for well over a decade, yet there has been little progress in understanding the basic behaviour of this apparently simple material. We present experimental x-ray diffraction data showing complex elastic strain profiles in laser <span class="hlt">compressed</span> samples on nanosecond timescales. We also present molecular dynamics and elasticity code modelling which suggests that a pressure induced phase transition is the cause of the previously reported ‘anomalous’ elastic waves. Moreover, this interpretation allows for measurement of the kinetic timescales for transition. This model is also discussed in the wider context of reported deformation of silicon to rapid <span class="hlt">compression</span> in the literature. PMID:27071341</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/5316742','DOE-PATENT-XML'); return false;" href="https://www.osti.gov/biblio/5316742"><span>Isentropic <span class="hlt">compressive</span> wave generator and method of making same</span></a></p> <p><a target="_blank" href="http://www.osti.gov/doepatents">DOEpatents</a></p> <p>Barker, L.M.</p> <p></p> <p>An isentropic <span class="hlt">compressive</span> wave generator and method of making same are disclosed. The wave generator comprises a disk or flat pillow member having component materials of different <span class="hlt">shock</span> impedances formed in a configuration resulting in a smooth <span class="hlt">shock</span> impedance gradient over the thickness thereof for interpositioning between an impactor member and a target specimen for producing a <span class="hlt">shock</span> wave of a smooth predictable rise time. The method of making the pillow member comprises the reduction of the component materials to a powder form and forming the pillow member by sedimentation and <span class="hlt">compressive</span> techniques.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018PhyB..541...89W','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018PhyB..541...89W"><span>Resistivity behavior of hydrogen and liquid silane at high <span class="hlt">shock</span> <span class="hlt">compression</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Wang, Yi-Gao; Liu, Fu-Sheng; Liu, Qi-Jun</p> <p>2018-07-01</p> <p>To study the electrical properties of hydrogen rich compounds under extreme conditions, the electrical resistivity of density hydrogen and silane fluid was measured, respectively. The hydrogen sample was prepared by <span class="hlt">compressing</span> pure hydrogen gas to 10 MPa in a coolant target system at the temperature of 77 K. The silane sample can be obtained with the same method. High-pressure and high-temperature experiments were performed using a two-stage light-gas gun. The electrical resistivity of the sample decreased with increasing pressure and temperature as expected. A minimum electrical resistivity value of 0.3 × 10-3 Ω cm at 138 GPa and 4100 K was obtained for silane. The minimum resistivity of hydrogen in the state of 102 GPa and 4300 K was 0.35 Ω cm. It showed that the measured electrical resistivity of the <span class="hlt">shock-compressed</span> hydrogen was an order of magnitude higher than fluid silane at 50-90 GPa. However, beyond 100 GPa, the resistivity difference between silane and hydrogen was very minor. The carriers in the sample were hydrogen, and the concentration of hydrogen atoms in these two substances was close to each other. These results supported the theoretical prediction that silane was interpreted simply in terms of chemical decomposition into silicon nanoparticles and fluid hydrogen, and electrical conduction flows predominately dominated by the fluid hydrogen. In addition, the results also supported the theory of "chemical precompression", the existence of Sisbnd H bond helped to reduce the pressure of hydrogen metallization. These findings could lead the way for further metallic phases of hydrogen-rich materials and experimental studies.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015AGUFMMR13C2728J','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015AGUFMMR13C2728J"><span>Waste Heat Approximation for Understanding Dynamic <span class="hlt">Compression</span> in Nature and Experiments</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Jeanloz, R.</p> <p>2015-12-01</p> <p>Energy dissipated during dynamic <span class="hlt">compression</span> quantifies the residual heat left in a planet due to impact and accretion, as well as the deviation of a loading path from an ideal isentrope. Waste heat ignores the difference between the pressure-volume isentrope and Hugoniot in approximating the dissipated energy as the area between the Rayleigh line and Hugoniot (assumed given by a linear dependence of <span class="hlt">shock</span> velocity on particle velocity). Strength and phase transformations are ignored: justifiably, when considering sufficiently high dynamic pressures and reversible transformations. Waste heat mis-estimates the dissipated energy by less than 10-20 percent for volume <span class="hlt">compressions</span> under 30-60 percent. Specific waste heat (energy per mass) reaches 0.2-0.3 c02 at impact velocities 2-4 times the zero-pressure bulk sound velocity (c0), its maximum possible value being 0.5 c02. As larger impact velocities are implied for typical orbital velocities of Earth-like planets, and c02 ≈ 2-30 MJ/kg for rock, the specific waste heat due to accretion corresponds to temperature rises of about 3-15 x 103 K for rock: melting accompanies accretion even with only 20-30 percent waste heat retained. Impact sterilization is similarly quantified in terms of waste heat relative to the energy required to vaporize H2O (impact velocity of 7-8 km/s, or 4.5-5 c0, is sufficient). Waste heat also clarifies the relationship between <span class="hlt">shock</span>, multi-<span class="hlt">shock</span> and ramp loading experiments, as well as the effect of (static) pre-<span class="hlt">compression</span>. Breaking a <span class="hlt">shock</span> into 2 steps significantly reduces the dissipated energy, with minimum waste heat achieved for two equal volume <span class="hlt">compressions</span> in succession. Breaking a <span class="hlt">shock</span> into as few as 4 steps reduces the waste heat to within a few percent of zero, documenting how multi-<span class="hlt">shock</span> loading approaches an isentrope. Pre-<span class="hlt">compression</span>, being less dissipative than an initial <span class="hlt">shock</span> to the same strain, further reduces waste heat. Multi-<span class="hlt">shock</span> (i.e., high strain-rate) loading of pre-<span class="hlt">compressed</span></p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19940002884&hterms=mixed+methods&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D10%26Ntt%3Dmixed%2Bmethods','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19940002884&hterms=mixed+methods&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D10%26Ntt%3Dmixed%2Bmethods"><span>FLOW FIELD IN SUPERSONIC MIXED-<span class="hlt">COMPRESSION</span> INLETS AT ANGLE OF ATTACK USING THE THREE DIMENSIONAL METHOD OF CHARACTERISTICS WITH DISCRETE <span class="hlt">SHOCK</span> WAVE FITTING</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Bishop, A. R.</p> <p>1994-01-01</p> <p>This computer program calculates the flow field in the supersonic portion of a mixed-<span class="hlt">compression</span> aircraft inlet at non-zero angle of attack. This approach is based on the method of characteristics for steady three-dimensional flow. The results of this program agree with those produced by the two-dimensional method of characteristics when axisymmetric flow fields are calculated. Except in regions of high viscous interaction and boundary layer removal, the results agree well with experimental data obtained for threedimensional flow fields. The flow field in a variety of axisymmetric mixed <span class="hlt">compression</span> inlets can be calculated using this program. The bow <span class="hlt">shock</span> wave and the internal <span class="hlt">shock</span> wave system are calculated using a discrete <span class="hlt">shock</span> wave fitting procedure. The internal flow field can be calculated either with or without the discrete fitting of the internal <span class="hlt">shock</span> wave system. The influence of molecular transport can be included in the calculation of the external flow about the forebody and in the calculation of the internal flow when internal <span class="hlt">shock</span> waves are not discretely fitted. The viscous and thermal diffussion effects are included by treating them as correction terms in the method of characteristics procedure. Dynamic viscosity is represented by Sutherland's law and thermal conductivity is represented as a quadratic function of temperature. The thermodynamic model used is that of a thermally and calorically perfect gas. The program assumes that the cowl lip is contained in a constant plane and that the centerbody contour and cowl contour are smooth and have continuous first partial derivatives. This program cannot calculate subsonic flow, the external flow field if the bow <span class="hlt">shock</span> wave does not exist entirely around the forebody, or the internal flow field if the bow flow field is injected into the annulus. Input to the program consists of parameters to control execution, to define the geometry, and the vehicle orientation. Output consists of a list of parameters</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2007SPIE.6722E..1XY','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2007SPIE.6722E..1XY"><span>Laser <span class="hlt">shock</span> wave and its applications</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Yang, Chaojun; Zhang, Yongkang; Zhou, Jianzhong; Zhang, Fang; Feng, Aixin</p> <p>2007-12-01</p> <p>The technology of laser <span class="hlt">shock</span> wave is used to not only surface modification but also metal forming. It can be divided into three parts: laser <span class="hlt">shock</span> processing, laser <span class="hlt">shock</span> forming (LSF) and laser peenforming(LPF). Laser <span class="hlt">shock</span> processing as a surface treatment to metals can make engineering components have a residual <span class="hlt">compressive</span> stress so that it obviously improves their fatigue strength and stress corrosion performances, while laser <span class="hlt">shock</span> forming (LSF) is a novel technique that is used in plastic deformation of sheet metal recently and Laser peen forming (LPF) is another new sheet metal forming process presented in recent years. They all can be carried out by a high-power and repetition pulse Nd:Glass laser device made by Jiangsu University. Laser <span class="hlt">shock</span> technology has characterized of ultrahigh pressure and high strain rate (10 6 - 10 7s -1). Now, for different materials, we are able to form different metals to contours and shapes and simultaneity leave their surfaces in crack-resistant <span class="hlt">compressive</span> stress state. The results show that the technology of laser <span class="hlt">shock</span> wave can strengthen surface property and prolong fatigue life and especially can deform metals to shapes that could not be adequately made using conventional methods. With the development of the technology of laser <span class="hlt">shock</span> wave, the applied fields of laser will become greater and greater.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/18248049','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/18248049"><span>X-ray diffraction from <span class="hlt">shock</span>-loaded polycrystals.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Swift, Damian C</p> <p>2008-01-01</p> <p>X-ray diffraction was demonstrated from <span class="hlt">shock-compressed</span> polycrystalline metals on nanosecond time scales. Laser ablation was used to induce <span class="hlt">shock</span> waves in polycrystalline foils of Be, 25-125 microm thick. A second laser pulse was used to generate a plasma x-ray source by irradiation of a Ti foil. The x-ray source was collimated to produce a beam of controllable diameter, which was directed at the Be sample. X-rays were diffracted from the sample, and detected using films and x-ray streak cameras. The diffraction angle was observed to change with <span class="hlt">shock</span> pressure. The diffraction angles were consistent with the uniaxial (elastic) and isotropic (plastic) <span class="hlt">compressions</span> expected for the loading conditions used. Polycrystalline diffraction will be used to measure the response of the crystal lattice to high <span class="hlt">shock</span> pressures and through phase changes.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016ApJ...827...47L','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016ApJ...827...47L"><span>Combining Diffusive <span class="hlt">Shock</span> Acceleration with Acceleration by Contracting and Reconnecting Small-scale Flux Ropes at Heliospheric <span class="hlt">Shocks</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>le Roux, J. A.; Zank, G. P.; Webb, G. M.; Khabarova, O. V.</p> <p>2016-08-01</p> <p>Computational and observational evidence is accruing that heliospheric <span class="hlt">shocks</span>, as emitters of vorticity, can produce downstream magnetic flux ropes and filaments. This led Zank et al. to investigate a new paradigm whereby energetic particle acceleration near <span class="hlt">shocks</span> is a combination of diffusive <span class="hlt">shock</span> acceleration (DSA) with downstream acceleration by many small-scale contracting and reconnecting (merging) flux ropes. Using a model where flux-rope acceleration involves a first-order Fermi mechanism due to the mean <span class="hlt">compression</span> of numerous contracting flux ropes, Zank et al. provide theoretical support for observations that power-law spectra of energetic particles downstream of heliospheric <span class="hlt">shocks</span> can be harder than predicted by DSA theory and that energetic particle intensities should peak behind <span class="hlt">shocks</span> instead of at <span class="hlt">shocks</span> as predicted by DSA theory. In this paper, a more extended formalism of kinetic transport theory developed by le Roux et al. is used to further explore this paradigm. We describe how second-order Fermi acceleration, related to the variance in the electromagnetic fields produced by downstream small-scale flux-rope dynamics, modifies the standard DSA model. The results show that (I) this approach can qualitatively reproduce observations of particle intensities peaking behind the <span class="hlt">shock</span>, thus providing further support for the new paradigm, and (II) stochastic acceleration by <span class="hlt">compressible</span> flux ropes tends to be more efficient than incompressible flux ropes behind <span class="hlt">shocks</span> in modifying the DSA spectrum of energetic particles.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/21277099-al-absorption-spectroscopy-shock-wave-heating-compression-laser-driven-planar-foil','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/21277099-al-absorption-spectroscopy-shock-wave-heating-compression-laser-driven-planar-foil"><span>Al 1s-2p absorption spectroscopy of <span class="hlt">shock</span>-wave heating and <span class="hlt">compression</span> in laser-driven planar foil</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Sawada, H.; Regan, S. P.; Radha, P. B.</p> <p></p> <p>Time-resolved Al 1s-2p absorption spectroscopy is used to diagnose direct-drive, <span class="hlt">shock</span>-wave heating and <span class="hlt">compression</span> of planar targets having nearly Fermi-degenerate plasma conditions (T{sub e}{approx}10-40 eV, {rho}{approx}3-11 g/cm{sup 3}) on the OMEGA Laser System [T. R. Boehly et al., Opt. Commun. 133, 495 (1997)]. A planar plastic foil with a buried Al tracer layer was irradiated with peak intensities of 10{sup 14}-10{sup 15} W/cm{sup 2} and probed with the pseudocontinuum M-band emission from a point-source Sm backlighter in the range of 1.4-1.7 keV. The laser ablation process launches 10-70 Mbar <span class="hlt">shock</span> waves into the CH/Al/CH target. The Al 1s-2p absorption spectramore » were analyzed using the atomic physic code PRISMSPECT to infer T{sub e} and {rho} in the Al layer, assuming uniform plasma conditions during <span class="hlt">shock</span>-wave heating, and to determine when the heat front penetrated the Al layer. The drive foils were simulated with the one-dimensional hydrodynamics code LILAC using a flux-limited (f=0.06 and f=0.1) and nonlocal thermal-transport model [V. N. Goncharov et al., Phys. Plasmas 13, 012702 (2006)]. The predictions of simulated <span class="hlt">shock</span>-wave heating and the timing of heat-front penetration are compared to the observations. The experimental results for a wide variety of laser-drive conditions and buried depths have shown that the LILAC predictions using f=0.06 and the nonlocal model accurately model the <span class="hlt">shock</span>-wave heating and timing of the heat-front penetration while the <span class="hlt">shock</span> is transiting the target. The observed discrepancy between the measured and simulated <span class="hlt">shock</span>-wave heating at late times of the drive can be explained by the reduced radiative heating due to lateral heat flow in the corona.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19950010849','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19950010849"><span>Interactive computer graphics applications for <span class="hlt">compressible</span> aerodynamics</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Benson, Thomas J.</p> <p>1994-01-01</p> <p>Three computer applications have been developed to solve inviscid <span class="hlt">compressible</span> fluids problems using interactive computer graphics. The first application is a <span class="hlt">compressible</span> flow calculator which solves for isentropic flow, normal <span class="hlt">shocks</span>, and oblique <span class="hlt">shocks</span> or centered expansions produced by two dimensional ramps. The second application couples the solutions generated by the first application to a more graphical presentation of the results to produce a desk top simulator of three <span class="hlt">compressible</span> flow problems: 1) flow past a single <span class="hlt">compression</span> ramp; 2) flow past two ramps in series; and 3) flow past two opposed ramps. The third application extends the results of the second to produce a design tool which solves for the flow through supersonic external or mixed <span class="hlt">compression</span> inlets. The applications were originally developed to run on SGI or IBM workstations running GL graphics. They are currently being extended to solve additional types of flow problems and modified to operate on any X-based workstation.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017EGUGA..19.4774F','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017EGUGA..19.4774F"><span>On the finite length-scale of <span class="hlt">compressible</span> <span class="hlt">shock</span>-waves formed in free-surface flows of dry granular materials down a slope</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Faug, Thierry</p> <p>2017-04-01</p> <p>The Rankine-Hugoniot jump conditions traditionally describe the theoretical relationship between the equilibrium state on both sides of a <span class="hlt">shock</span>-wave. They are based on the crucial assumption that the length-scale needed to adjust the equilibrium state upstream of the <span class="hlt">shock</span> to downstream of it is too small to be of significance to the problem. They are often used with success to describe the <span class="hlt">shock</span>-waves in a number of applications found in both fluid and solid mechanics. However, the relations based on jump conditions at singular surfaces may fail to capture some features of the <span class="hlt">shock</span>-waves formed in complex materials, such as granular matter. This study addresses the particular problem of <span class="hlt">compressible</span> <span class="hlt">shock</span>-waves formed in flows of dry granular materials down a slope. This problem is for instance relevant to full-scale geophysical granular flows in interaction with natural obstacles or man-made structures, such as topographical obstacles or mitigation dams respectively. Steady-state jumps formed in granular flows and travelling <span class="hlt">shock</span>-waves produced at the impact of a granular avalanche-flow with a rigid wall are considered. For both situations, new analytical relations which do not consider that the granular <span class="hlt">shock</span>-wave shrinks into a singular surface are derived, by using balance equations in their depth-averaged forms for mass and momentum. However, these relations need additional inputs that are closure relations for the size and the shape of the <span class="hlt">shock</span>-wave, and a relevant constitutive friction law. Small-scale laboratory tests and numerical simulations based on the discrete element method are shortly presented and used to infer crucial information needed for the closure relations. This allows testing some predictive aspects of the simple analytical approach proposed for both steady-state and travelling <span class="hlt">shock</span>-waves formed in free-surface flows of dry granular materials down a slope.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2007SPIE.6694E..16B','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2007SPIE.6694E..16B"><span>Survival of microbial life under <span class="hlt">shock</span> <span class="hlt">compression</span>: implications for Panspermia</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Burchell, M.</p> <p>2007-09-01</p> <p>An analysis is carried out of the survival fraction of micro-organisms exposed to extreme <span class="hlt">shock</span> pressures. A variety of data sources are used in this analysis. The key findings are that survival depends on the behaviour of the cell wall. Below a critical <span class="hlt">shock</span> pressure there is a relatively slow fall in survival fraction as <span class="hlt">shock</span> pressures increase. Above the critical threshold survival starts to fall rapidly as <span class="hlt">shock</span> pressure increases further. The critical <span class="hlt">shock</span> pressures found here are in the range 2.4 to 20 GPa, and vary not only from organism to organism, but also depend on the growth stage of given organisms, with starved (i.e., no growth) states favoured for survival. At the <span class="hlt">shock</span> pressures typical of those involved in interplanetary transfer of rocky materials, the survival fractions are found to be small but finite. This lends credence to the idea of Panspermia, i.e. life may naturally migrate through space. Thus for example, Martian meteorites should not a prior be considered as sterile due to the <span class="hlt">shock</span> processes they have undergone, but their lack of viable micro-organisms either reflects no such life being present at the source at the time of departure or the influence of other hazardous processes such as radiation in space or heating of surfaces during entry into a planetary atmosphere.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2014APS..DPPUO4003B','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2014APS..DPPUO4003B"><span>Measurement of the <span class="hlt">Shock</span> Velocity and Symmetry History in Decaying <span class="hlt">Shock</span> Pulses</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Baker, Kevin; Milovich, Jose; Jones, Oggie; Robey, Harry; Smalyuk, Vladimir; Casey, Daniel; Celliers, Peter; Clark, Dan; Giraldez, Emilio; Haan, Steve; Hamza, Alex; Berzak-Hopkins, Laura; Jancaitis, Ken; Kroll, Jeremy; Lafortune, Kai; MacGowan, Brian; Macphee, Andrew; Moody, John; Nikroo, Abbas; Peterson, Luc; Raman, Kumar; Weber, Chris; Widmayer, Clay</p> <p>2014-10-01</p> <p>Decaying first <span class="hlt">shock</span> pulses are predicted in simulations to provide more stable implosions and still achieve a low adiabat in the fuel, enabling a higher fuel <span class="hlt">compression</span> similar to ``low foot'' laser pulses. The first step in testing these predictions was to measure the <span class="hlt">shock</span> velocity for both a three <span class="hlt">shock</span> and a four <span class="hlt">shock</span> adiabat-shaped pulse in a keyhole experimental platform. We present measurements of the <span class="hlt">shock</span> velocity history, including the decaying <span class="hlt">shock</span> velocity inside the ablator, and compare it with simulations, as well as with previous low and high foot pulses. Using the measured pulse shape, the predicted adiabat from simulations is presented and compared with the calculated adiabat from low and high foot laser pulse shapes. This work was performed under the auspices of the U.S. Department of Energy by LLNL under Contract DE-AC52-07NA27344.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19740008381','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19740008381"><span>Terminal-<span class="hlt">shock</span> and restart control of a Mach 2.5, axisymmetric, mixed <span class="hlt">compression</span> inlet with 40 percent internal contraction. [wind tunnel tests</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Baumbick, R. J.</p> <p>1974-01-01</p> <p>Results of experimental tests conducted on a supersonic, mixed-<span class="hlt">compression</span>, axisymmetric inlet are presented. The inlet is designed for operation at Mach 2.5 with a turbofan engine (TF-30). The inlet was coupled to either a choked orifice plate or a long duct which had a variable-area choked exit plug. Closed-loop frequency responses of selected diffuser static pressures used in the terminal-<span class="hlt">shock</span> control system are presented. Results are shown for Mach 2.5 conditions with the inlet coupled to either the choked orifice plate or the long duct. Inlet unstart-restart traces are also presented. High-response inlet bypass doors were used to generate an internal disturbance and also to achieve terminal-<span class="hlt">shock</span> control.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_11");'>11</a></li> <li><a href="#" onclick='return showDiv("page_12");'>12</a></li> <li class="active"><span>13</span></li> <li><a href="#" onclick='return showDiv("page_14");'>14</a></li> <li><a href="#" onclick='return showDiv("page_15");'>15</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_13 --> <div id="page_14" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_12");'>12</a></li> <li><a href="#" onclick='return showDiv("page_13");'>13</a></li> <li class="active"><span>14</span></li> <li><a href="#" onclick='return showDiv("page_15");'>15</a></li> <li><a href="#" onclick='return showDiv("page_16");'>16</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="261"> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/23505053','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/23505053"><span><span class="hlt">Shock</span> wave treatment improves nerve regeneration in the rat.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Mense, Siegfried; Hoheisel, Ulrich</p> <p>2013-05-01</p> <p>The aims of the experiments were to: (1) determine whether low-energy <span class="hlt">shock</span> wave treatment accelerates the recovery of muscle sensitivity and functionality after a nerve lesion; and (2) assess the effect of <span class="hlt">shock</span> waves on the regeneration of injured nerve fibers. After <span class="hlt">compression</span> of a muscle nerve in rats the effects of <span class="hlt">shock</span> wave treatment on the sequelae of the lesion were tested. In non-anesthetized animals, pressure pain thresholds and exploratory activity were determined. The influence of the treatment on the distance of nerve regeneration was studied in immunohistochemical experiments. Both behavioral and immunohistochemical data show that <span class="hlt">shock</span> wave treatment accelerates the recovery of muscle sensitivity and functionality and promotes regeneration of injured nerve fibers. Treatment with focused <span class="hlt">shock</span> waves induces an improvement of nerve regeneration in a rodent model of nerve <span class="hlt">compression</span>. Copyright © 2012 Wiley Periodicals, Inc.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017AGUFMSH23C2674B','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017AGUFMSH23C2674B"><span>Survey of <span class="hlt">compressions</span> in the SW (1 AU), and after termination <span class="hlt">shock</span> at Voyager (in sheath & LISM)</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Berdichevsky, D. B.</p> <p>2017-12-01</p> <p>Examples of the plasma <span class="hlt">compression</span> as it is observed in the solar wind at 1 AU with the suite of instruments in the SC Wind, and after the termination <span class="hlt">shock</span> with both Voyager SC, as well as with Voyager 1 in the local interstellar medium (LISM) are presented. The work will focus on similarities and differences in the observations at the different locations. At priory is fair to mention that the 4 regions differ in several aspects. At 1 AU the solar wind (SW) flow is mostly alfvenic. In the sheath after the termination <span class="hlt">shock</span> the possibly subsonic solar wind is mostly compressional but fluctuation modes in scales of one hour are much less observed at Voyager 1 than at Voyager 2 path. Finally Burlaga and Ness1 documented the nature of the compressional flow in the `depletion' layer at the start of the LISM as well later in this medium, showing the low plasma-beta character of this LISM region in Voyager 1 path. 1Burlaga L.F., and N. Ness, ApJ, 784, 146 (14pp), 2014.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018JPhCS.946a2045E','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018JPhCS.946a2045E"><span>Influence of deposited nanoparticles on the spall strength of metals under the action of picosecond pulses of <span class="hlt">shock</span> <span class="hlt">compression</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Ebel, A. A.; Mayer, A. E.</p> <p>2018-01-01</p> <p>Molecular dynamic simulations of the generation and propagation of <span class="hlt">shock</span> pulses of picosecond duration initiated by nanoscale impactors, and their interaction with the rear surface is carried out for aluminum and copper. It is shown that the presence of deposited nanoparticles on the rear surface increases the threshold value of the impact intensity leading to the rear spallation. The interaction of a <span class="hlt">shock</span> wave with nanoparticles leads to severe plastic deformation in the surface layer of the metal including nanoparticles. A part of the <span class="hlt">compression</span> pulse energy is expended on the plastic deformation, which suppresses the spall fracture. Spallation threshold substantially increases at large diameters of deposited nanoparticles, but instability develops on the rear surface of the target, which is accompanied by ejection of droplets. The instability disrupts the integrity of the rear surface, though the loss of integrity occurs through the ejection of mass, rather than a spallation.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/22679545-combining-diffusive-shock-acceleration-acceleration-contracting-reconnecting-small-scale-flux-ropes-heliospheric-shocks','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/22679545-combining-diffusive-shock-acceleration-acceleration-contracting-reconnecting-small-scale-flux-ropes-heliospheric-shocks"><span>COMBINING DIFFUSIVE <span class="hlt">SHOCK</span> ACCELERATION WITH ACCELERATION BY CONTRACTING AND RECONNECTING SMALL-SCALE FLUX ROPES AT HELIOSPHERIC <span class="hlt">SHOCKS</span></span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Le Roux, J. A.; Zank, G. P.; Webb, G. M.</p> <p>2016-08-10</p> <p>Computational and observational evidence is accruing that heliospheric <span class="hlt">shocks</span>, as emitters of vorticity, can produce downstream magnetic flux ropes and filaments. This led Zank et al. to investigate a new paradigm whereby energetic particle acceleration near <span class="hlt">shocks</span> is a combination of diffusive <span class="hlt">shock</span> acceleration (DSA) with downstream acceleration by many small-scale contracting and reconnecting (merging) flux ropes. Using a model where flux-rope acceleration involves a first-order Fermi mechanism due to the mean <span class="hlt">compression</span> of numerous contracting flux ropes, Zank et al. provide theoretical support for observations that power-law spectra of energetic particles downstream of heliospheric <span class="hlt">shocks</span> can be harder thanmore » predicted by DSA theory and that energetic particle intensities should peak behind <span class="hlt">shocks</span> instead of at <span class="hlt">shocks</span> as predicted by DSA theory. In this paper, a more extended formalism of kinetic transport theory developed by le Roux et al. is used to further explore this paradigm. We describe how second-order Fermi acceleration, related to the variance in the electromagnetic fields produced by downstream small-scale flux-rope dynamics, modifies the standard DSA model. The results show that (i) this approach can qualitatively reproduce observations of particle intensities peaking behind the <span class="hlt">shock</span>, thus providing further support for the new paradigm, and (ii) stochastic acceleration by <span class="hlt">compressible</span> flux ropes tends to be more efficient than incompressible flux ropes behind <span class="hlt">shocks</span> in modifying the DSA spectrum of energetic particles.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2008IJMPB..22.1183B','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2008IJMPB..22.1183B"><span>Dynamic <span class="hlt">Compressibility</span> of High-Porosity Dampers of Thermal and <span class="hlt">Shock</span> Loadings:. Modeling and Experiment</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Bragov, Anatoly; Konstantinov, Alexander; Lomunov, Andrey; Sadyrin, Anatoly; Sergeichev, Ivan; Kruszka, Leopold</p> <p></p> <p>High-porosity materials, such as chamotte and mullite, possess a heat of fusion. Owing to their properties, these materials can be used with success as damping materials in containers for airplane, automobile, etc. transportation of radioactive or highly toxic materials. Experimental studies of the dynamic properties have been executed with using some original modifications of the Kolsky method. These modified experiments have allowed studying the dynamic <span class="hlt">compressibility</span> of high-porosity chamotte at deformations up to 80% and amplitudes up to 50 MPa. The equations of the mathematical model describing <span class="hlt">shock</span> compacting of chamotte as a highly porous, fragile, collapsing material are presented. Deformation of high-porous materials at non-stationary loadings is usually accompanied by fragile destruction of interpore partitions as observed in other porous ceramic materials. Comparison of numerical and experimental results has shown their good conformity.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19960003341','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19960003341"><span><span class="hlt">Shock</span> waves data for minerals</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Ahrens, Thomas J.; Johnson, Mary L.</p> <p>1994-01-01</p> <p><span class="hlt">Shock</span> <span class="hlt">compression</span> of the materials of planetary interiors yields data which upon comparison with density-pressure and density-sound velocity profiles constrain internal composition and temperature. Other important applications of <span class="hlt">shock</span> wave data and related properties are found in the impact mechanics of terrestrial planets and solid satellites. <span class="hlt">Shock</span> wave equation of state, <span class="hlt">shock</span>-induced dynamic yielding and phase transitions, and <span class="hlt">shock</span> temperature are discussed. In regions where a substantial phase change in the material does not occur, the relationship between the particle velocity, U(sub p), and the <span class="hlt">shock</span> velocity, U(sub s), is given by U(sub s) = C(sub 0) + S U(sub p), where C(sub 0) is the <span class="hlt">shock</span> velocity at infinitesimally small particle velocity, or the ambient pressure bulk sound velocity. Numerical values for the <span class="hlt">shock</span> wave equation of state for minerals and related materials of the solar system are provided.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016APS..DFD.G5004F','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016APS..DFD.G5004F"><span><span class="hlt">Shock</span> wave-free interface interaction</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Frolov, Roman; Minev, Peter; Krechetnikov, Rouslan</p> <p>2016-11-01</p> <p>The problem of <span class="hlt">shock</span> wave-free interface interaction has been widely studied in the context of <span class="hlt">compressible</span> two-fluid flows using analytical, experimental, and numerical techniques. While various physical effects and possible interaction patterns for various geometries have been identified in the literature, the effects of viscosity and surface tension are usually neglected in such models. In our study, we apply a novel numerical algorithm for simulation of viscous <span class="hlt">compressible</span> two-fluid flows with surface tension to investigate the influence of these effects on the <span class="hlt">shock</span>-interface interaction. The method combines together the ideas from Finite Volume adaptation of invariant domains preserving algorithm for systems of hyperbolic conservation laws by Guermond and Popov and ADI parallel solver for viscous incompressible NSEs by Guermond and Minev. This combination has been further extended to a two-fluid flow case, including surface tension effects. Here we report on a quantitative study of how surface tension and viscosity affect the structure of the <span class="hlt">shock</span> wave-free interface interaction region.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/22038552-mach-bow-shock-control-nanosecond-pulse-surface-dielectric-barrier-discharge','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/22038552-mach-bow-shock-control-nanosecond-pulse-surface-dielectric-barrier-discharge"><span>Mach 5 bow <span class="hlt">shock</span> control by a nanosecond pulse surface dielectric barrier discharge</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Nishihara, M.; Takashima, K.; Rich, J. W.</p> <p>2011-06-15</p> <p>Bow <span class="hlt">shock</span> perturbations in a Mach 5 air flow, produced by low-temperature, nanosecond pulse, and surface dielectric barrier discharge (DBD), are detected by phase-locked schlieren imaging. A diffuse nanosecond pulse discharge is generated in a DBD plasma actuator on a surface of a cylinder model placed in air flow in a small scale blow-down supersonic wind tunnel. Discharge energy coupled to the actuator is 7.3-7.8 mJ/pulse. Plasma temperature inferred from nitrogen emission spectra is a few tens of degrees higher than flow stagnation temperature, T = 340 {+-} 30 K. Phase-locked Schlieren images are used to detect <span class="hlt">compression</span> waves generatedmore » by individual nanosecond discharge pulses near the actuator surface. The <span class="hlt">compression</span> wave propagates upstream toward the baseline bow <span class="hlt">shock</span> standing in front of the cylinder model. Interaction of the <span class="hlt">compression</span> wave and the bow <span class="hlt">shock</span> causes its displacement in the upstream direction, increasing <span class="hlt">shock</span> stand-off distance by up to 25%. The <span class="hlt">compression</span> wave speed behind the bow <span class="hlt">shock</span> and the perturbed bow <span class="hlt">shock</span> velocity are inferred from the Schlieren images. The effect of <span class="hlt">compression</span> waves generated by nanosecond discharge pulses on <span class="hlt">shock</span> stand-off distance is demonstrated in a single-pulse regime (at pulse repetition rates of a few hundred Hz) and in a quasi-continuous mode (using a two-pulse sequence at a pulse repetition rate of 100 kHz). The results demonstrate feasibility of hypersonic flow control by low-temperature, repetitive nanosecond pulse discharges.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=20000116526&hterms=Notebook+Computers&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D50%26Ntt%3DNotebook%2BComputers.','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=20000116526&hterms=Notebook+Computers&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D50%26Ntt%3DNotebook%2BComputers."><span>Adiabatic <span class="hlt">Compression</span> Sensitivity of Liquid Fuels and Monopropellants</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Ismail, Ismail M. K.; Hawkins, Tom W.</p> <p>2000-01-01</p> <p>Liquid rocket propellants can be sensitive to rapid <span class="hlt">compression</span>. Such liquids may undergo decomposition and their handling may be accompanied with risk. Decomposition produces small gas bubbles in the liquid, which upon rapid <span class="hlt">compression</span> may cause catastrophic explosions. The rapid <span class="hlt">compression</span> can result from mechanical <span class="hlt">shocks</span> applied on the tank containing the liquid or from rapid closure of the valves installed on the lines. It is desirable to determine the conditions that may promote explosive reactions. At Air Force Research Laboratory (AFRL), we constructed an apparatus and established a safe procedure for estimating the sensitivity of propellant materials towards mechanical <span class="hlt">shocks</span> (Adiabatic <span class="hlt">Compression</span> Tester). A sample is placed on a stainless steel U-tube, held isothermally at a temperature between 20 and 150 C then exposed to an abrupt mechanical <span class="hlt">shock</span> of nitrogen gas at a pressure between 6.9 and 20.7 MPa (1000 to 3000 psi). The apparatus is computer interfaced and is driven with LABTECH NOTEBOOK-pro (registered) Software. In this presentation, the design of the apparatus is shown, the operating procedure is outlined, and the safety issues are addressed. The results obtained on different energetic materials are presented.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/1340520','SCIGOV-STC'); return false;" href="https://www.osti.gov/servlets/purl/1340520"><span><span class="hlt">Shock</span> formation in Ne, Ar, Kr, and Xe on deuterium gas puff implosions</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Narkis, J.; Rahman, H. U.; Ney, P.</p> <p>2016-12-29</p> <p>1- and 2-D simulations of 1-cm radius, gas-puff liners of Ne, Ar, Kr, and Xe imploding onto a deuterium target are conducted using the discharge parameters for the Zebra (1 MA, 130 ns) driver using the resistive MHD code MACH2. This is an implementation of the Staged Z-pinch concept, in which the target is driven to high-energy-density first by <span class="hlt">shock</span> <span class="hlt">compression</span> launched by a diffused azimuthal magnetic field (J×B force), and then by the adiabatic <span class="hlt">compression</span> as the liner converges on axis. During the run-in phase, the initial <span class="hlt">shock</span> heating preheats the deuterium plasma, with a subsequent stable, adiabatic compressionmore » heating the target to high energy density. <span class="hlt">Shock</span> <span class="hlt">compression</span> of the target coincides with the development of a J×B force at the target/liner interface. Stronger B-field transport and earlier <span class="hlt">shock</span> <span class="hlt">compression</span> increases with higher-Z liners, which results in an earlier <span class="hlt">shock</span> arrival on axis. As a result, delayed <span class="hlt">shock</span> formation in lower-Z liners yields a relative increase in <span class="hlt">shock</span> heating, however, the 2-D simulations show an increased target isolation from magneto-Rayleigh-Taylor instability penetration, suggesting that an optimal balance between these two effects is reached in an Ar or Kr liner, rather than with Xe.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/865325','DOE-PATENT-XML'); return false;" href="https://www.osti.gov/servlets/purl/865325"><span>Isentropic <span class="hlt">compressive</span> wave generator impact pillow and method of making same</span></a></p> <p><a target="_blank" href="http://www.osti.gov/doepatents">DOEpatents</a></p> <p>Barker, Lynn M.</p> <p>1985-01-01</p> <p>An isentropic <span class="hlt">compressive</span> wave generator and method of making same. The w generator comprises a disk or flat "pillow" member having component materials of different <span class="hlt">shock</span> impedances formed in a configuration resulting in a smooth <span class="hlt">shock</span> impedance gradient over the thickness thereof for interpositioning between an impactor member and a target specimen for producing a <span class="hlt">shock</span> wave of a smooth predictable rise time. The method of making the pillow member comprises the reduction of the component materials to a powder form and forming the pillow member by sedimentation and <span class="hlt">compressive</span> techniques.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1099255-probing-interiors-ice-giants-shock-compression-water-gpa-cm','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1099255-probing-interiors-ice-giants-shock-compression-water-gpa-cm"><span>Probing the Interiors of the Ice Giants: <span class="hlt">Shock</span> <span class="hlt">Compression</span> of Water to 700 GPa and 3.8 g/cm³</span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>Knudson, M. D.; Desjarlais, M. P.; Lemke, R. W.; ...</p> <p>2012-02-27</p> <p>Recently, there has been a tremendous increase in the number of identified extrasolar planetary systems. Our understanding of their formation is tied to exoplanet internal structure models, which rely upon equations of state of light elements and compounds such as water. Here, we present <span class="hlt">shock</span> <span class="hlt">compression</span> data for water with unprecedented accuracy that show that water equations of state commonly used in planetary modeling significantly overestimate the <span class="hlt">compressibility</span> at conditions relevant to planetary interiors. Furthermore, we show that its behavior at these conditions, including reflectivity and isentropic response, is well-described by a recent first-principles based equation of state. These findingsmore » advocate that this water model be used as the standard for modeling Neptune, Uranus, and “hot Neptune” exoplanets and should improve our understanding of these types of planets.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19720046519&hterms=induction+melting&qs=N%3D0%26Ntk%3DAll%26Ntx%3Dmode%2Bmatchall%26Ntt%3Dinduction%2Bmelting','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19720046519&hterms=induction+melting&qs=N%3D0%26Ntk%3DAll%26Ntx%3Dmode%2Bmatchall%26Ntt%3Dinduction%2Bmelting"><span><span class="hlt">Shock</span> melting and vaporization of metals.</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Ahrens, T. J.</p> <p>1972-01-01</p> <p>The effect of initial porosity on <span class="hlt">shock</span> induction of melting and vaporization is investigated for Ba, Sr, Li, Fe, Al, U, and Th. For the less <span class="hlt">compressible</span> of these metals, it is found that for a given strong <span class="hlt">shock</span>-generation system (explosive in contact, or flyer-plate impact) an optimum initial specific volume exists such that the total entropy production, and hence the amount of metal liquid or vapor, is a maximum. Initial volumes from 1.4 to 2.0 times crystal volumes, depending on the metal sample and <span class="hlt">shock</span>-inducing system, will result in optimum post-<span class="hlt">shock</span> entropies.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19960050025','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19960050025"><span>Computation of Thermally Perfect Properties of Oblique <span class="hlt">Shock</span> Waves</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Tatum, Kenneth E.</p> <p>1996-01-01</p> <p>A set of <span class="hlt">compressible</span> flow relations describing flow properties across oblique <span class="hlt">shock</span> waves, derived for a thermally perfect, calorically imperfect gas, is applied within the existing thermally perfect gas (TPG) computer code. The relations are based upon a value of cp expressed as a polynomial function of temperature. The updated code produces tables of <span class="hlt">compressible</span> flow properties of oblique <span class="hlt">shock</span> waves, as well as the original properties of normal <span class="hlt">shock</span> waves and basic isentropic flow, in a format similar to the tables for normal <span class="hlt">shock</span> waves found in NACA Rep. 1135. The code results are validated in both the calorically perfect and the calorically imperfect, thermally perfect temperature regimes through comparisons with the theoretical methods of NACA Rep. 1135, and with a state-of-the-art computational fluid dynamics code. The advantages of the TPG code for oblique <span class="hlt">shock</span> wave calculations, as well as for the properties of isentropic flow and normal <span class="hlt">shock</span> waves, are its ease of use, and its applicability to any type of gas (monatomic, diatomic, triatomic, polyatomic, or any specified mixture thereof).</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2011PMM...112..535E','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2011PMM...112..535E"><span>Semiempirical models for description of shear modulus in wide ranges of temperatures and pressures of <span class="hlt">shock</span> <span class="hlt">compression</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>El'Kin, V. M.; Mikhailov, V. N.; Mikhailova, T. Yu.</p> <p>2011-12-01</p> <p>In this paper, we discuss the potentials of the Steinberg-Cochran-Guinan (SCG) and Burakovsky-Preston (BP) models for the description of the shear-modulus behavior at temperatures and pressures that arise behind the <span class="hlt">shock</span>-wave front. A modernized variant of the SCG model is suggested, which reduces to the introduction of a free parameter and the representation of the model in the volume-temperature coordinates (( V, T) model). A systematic comparison is performed of all three models of shear modulus with experimental data and data of ab initio calculations for metals such as Al, Be, Cu, K, Na, Mg, Mo, W, and Ta in a wide range of pressures. In addition, for Al, Cu, Mo, W, and Ta there is performed a comparison with the known temperature dependences of the shear modulus and with the results of measurements of the velocities of longitudinal sound behind the <span class="hlt">shock</span>-wave front. It is shown that in the original form the SCG and BP models give overestimated values of the shear modulus as compared to the data of ab initio calculations and <span class="hlt">shock</span>-wave experiments. The ( V, T) model, due to the use of a free parameter, makes it possible to optimally describe the totality of experimental and calculated data. The same result is achieved in the case of the BP model after a redefining of its initial parameters. The adequate description of the shear modulus in the range of high intermediate pressures characteristic of the solid-phase states behind the <span class="hlt">shock</span>-wave front is accompanied in both cases by the violation of the correct asymptotic behavior of the shear modulus at ultrahigh <span class="hlt">compressions</span> which is originally laid into the SCG and BP models.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2009PhRvB..79q4108M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2009PhRvB..79q4108M"><span>Metallization of aluminum hydride AlH3 at high multiple-<span class="hlt">shock</span> pressures</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Molodets, A. M.; Shakhray, D. V.; Khrapak, A. G.; Fortov, V. E.</p> <p>2009-05-01</p> <p>A study of electrophysical and thermodynamic properties of alane AlH3 under multishock <span class="hlt">compression</span> has been carried out. The increase in specific electroconductivity of alane at <span class="hlt">shock</span> <span class="hlt">compression</span> up to pressure 100 GPa has been measured. High pressures and temperatures were obtained with an explosive device, which accelerates the stainless impactor up to 3 km/s. A strong <span class="hlt">shock</span> wave is generated on impact with a holder containing alane. The impact <span class="hlt">shock</span> is split into a <span class="hlt">shock</span> wave reverberating in alane between two stiff metal anvils. This <span class="hlt">compression</span> loads the alane sample by a multishock manner up to pressure 80-90 GPa, heats alane to the temperature of about 1500-2000 K, and lasts 1μs . The conductivity of <span class="hlt">shocked</span> alane increases in the range up to 60-75 GPa and is about 30(Ωcm)-1 . In this region the semiconductor regime is true for <span class="hlt">shocked</span> alane. The conductivity of alane achieves approximately 500(Ωcm)-1 at 80-90 GPa. In this region, conductivity is interpreted in frames of the conception of the “dielectric catastrophe,” taking into consideration significant differences between the electronic states of isolated molecule AlH3 and condensed alane.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19680000266','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19680000266"><span><span class="hlt">Shock</span>-absorbing caster wheel is simple and compact</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Kindley, R. J.</p> <p>1968-01-01</p> <p>Compact <span class="hlt">shock</span>-absorbing caster wheel mitigates or absorbs <span class="hlt">shock</span> by a <span class="hlt">compressible</span> tire which deforms into a cavity between its inner edge and the wheel hub. A tee-shaped annular ring embedded in the tire distributes loads more uniformly throughout both wheel and tire.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/17718475','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/17718475"><span><span class="hlt">Shock</span> wave-induced phase transition in RDX single crystals.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Patterson, James E; Dreger, Zbigniew A; Gupta, Yogendra M</p> <p>2007-09-20</p> <p>The real-time, molecular-level response of oriented single crystals of hexahydro-1,3,5-trinitro-s-triazine (RDX) to <span class="hlt">shock</span> <span class="hlt">compression</span> was examined using Raman spectroscopy. Single crystals of [111], [210], or [100] orientation were <span class="hlt">shocked</span> under stepwise loading to peak stresses from 3.0 to 5.5 GPa. Two types of measurements were performed: (i) high-resolution Raman spectroscopy to probe the material at peak stress and (ii) time-resolved Raman spectroscopy to monitor the evolution of molecular changes as the <span class="hlt">shock</span> wave reverberated through the material. The frequency shift of the CH stretching modes under <span class="hlt">shock</span> loading appeared to be similar for all three crystal orientations below 3.5 GPa. Significant spectral changes were observed in crystals <span class="hlt">shocked</span> above 4.5 GPa. These changes were similar to those observed in static pressure measurements, indicating the occurrence of the alpha-gamma phase transition in <span class="hlt">shocked</span> RDX crystals. No apparent orientation dependence in the molecular response of RDX to <span class="hlt">shock</span> <span class="hlt">compression</span> up to 5.5 GPa was observed. The phase transition had an incubation time of approximately 100 ns when RDX was <span class="hlt">shocked</span> to 5.5 GPa peak stress. The observation of the alpha-gamma phase transition under <span class="hlt">shock</span> wave loading is briefly discussed in connection with the onset of chemical decomposition in <span class="hlt">shocked</span> RDX.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2014TePhL..40.1003B','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2014TePhL..40.1003B"><span>An electromagnetic railgun accelerator: a generator of strong <span class="hlt">shock</span> waves in channels</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Bobashev, S. V.; Zhukov, B. G.; Kurakin, R. O.; Ponyaev, S. A.; Reznikov, B. I.</p> <p>2014-11-01</p> <p>Processes that accompany the generation of strong <span class="hlt">shock</span> waves during the acceleration of a free plasma piston (PP) in the electromagnetic railgun channel have been experimentally studied. The formation of <span class="hlt">shock</span> waves in the railgun channel and the motion of a <span class="hlt">shock-wave-compressed</span> layer proceed (in contrast to the case of a classical <span class="hlt">shock</span> tube) in a rather strong electric field (up to 300 V/cm). The experiments were performed at the initial gas pressures in the channel ranging from 25 to 500 Torr. At 25 Torr, the <span class="hlt">shock</span>-wave Mach numbers reached 32 in argon and 16 in helium. At high concentrations of charged particles behind the <span class="hlt">shock</span> wave, the electric field causes the passage of a part of the discharge current through the volume of the <span class="hlt">shock-wave-compressed</span> layer, which induces intense glow comparable with that of the PP glow.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016JAP...120l5902S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016JAP...120l5902S"><span>High precision Hugoniot measurements on statically pre-<span class="hlt">compressed</span> fluid helium</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Seagle, Christopher T.; Reinhart, William D.; Lopez, Andrew J.; Hickman, Randy J.; Thornhill, Tom F.</p> <p>2016-09-01</p> <p>The capability for statically pre-<span class="hlt">compressing</span> fluid targets for Hugoniot measurements utilizing gas gun driven flyer plates has been developed. Pre-<span class="hlt">compression</span> expands the capability for initial condition control, allowing access to thermodynamic states off the principal Hugoniot. Absolute Hugoniot measurements with an uncertainty less than 3% on density and pressure were obtained on statically pre-<span class="hlt">compressed</span> fluid helium utilizing a two stage light gas gun. Helium is highly <span class="hlt">compressible</span>; the locus of <span class="hlt">shock</span> states resulting from dynamic loading of an initially <span class="hlt">compressed</span> sample at room temperature is significantly denser than the cryogenic fluid Hugoniot even for relatively modest (0.27-0.38 GPa) initial pressures. The dynamic response of pre-<span class="hlt">compressed</span> helium in the initial density range of 0.21-0.25 g/cm3 at ambient temperature may be described by a linear <span class="hlt">shock</span> velocity (us) and particle velocity (up) relationship: us = C0 + sup, with C0 = 1.44 ± 0.14 km/s and s = 1.344 ± 0.025.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_12");'>12</a></li> <li><a href="#" onclick='return showDiv("page_13");'>13</a></li> <li class="active"><span>14</span></li> <li><a href="#" onclick='return showDiv("page_15");'>15</a></li> <li><a href="#" onclick='return showDiv("page_16");'>16</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_14 --> <div id="page_15" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_13");'>13</a></li> <li><a href="#" onclick='return showDiv("page_14");'>14</a></li> <li class="active"><span>15</span></li> <li><a href="#" onclick='return showDiv("page_16");'>16</a></li> <li><a href="#" onclick='return showDiv("page_17");'>17</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="281"> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/22402618-dislocation-structure-produced-ultrashort-shock-pulse','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/22402618-dislocation-structure-produced-ultrashort-shock-pulse"><span>Dislocation structure produced by an ultrashort <span class="hlt">shock</span> pulse</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Matsuda, Tomoki, E-mail: t-matsu@mapse.eng.osaka-u.ac.jp; Hirose, Akio; Sano, Tomokazu</p> <p></p> <p>We found an ultrashort <span class="hlt">shock</span> pulse driven by a femtosecond laser pulse on <span class="hlt">iron</span> generates a different dislocation structure than the <span class="hlt">shock</span> process which is on the nanosecond timescale. The ultrashort <span class="hlt">shock</span> pulse produces a highly dense dislocation structure that varies by depth. According to transmission electron microscopy, dislocations away from the surface produce microbands via a network structure similar to a long <span class="hlt">shock</span> process, but unlike a long <span class="hlt">shock</span> process dislocations near the surface have limited intersections. Considering the dislocation motion during the <span class="hlt">shock</span> process, the structure near the surface is attributed to the ultrashort <span class="hlt">shock</span> duration. This approachmore » using an ultrashort <span class="hlt">shock</span> pulse will lead to understanding the whole process off <span class="hlt">shock</span> deformation by clarifying the early stage.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017APS..SHK.J3004S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017APS..SHK.J3004S"><span>Numerical predictions of <span class="hlt">shock</span> propagation through unreactive and reactive liquids with experimental validation</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Stekovic, Svjetlana; Nissen, Erin; Bhowmick, Mithun; Stewart, Donald S.; Dlott, Dana D.</p> <p>2017-06-01</p> <p>The objective of this work is to numerically analyze <span class="hlt">shock</span> behavior as it propagates through <span class="hlt">compressed</span>, unreactive and reactive liquid, such as liquid water and liquid nitromethane. Parameters, such as pressure and density, are analyzed using the Mie-Gruneisen EOS and each multi-material system is modeled using the ALE3D software. The motivation for this study is based on provided high-resolution, optical interferometer (PDV) and optical pyrometer measurements. In the experimental set-up, a liquid is placed between an Al 1100 plate and Pyrex BK-7 glass. A laser-driven Al 1100 flyer impacts the plate, causing the liquid to be highly <span class="hlt">compressed</span>. The numerical model investigates the influence of the high pressure, <span class="hlt">shock-compressed</span> behavior in each liquid, the energy transfer, and the wave impedance at the interface of each material in contact. The numerical results using ALE3D will be validated by experimental data. This work aims to provide further understanding of <span class="hlt">shock-compressed</span> behavior and how the <span class="hlt">shock</span> influences phase transition in each liquid.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/1999APS..DFD..JG05E','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/1999APS..DFD..JG05E"><span><span class="hlt">Compressible</span> Vortex Ring</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Elavarasan, Ramasamy; Arakeri, Jayawant; Krothapalli, Anjaneyulu</p> <p>1999-11-01</p> <p>The interaction of a high-speed vortex ring with a <span class="hlt">shock</span> wave is one of the fundamental issues as it is a source of sound in supersonic jets. The complex flow field induced by the vortex alters the propagation of the <span class="hlt">shock</span> wave greatly. In order to understand the process, a <span class="hlt">compressible</span> vortex ring is studied in detail using Particle Image Velocimetry (PIV) and shadowgraphic techniques. The high-speed vortex ring is generated from a <span class="hlt">shock</span> tube and the <span class="hlt">shock</span> wave, which precedes the vortex, is reflected back by a plate and made to interact with the vortex. The shadowgraph images indicate that the reflected <span class="hlt">shock</span> front is influenced by the non-uniform flow induced by the vortex and is decelerated while passing through the vortex. It appears that after the interaction the <span class="hlt">shock</span> is "split" into two. The PIV measurements provided clear picture about the evolution of the vortex at different time interval. The centerline velocity traces show the maximum velocity to be around 350 m/s. The velocity field, unlike in incompressible rings, contains contributions from both the <span class="hlt">shock</span> and the vortex ring. The velocity distribution across the vortex core, core diameter and circulation are also calculated from the PIV data.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/23421276','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/23421276"><span><span class="hlt">Shock</span> induced reaction of Ni/Al nanopowder mixture.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Meng, C M; Wei, J J; Chen, Q Y</p> <p>2012-11-01</p> <p>Nanopowder Ni/Al mixture (mixed in Al:Ni = 2:1 stoichiometry) was <span class="hlt">shock</span> <span class="hlt">compressed</span> by employing single and two-stage light gas gun. The particle size of Al and Ni are 100-200 nm and 50-70 nm respectively, morphologies of Al and Ni are sphere like either. Recovered product was characterized by scanning electron microscope (SEM) and X-ray diffraction (XRD) analysis. According to the XRD spectrum, the mixed powder undergo complete reaction under <span class="hlt">shock</span> <span class="hlt">compression</span>, reaction product consist of Ni2Al3, NiAl and corundum structure Al2O3 compound. Grain size of Ni-Al compound is less than 100 nm. With the <span class="hlt">shock</span> pressure increasing, the ratio of Ni2Al3 decreased obviously. The corundum crystal size is 400-500 nm according to the SEM observation. The results of <span class="hlt">shock</span> recovery experiments and analysis show that the threshold pressure for reaction of nano size powder Ni/Al mixture is much less than that of micro size powder.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/1999APS..SHK..B201B','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/1999APS..SHK..B201B"><span><span class="hlt">Shock-Compressed</span> Hydrogen</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Bickham, S. R.; Collins, L. A.; Kress, J. D.; Lenosky, T. J.</p> <p>1999-06-01</p> <p>To investigate recent gas-gun and laser experiments on hydrogen at elevated temperatures and high densities, we have performed quantum molecular dynamics simulations using a variety of sophisticated models, ranging from tight-binding(TB) to density functional(DF)(T.J. Lenosky, J.D. Kress, L.A. Collins, and I. Kwon Phys. Rev. B 55), R11907(1997) and references therein.. The TB models have been especially tailored to reproduce experimental findings, such as Diamond-Anvil Cell data, and ab initio calculations, such as H_2, H_3, and H4 potential energy surfaces. The DF calculations have employed the local-density approximation(LDA) as well as generalized gradient corrections(GGA) with large numbers of plane-waves ( ~10^5) that represent a very broad range of excited and continuum electronic states. Good agreement obtains among all these models. The simulations exhibit a rapidly rising electrical conductivity at low temperatures and high pressures in good agreement with the gas-gun results. This conduction property stems from a mobility of the electrons provided principally by the dissociated monomers. The Hugoniot for the conditions of the laser experiment, generated from the TB Equation-of-State, shows a maximum <span class="hlt">compression</span> of around four instead of the observed six. We also report optical properties of the hydrogen media.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016PhRvL.116d8101T','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016PhRvL.116d8101T"><span>Density <span class="hlt">Shock</span> Waves in Confined Microswimmers</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Tsang, Alan Cheng Hou; Kanso, Eva</p> <p>2016-01-01</p> <p>Motile and driven particles confined in microfluidic channels exhibit interesting emergent behavior, from propagating density bands to density <span class="hlt">shock</span> waves. A deeper understanding of the physical mechanisms responsible for these emergent structures is relevant to a number of physical and biomedical applications. Here, we study the formation of density <span class="hlt">shock</span> waves in the context of an idealized model of microswimmers confined in a narrow channel and subject to a uniform external flow. Interestingly, these density <span class="hlt">shock</span> waves exhibit a transition from "subsonic" with <span class="hlt">compression</span> at the back to "supersonic" with <span class="hlt">compression</span> at the front of the population as the intensity of the external flow increases. This behavior is the result of a nontrivial interplay between hydrodynamic interactions and geometric confinement, and it is confirmed by a novel quasilinear wave model that properly captures the dependence of the <span class="hlt">shock</span> formation on the external flow. These findings can be used to guide the development of novel mechanisms for controlling the emergent density distribution and the average population speed, with potentially profound implications on various processes in industry and biotechnology, such as the transport and sorting of cells in flow channels.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018PhPl...25d2111I','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018PhPl...25d2111I"><span>Existence regimes for <span class="hlt">shocks</span> in inhomogeneous magneto-plasmas having entropy</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Iqbal, Javed; Yaqub Khan, M.</p> <p>2018-04-01</p> <p>The finding of connection of plasma density and temperature with entropy gives an incitement to study different plasma models with respect to entropy. Nonlinear dissipative one- and two-dimensional structures (<span class="hlt">shocks</span>) are investigated in nonuniform magnetized plasma with respect to entropy. The dissipation comes in the medium through ion-neutral collisions. The linear dispersion relation is derived. The Korteweg-deVries-Burgers and Kadomtsev-Petviashvili-Burgers equations are derived for nonlinear drift waves in 1-D and 2-D by employing the drift approximation. It is found that vd/u ( vd is the diamagnetic drift velocity and u is the velocity of nonlinear structure) plays a significant role in the <span class="hlt">shock</span> formation. It is also found that entropy has a significant effect on the strength of <span class="hlt">shocks</span>. It is noticed that v d/u determines the rarefactive and <span class="hlt">compressive</span> nature of the <span class="hlt">shocks</span>. It is observed that upper and lower bounds exist for the <span class="hlt">shock</span> velocity. It is also observed that the existing regimes for both one- and two-dimensional <span class="hlt">shocks</span> for kappa distributed electrons are different from <span class="hlt">shocks</span> with Cairns distributed electrons. Both rarefactive and <span class="hlt">compressive</span> <span class="hlt">shocks</span> are found for the 1-D drift waves with kappa distributed electrons. Interestingly, it is noticed that entropy enhances the strength of one- and two-dimensional <span class="hlt">shocks</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1260498-new-experimental-platform-study-high-density-laser-compressed-matter','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1260498-new-experimental-platform-study-high-density-laser-compressed-matter"><span>New experimental platform to study high density laser-<span class="hlt">compressed</span> matter</span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>Doppner, T.; LePape, S.; Ma, T.; ...</p> <p>2014-09-26</p> <p>We have developed a new experimental platform at the Linac Coherent Light Source (LCLS) which combines simultaneous angularly and spectrally resolved x-ray scatteringmeasurements. This technique offers a new insights on the structural and thermodynamic properties of warm dense matter. The < 50 fs temporal duration of the x-ray pulse provides near instantaneous snapshots of the dynamics of the <span class="hlt">compression</span>. We present a proof of principle experiment for this platform to characterize a <span class="hlt">shock-compressed</span> plastic foil. We observe the disappearance of the plastic semi-crystal structure and the formation of a <span class="hlt">compressed</span> liquid ion-ion correlation peak. As a result, the plasma parametersmore » of <span class="hlt">shock-compressed</span> plastic can be measured as well, but requires an averaging over a few tens of shots.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5125102','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5125102"><span>Superstrength of nanograined steel with nanoscale intermetallic precipitates transformed from <span class="hlt">shock-compressed</span> martensitic steel</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Yu, Hailiang; Yan, Ming; Lu, Cheng; Tieu, Anh Kiet; Li, Huijun; Zhu, Qiang; Godbole, Ajit; Li, Jintao; Su, Lihong; Kong, Charlie</p> <p>2016-01-01</p> <p>An increasing number of industrial applications need superstrength steels. It is known that refined grains and nanoscale precipitates can increase strength. The hardest martensitic steel reported to date is C0.8 steel, whose nanohardness can reach 11.9 GPa through incremental interstitial solid solution strengthening. Here we report a nanograined (NG) steel dispersed with nanoscale precipitates which has an extraordinarily high hardness of 19.1 GPa. The NG steel (<span class="hlt">shock-compressed</span> Armox 500T steel) was obtained under these conditions: high strain rate of 1.2 μs−1, high temperature rise rate of 600 Kμs−1 and high pressure of 17 GPa. The mean grain size achieved was 39 nm and reinforcing precipitates were indexed in the NG steel. The strength of the NG steel is expected to be ~3950 MPa. The discovery of the NG steel offers a general pathway for designing new advanced steel materials with exceptional hardness and excellent strength. PMID:27892460</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19980039333','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19980039333"><span>Studies of <span class="hlt">Shock</span> Wave Interactions with Homogeneous and Isotropic Turbulence</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Briassulis, G.; Agui, J.; Watkins, C. B.; Andreopoulos, Y.</p> <p>1998-01-01</p> <p>A nearly homogeneous nearly isotropic <span class="hlt">compressible</span> turbulent flow interacting with a normal <span class="hlt">shock</span> wave has been studied experimentally in a large <span class="hlt">shock</span> tube facility. Spatial resolution of the order of 8 Kolmogorov viscous length scales was achieved in the measurements of turbulence. A variety of turbulence generating grids provide a wide range of turbulence scales. Integral length scales were found to substantially decrease through the interaction with the <span class="hlt">shock</span> wave in all investigated cases with flow Mach numbers ranging from 0.3 to 0.7 and <span class="hlt">shock</span> Mach numbers from 1.2 to 1.6. The outcome of the interaction depends strongly on the state of <span class="hlt">compressibility</span> of the incoming turbulence. The length scales in the lateral direction are amplified at small Mach numbers and attenuated at large Mach numbers. Even at large Mach numbers amplification of lateral length scales has been observed in the case of fine grids. In addition to the interaction with the <span class="hlt">shock</span> the present work has documented substantial <span class="hlt">compressibility</span> effects in the incoming homogeneous and isotropic turbulent flow. The decay of Mach number fluctuations was found to follow a power law similar to that describing the decay of incompressible isotropic turbulence. It was found that the decay coefficient and the decay exponent decrease with increasing Mach number while the virtual origin increases with increasing Mach number. A mechanism possibly responsible for these effects appears to be the inherently low growth rate of <span class="hlt">compressible</span> shear layers emanating from the cylindrical rods of the grid.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/1342845','SCIGOV-STC'); return false;" href="https://www.osti.gov/servlets/purl/1342845"><span>Introduction to <span class="hlt">Shock</span> Waves and <span class="hlt">Shock</span> Wave Research</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Anderson, William Wyatt</p> <p>2017-02-02</p> <p>M-9 and a number of other organizations at LANL and elsewhere study materials in dynamic processes. Often, this is described as “<span class="hlt">shock</span> wave research,” but in reality is broader than is implied by that term. Most of our work is focused on dynamic <span class="hlt">compression</span> and associated phenomena, but you will find a wide variety of things we do that, while related, are not simple <span class="hlt">compression</span> of materials, but involve a much richer variety of phenomena. This tutorial will introduce some of the underlying physics involved in this work, some of the more common types of phenomena we study, and commonmore » techniques. However, the list will not be exhaustive by any means.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/10143579','SCIGOV-STC'); return false;" href="https://www.osti.gov/servlets/purl/10143579"><span>Structures and properties of materials recovered from high <span class="hlt">shock</span> pressures</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Nellis, W.J.</p> <p>1994-03-01</p> <p><span class="hlt">Shock</span> <span class="hlt">compression</span> produces high dynamic pressures, densities, temperatures, and their quench rates. Because of these extreme conditions, <span class="hlt">shock</span> <span class="hlt">compression</span> produces materials with novel crystal structures, microstructures, and physical properties. Using a 6.5-m-long two-stage gun, we perform experiments with specimens up to 10 mm in diameter and 0.001--1 mm thick. For example, oriented disks of melt-textured superconducting YBa{sub 2}Cu{sub 3}O{sub 7} were <span class="hlt">shocked</span> to 7 GPa without macroscopic fracture. Lattice defects are deposited in the crystal, which improve magnetic hysteresis at {approximately}1 kOe. A computer code has been developed to simulate <span class="hlt">shock</span> compaction of 100 powder particles. Computations will be comparedmore » with experiments with 15--20 {mu}m Cu powders. The method is applicable to other powders and dynamic conditions.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/1999APS..SHK..B205H','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/1999APS..SHK..B205H"><span>Sound velocities in <span class="hlt">shocked</span> liquid D2 to 28 GPa</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Holmes, N. C.; Ross, M.; Nellis, W. J.</p> <p>1999-06-01</p> <p>Recent measurements of <span class="hlt">shock</span> temperatures(N. C. Holmes, W. J. Nellis, and M. Ross, Phys. Rev.) B52, 15835 (1995). and laser-driven Hugoniot measurements(L. B. Da Silva, et al.), Phys. Rev. Lett. 78, 483 (1997). of <span class="hlt">shocked</span> liquid deuterium strongly indicate that molecular dissociation is important above 20 GPa. Since the amount of expected dissociation is small on the Hugoniot at the 30 GPa limit of conventional impact experiments, other methods must be used to test our understanding of the physics of highly <span class="hlt">compressed</span> deuterium in this regime. We have recently performed experiments to measure the sound velocity of deuterium which test the isentropic <span class="hlt">compressibility</span>, c^2 = (partial P/partial ρ)_S. We used the <span class="hlt">shock</span> overtake method to measure sound velocities at several <span class="hlt">shock</span> pressures between 10--28 GPa. These data provide support for recently developed molecular dissociation models.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017JPhCS.927a2078Z','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017JPhCS.927a2078Z"><span>Generation of quasi-perpendicular Collisionless <span class="hlt">Shocks</span> by Laser-Produced Plasma to simulate the effects of super-<span class="hlt">compression</span> of the Earth’s magnetosphere</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Zakharov, Yu P.; Ponomarenko, A. G.; Terekhin, V. A.; Golubev, A. I.; Antonov, V. M.; Boyarintsev, E. L.; Vchivkov, K. V.; Melekhov, A. V.; Posukh, V. G.; Prokopov, P. A.</p> <p>2017-11-01</p> <p>Giant plasma releases of so called Coronal Mass Ejections (CME, with kinetic energy up to Ek ∼ 1036 эрг) from the surface of the Sun and their potential catastrophical impact onto Earth’s magnetosphere, with the probable opportunity to <span class="hlt">compress</span> it in 2, 3 or more times [1, 2], represent one of the most important problem in the geophysical and historical bio-evolutional investigations of the past and present of the Earth. It was supposed that the re-connection of dipole magnetic field at magnetopause could play [2] an exclusive role in its inward shift, but from the more general point of view (to perform laboratory simulation [3-6] of magnetopause dynamics), a more important and common features of CME propagation in Solar Wind plasma are the formation of collisionless Quasi-Perpendicular <span class="hlt">Shocks</span> (Q-PS) ahead of Super-Alfvenic CME. It is provided by the almost radial (along to R) motion of CME from the Sun, while the Interplanetary Magnetic Field B0 has an angle θ ∼ 45° (relative to R) near the Earth orbit. Up to date, in spite of intensive development of laser energetics and energy of Laser-produced Plasma (LP), such Q-PS never were generated by LP [7], excluding recent experiment [8] at KI-1 facility of ILP. In the given work, a first results of our study were presented together with relevant calculations by hybrid code and the basic physics of VNIIEF-model [9] for the collisionless Magnetic Laminar Mechanism (MLM) of interaction between a spherical LP and magnetized Background Plasma (BP). A special analysis was done on the conditions and data of the formation of whistler precursor in front of revealed oblique (Q-PS) <span class="hlt">shocks</span> as well as on the first data of dipole's field <span class="hlt">compression</span> by BP and <span class="hlt">Shocks</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=314194','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=314194"><span>Chronic exposure to nitric oxide alters the free <span class="hlt">iron</span> pool in endothelial cells: Role of mitochondrial respiratory complexes and heat <span class="hlt">shock</span> proteins</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Ramachandran, Anup; Ceaser, Erin; Darley-Usmar, Victor M.</p> <p>2004-01-01</p> <p>The mechanisms of nitric oxide (NO) signaling include binding to the <span class="hlt">iron</span> centers in soluble guanylate cyclase and cytochrome c oxidase and posttranslational modification of proteins by S-nitrosation. Low levels of NO control mitochondrial number in cells, but little is known of the impact of chronic exposure to high levels of NO on mitochondrial function in endothelial cells. The focus of this study is the interaction of NO with mitochondrial respiratory complexes in cell culture and the effect this has on <span class="hlt">iron</span> homeostasis. We demonstrate that chronic exposure of endothelial cells to NO decreased activity and protein levels of complexes I, II, and IV, whereas citrate synthase and ATP synthase were unaffected. Inhibition of these respiratory complexes was accompanied by an increase in cellular S-nitrosothiol levels, modification of cysteines residues, and an increase in the labile <span class="hlt">iron</span> pool. The NO-dependent increase in the free <span class="hlt">iron</span> pool and inhibition of complex II was prevented by inhibition of mitochondrial protein synthesis, consistent with a major contribution of the organelle to <span class="hlt">iron</span> homeostasis. In addition, inhibition of mitochondrial protein synthesis was associated with an increase in heat <span class="hlt">shock</span> protein 60 levels, which may be an additional mechanism leading to preservation of complex II activity. PMID:14691259</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/1336361','SCIGOV-STC'); return false;" href="https://www.osti.gov/servlets/purl/1336361"><span>High precision Hugoniot measurements on statically pre-<span class="hlt">compressed</span> fluid helium</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Seagle, Christopher T.; Reinhart, William D.; Lopez, Andrew J.</p> <p></p> <p>Here we describe how the capability for statically pre-<span class="hlt">compressing</span> fluid targets for Hugoniot measurements utilizing gas gun driven flyer plates has been developed. Pre-<span class="hlt">compression</span> expands the capability for initial condition control, allowing access to thermodynamic states off the principal Hugoniot. Absolute Hugoniot measurements with an uncertainty less than 3% on density and pressure were obtained on statically pre-<span class="hlt">compressed</span> fluid helium utilizing a two stage light gas gun. Helium is highly <span class="hlt">compressible</span>; the locus of <span class="hlt">shock</span> states resulting from dynamic loading of an initially <span class="hlt">compressed</span> sample at room temperature is significantly denser than the cryogenic fluid Hugoniot even for relatively modestmore » (0.27–0.38 GPa) initial pressures. Lastly, the dynamic response of pre-<span class="hlt">compressed</span> helium in the initial density range of 0.21–0.25 g/cm3 at ambient temperature may be described by a linear <span class="hlt">shock</span> velocity (us) and particle velocity (u p) relationship: u s = C 0 + su p, with C 0 = 1.44 ± 0.14 km/s and s = 1.344 ± 0.025.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1336361-high-precision-hugoniot-measurements-statically-pre-compressed-fluid-helium','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1336361-high-precision-hugoniot-measurements-statically-pre-compressed-fluid-helium"><span>High precision Hugoniot measurements on statically pre-<span class="hlt">compressed</span> fluid helium</span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>Seagle, Christopher T.; Reinhart, William D.; Lopez, Andrew J.; ...</p> <p>2016-09-27</p> <p>Here we describe how the capability for statically pre-<span class="hlt">compressing</span> fluid targets for Hugoniot measurements utilizing gas gun driven flyer plates has been developed. Pre-<span class="hlt">compression</span> expands the capability for initial condition control, allowing access to thermodynamic states off the principal Hugoniot. Absolute Hugoniot measurements with an uncertainty less than 3% on density and pressure were obtained on statically pre-<span class="hlt">compressed</span> fluid helium utilizing a two stage light gas gun. Helium is highly <span class="hlt">compressible</span>; the locus of <span class="hlt">shock</span> states resulting from dynamic loading of an initially <span class="hlt">compressed</span> sample at room temperature is significantly denser than the cryogenic fluid Hugoniot even for relatively modestmore » (0.27–0.38 GPa) initial pressures. Lastly, the dynamic response of pre-<span class="hlt">compressed</span> helium in the initial density range of 0.21–0.25 g/cm3 at ambient temperature may be described by a linear <span class="hlt">shock</span> velocity (us) and particle velocity (u p) relationship: u s = C 0 + su p, with C 0 = 1.44 ± 0.14 km/s and s = 1.344 ± 0.025.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/1993ExFl...15..183L','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/1993ExFl...15..183L"><span>Head-on collision of normal <span class="hlt">shock</span> waves with rigid porous materials</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Levy, A.; Ben-Dor, G.; Skews, B. W.; Sorek, S.</p> <p>1993-08-01</p> <p>The head-on collision of a planar <span class="hlt">shock</span> wave with a rigid porous material has been investigated experimentally in a 75 mm × 75 mm <span class="hlt">shock</span> tube. The experimental study indicated that unlike the reflection from a flexible porous material (e.g., polyurethane foam) where the transmitted <span class="hlt">compression</span> waves do not converge to a sharp <span class="hlt">shock</span> wave, in the case of a rigid porous material (e.g., alumina) the transmitted <span class="hlt">compression</span> waves do converge to a sharp <span class="hlt">shock</span> wave, which decays as it propagates along the porous material. In addition to this major difference, many other differences were observed. They are outlined in the following sections. Based on these observations a suggestion modifying the phenomenology of the reflection/interaction process in the case a porous material with large permeability is proposed.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017ApPhL.111f1902B','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017ApPhL.111f1902B"><span><span class="hlt">Shock</span> initiation of explosives: High temperature hot spots explained</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Bassett, Will P.; Johnson, Belinda P.; Neelakantan, Nitin K.; Suslick, Kenneth S.; Dlott, Dana D.</p> <p>2017-08-01</p> <p>We investigated the <span class="hlt">shock</span> initiation of energetic materials with a tabletop apparatus that uses km s-1 laser-driven flyer plates to initiate tiny explosive charges and obtains complete temperature histories with a high dynamic range. By comparing various microstructured formulations, including a pentaerythritol tetranitrate (PETN) based plastic explosive (PBX) denoted XTX-8003, we determined that micron-scale pores were needed to create high hot spot temperatures. In charges where micropores (i.e., micron-sized pores) were present, a hot spot temperature of 6000 K was observed; when the micropores were pre-<span class="hlt">compressed</span> to nm scale, however, the hot spot temperature dropped to ˜4000 K. By comparing XTX-8003 with an analog that replaced PETN by nonvolatile silica, we showed that the high temperatures require gas in the pores, that the high temperatures were created by adiabatic gas <span class="hlt">compression</span>, and that the temperatures observed can be controlled by the choice of ambient gases. The hot spots persist in <span class="hlt">shock-compressed</span> PBXs even in vacuum because the initially empty pores became filled with gas created in-situ by <span class="hlt">shock</span>-induced chemical decomposition.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2013AGUFMMR11B..08F','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2013AGUFMMR11B..08F"><span>Thermal Equation of State of <span class="hlt">Iron</span>: Constraint on the Density Deficit of Earth's Core</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Fei, Y.; Murphy, C. A.; Shibazaki, Y.; Huang, H.</p> <p>2013-12-01</p> <p>The seismically inferred densities of Earth's solid inner core and the liquid outer core are smaller than the measured densities of solid hcp-<span class="hlt">iron</span> and liquid <span class="hlt">iron</span>, respectively. The inner core density deficit is significantly smaller than the outer core density deficit, implying different amounts and/or identities of light-elements incorporated in the inner and outer cores. Accurate measurements of the thermal equation-of-state of <span class="hlt">iron</span> over a wide pressure and temperature range are required to precisely quantify the core density deficits, which are essential for developing a quantitative composition model for the core. The challenge has been evaluating the experimental uncertainties related to the choice of pressure scales and the sample environment, such as hydrostaticity at multi-megabar pressures and extreme temperatures. We have conducted high-pressure experiments on <span class="hlt">iron</span> in MgO, NaCl, and Ne pressure media and obtained in-situ X-ray diffraction data up to 200 GPa at room temperature. Using inter-calibrated pressure scales including the MgO, NaCl, Ne, and Pt scales, we have produced a consistent <span class="hlt">compression</span> curve of hcp-Fe at room temperature. We have also performed laser-heated diamond-anvil cell experiments on both Fe and Pt in a Ne pressure medium. The experiment was designed to quantitatively compare the thermal expansion of Fe and Pt in the same sample environment using Ne as the pressure medium. The thermal expansion data of hcp-Fe at high pressure were derived based on the thermal equation of state of Pt. Using the 300-K isothermal <span class="hlt">compression</span> curve of <span class="hlt">iron</span> derived from our static experiments as a constraint, we have developed a thermal equation of state of hcp-Fe that is consistent with the static P-V-T data of <span class="hlt">iron</span> and also reproduces the <span class="hlt">shock</span> wave Hugoniot data for pure <span class="hlt">iron</span>. The thermodynamic model, based on both static and dynamic data, is further used to calculate the density and bulk sound velocity of liquid <span class="hlt">iron</span>. Our results define the solid</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_13");'>13</a></li> <li><a href="#" onclick='return showDiv("page_14");'>14</a></li> <li class="active"><span>15</span></li> <li><a href="#" onclick='return showDiv("page_16");'>16</a></li> <li><a href="#" onclick='return showDiv("page_17");'>17</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_15 --> <div id="page_16" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_14");'>14</a></li> <li><a href="#" onclick='return showDiv("page_15");'>15</a></li> <li class="active"><span>16</span></li> <li><a href="#" onclick='return showDiv("page_17");'>17</a></li> <li><a href="#" onclick='return showDiv("page_18");'>18</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="301"> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19930086812','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19930086812"><span>Elevated Temperature Properties of Titanium Carbide Base Ceramals Containing Nickel or <span class="hlt">Iron</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Cooper, A L; Colteryahn, L E</p> <p>1951-01-01</p> <p>Elevated-temperature properties of titanium carbide base ceramals containing nickel or <span class="hlt">iron</span> were determined in oxidation, modulus of rupture, tensile strength, and thermal-<span class="hlt">shock</span> resistance. These materials followed the general growth law and exhibited two stages in oxidation. The following tensile strengths were found at 2000 degrees F: 13.3 weight percent nickel, 16, 150 pounds per square inch; 11.8 weight percent <span class="hlt">iron</span>, 12,500 pounds per square inch; unalloyed titanium carbide, 16,450 pounds per square inch. Nickel or <span class="hlt">iron</span> additions to titanium carbide improved the thermal-<span class="hlt">shock</span> resistance, nickel more. The path of fracture in tensile and thermal-<span class="hlt">shock</span> specimens was found to progress approximately 50 percent intergranularly and 50 percent transgranularly.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2011APS..SHK.J4001F','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2011APS..SHK.J4001F"><span>Professor Thomas J. Ahrens and <span class="hlt">Shock</span> Wave Physics in Russia</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Fortov, Vladimir E.; Kanel, Gennady I.</p> <p>2011-06-01</p> <p>Since his earlier works on the equations of state and dynamic mechanical properties of rocks and other materials Prof. T.J. Ahrens furnished large influence on development of the <span class="hlt">shock</span> wave physics in Russia. He always demonstrates a choice of excellent problems and a level of productivity in the field of <span class="hlt">shock</span> <span class="hlt">compression</span> science which is unparalleled. In recognition of his great contribution into science and international scientific collaboration Prof. Ahrens has been elected in Russian Academy of Sciences as its foreign member. In the presentation, emphasis will be done on the Comet Shoemaker-Levy project in which we had fruitful informal collaboration, on the problem of wide-range equations of state, and on stress relaxation at <span class="hlt">shock</span> <span class="hlt">compression</span> of solids.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017AIPC.1793i0004D','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017AIPC.1793i0004D"><span>Shockwave <span class="hlt">compression</span> of Ar gas at several initial densities</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Dattelbaum, Dana M.; Goodwin, Peter M.; Garcia, Daniel B.; Gustavsen, Richard L.; Lang, John M.; Aslam, Tariq D.; Sheffield, Stephen A.; Gibson, Lloyd L.; Morris, John S.</p> <p>2017-01-01</p> <p>Experimental data of the principal Hugoniot locus of variable density gas-phase noble and molecular gases are rare. The majority of <span class="hlt">shock</span> Hugoniot data is either from <span class="hlt">shock</span> tube experiments on low-pressure gases or from plate impact experiments on cryogenic, liquefied gases. In both cases, physics regarding <span class="hlt">shock</span> <span class="hlt">compressibility</span>, thresholds for the on-set of <span class="hlt">shock</span>-driven ionization, and even dissociation chemistry are difficult to infer for gases at intermediate densities. We have developed an experimental target design for gas gun-driven plate impact experiments on noble gases at initial pressures between 200-1000 psi. Using optical velocimetry, we are able to directly determine both the <span class="hlt">shock</span> and particle velocities of the gas on the principal Hugoniot locus, as well as clearly differentiate ionization thresholds. The target design also results in multiply <span class="hlt">shocking</span> the gas in a quasi-isentropic fashion yielding off-Hugoniot <span class="hlt">compression</span> data. We describe the results of a series of plate impact experiments on Ar with starting densities between 0.02-0.05 g/cm3 at room temperature. Furthermore, by coupling optical fibers to the targets, we have measured the time-resolved optical emission from the <span class="hlt">shocked</span> gas using a spectrometer coupled to an optical streak camera to spectrally-resolve the emission, and with a 5-color optical pyrometer for temperature determination.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1254684-practicality-magnetic-compression-plasma-density-control','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1254684-practicality-magnetic-compression-plasma-density-control"><span>Practicality of magnetic <span class="hlt">compression</span> for plasma density control</span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>Gueroult, Renaud; Fisch, Nathaniel J.</p> <p>2016-03-16</p> <p>Here, plasma densification through magnetic <span class="hlt">compression</span> has been suggested for time-resolved control of the wave properties in plasma-based accelerators [P. F. Schmit and N. J. Fisch, Phys. Rev. Lett. 109, 255003 (2012)]. Using particle in cell simulations with real mass ratio, the practicality of large magnetic <span class="hlt">compression</span> on timescales shorter than the ion gyro-period is investigated. For <span class="hlt">compression</span> times shorter than the transit time of a compressional Alfven wave across the plasma slab, results show the formation of two counter-propagating <span class="hlt">shock</span> waves, leading to a highly non-uniform plasma density profile. Furthermore, the plasma slab displays large hydromagnetic like oscillations aftermore » the driving field has reached steady state. Peak <span class="hlt">compression</span> is obtained when the two <span class="hlt">shocks</span> collide in the mid-plane. At this instant, very large plasma heating is observed, and the plasmaβ is estimated to be about 1. Although these results point out a densification mechanism quite different and more complex than initially envisioned, these features still might be advantageous in particle accelerators.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017AGUFMDI23B..04D','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017AGUFMDI23B..04D"><span>Forsterite <span class="hlt">Shock</span> Temperatures and Entropy: New Scaling Laws for Impact Melting and Vaporization</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Davies, E.; Root, S.; Kraus, R. G.; Townsend, J. P.; Spaulding, D.; Stewart, S. T.; Jacobsen, S. B.; Fratanduono, D.; Millot, M. A.; Mattsson, T. R.; Hanshaw, H. L.</p> <p>2017-12-01</p> <p>The observed masses, radii and temperatures of thousands of extra-solar planets have challenged our theoretical understanding of planet formation and planetary structures. Planetary materials are subject to extreme pressures and temperatures during formation and within the present-day interiors of large bodies. Here, we focus on improving understanding of the physical properties of rocky planets for calculations of internal structure and the outcomes of giant impacts. We performed flyer plate impact experiments on forsterite [Mg2SiO4] on the Z-Machine at Sandia National Laboratory and decaying <span class="hlt">shock</span> temperature measurements at the Omega EP laser at U. Rochester. At Z, planar, supported <span class="hlt">shock</span> waves are generated in single crystal samples, permitting observation of both <span class="hlt">compressed</span> and released states. Using available static and dynamic thermodynamic data, we calculate absolute entropy and heat capacity along the forsterite <span class="hlt">shock</span> Hugoniot. Entropy and heat capacity on the Hugoniot are larger than previous estimates. Our data constrain the thermodynamic properties of forsterite liquid at high pressures and temperatures and the amount of melt and vapor produced during impact events. For an ambient pressure of 1 bar, <span class="hlt">shock</span>-vaporization begins upon reaching the liquid region on the forsterite Hugoniot (about 200 GPa). Using hydrocode simulations of giant impacts between rocky planets with forsterite mantles and <span class="hlt">iron</span> cores and the new experimentally-constrained forsterite <span class="hlt">shock</span> entropy, we present a new scaling law for the fraction of mantle that is melted or vaporized by the initial <span class="hlt">shock</span> wave. Sandia National Laboratories is a multimission laboratory managed and operated by National Technology and Engineering Solutions of Sandia, LLC., a wholly owned subsidiary of Honeywell International, Inc., for the U.S. Department of Energy's National Nuclear Security Administration under contract DE-NA0003525. Prepared by LLNL under Contract DE-AC52-07NA27344. Prepared by the Center</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015APS..SHK.K5003Z','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015APS..SHK.K5003Z"><span><span class="hlt">Shock</span> response of nanoporous Cu--A molecular dynamics simulation</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Zhao, Fengpeng</p> <p>2015-06-01</p> <p><span class="hlt">Shock</span> response of porous materials can be of crucial significance for <span class="hlt">shock</span> physics and bears many practical applications in materials synthesis and engineering. Molecular dynamics simulations are carried out to investigate <span class="hlt">shock</span> response of nanoporous metal materials, including elastic-plastic deformation, Hugoniot states, <span class="hlt">shock</span>-induced melting, partial or complete void collapse, hotspot formation, nanojetting, and vaporization. A model nanoporous Cu with cylindrical voids and a high porosity under <span class="hlt">shocking</span> is established to investigate such physical properties as velocity, temperature, density, stress and von Mises stress at different stages of <span class="hlt">compression</span> and release. The elastic-plastic and overtaking <span class="hlt">shocks</span> are observed at different <span class="hlt">shock</span> strengths. A modified power-law P- α model is proposed to describe the Hugoniot states. The Grüneisen equation of state is validated. <span class="hlt">Shock</span>-induced melting shows no clear signs of bulk premelting or superheating. Void collapse via plastic flow nucleated from voids, and the exact processes are <span class="hlt">shock</span> strength dependent. With increasing <span class="hlt">shock</span> strengths, void collapse transits from the ``geometrical'' mode (collapse of a void is dominated by crystallography and void geometry and can be different from that of one another) to ``hydrodynamic'' mode (collapse of a void is similar to one another). The collapse may be achieved predominantly by plastic flows along the {111} slip planes, by way of alternating <span class="hlt">compression</span> and tension zones, by means of transverse flows, via forward and transverse flows, or through forward nano-jetting. The internal jetting induces pronounced <span class="hlt">shock</span> front roughening, leading to internal hotspot formation and sizable high speed jets on atomically flat free surfaces. P. O. Box 919-401, Mianyang, 621900, Sichuan, PRC.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2013APS..SHK.E3003C','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2013APS..SHK.E3003C"><span><span class="hlt">Shock</span> wave viscosity measurements</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Celliers, Peter</p> <p>2013-06-01</p> <p>Several decades ago a method was proposed and demonstrated to measure the viscosity of fluids at high pressure by observing the oscillatory damping of sinusoidal perturbations on a <span class="hlt">shock</span> front. A detailed mathematical analysis of the technique carried out subsequently by Miller and Ahrens revealed its potential, as well as a deep level of complexity in the analysis. We revisit the ideas behind this technique in the context of a recent experimental development: two-dimensional imaging velocimetry. The new technique allows one to capture a broad spectrum of perturbations down to few micron scale-lengths imposed on a <span class="hlt">shock</span> front from an initial perturbation. The detailed evolution of the perturbation spectrum is sensitive to the viscosity in the fluid behind the <span class="hlt">shock</span> front. Initial experiments are aimed at examining the viscosity of <span class="hlt">shock</span> <span class="hlt">compressed</span> SiO2 just above the <span class="hlt">shock</span> melting transition. This work performed under the auspices of the U.S. Department of Energy by Lawrence Livermore National Laboratory under Contract DE-AC52-07NA27344.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20140006630','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20140006630"><span>Whistler Waves Associated with Weak Interplanetary <span class="hlt">Shocks</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Velez, J. C. Ramirez; Blanco-Cano, X.; Aguilar-Rodriguez, E.; Russell, C. T.; Kajdic, P.; Jian,, L. K.; Luhmann, J. G.</p> <p>2012-01-01</p> <p>We analyze the properties of 98 weak interplanetary <span class="hlt">shocks</span> measured by the dual STEREO spacecraft over approximately 3 years during the past solar minimum. We study the occurrence of whistler waves associated with these <span class="hlt">shocks</span>, which on average are high beta <span class="hlt">shocks</span> (0.2 < Beta < 10). We have compared the waves properties upstream and downstream of the <span class="hlt">shocks</span>. In the upstream region the waves are mainly circularly polarized, and in most of the cases (approx. 75%) they propagate almost parallel to the ambient magnetic field (<30 deg.). In contrast, the propagation angle with respect to the <span class="hlt">shock</span> normal varies in a broad range of values (20 deg. to 90 deg.), suggesting that they are not phase standing. We find that the whistler waves can extend up to 100,000 km in the upstream region but in most cases (88%) are contained in a distance within 30,000 km from the <span class="hlt">shock</span>. This corresponds to a larger region with upstream whistlers associated with IP <span class="hlt">shocks</span> than previously reported in the literature. The maximum amplitudes of the waves are observed next to the <span class="hlt">shock</span> interface, and they decrease as the distance to the <span class="hlt">shock</span> increases. In most cases the wave propagation direction becomes more aligned with the magnetic field as the distance to the <span class="hlt">shock</span> increases. These two facts suggest that most of the waves in the upstream region are Landau damping as they move away from the <span class="hlt">shock</span>. From the analysis we also conclude that it is likely that the generation mechanism of the upstream whistler waves is taking place at the <span class="hlt">shock</span> interface. In the downstream region, the waves are irregularly polarized, and the fluctuations are very <span class="hlt">compressive</span>; that is, the <span class="hlt">compressive</span> component of the wave clearly dominates over the transverse one. The majority of waves in the downstream region (95%) propagate at oblique angles with respect to the ambient magnetic field (>60 deg.). The wave propagation with respect to the <span class="hlt">shock</span>-normal direction has no preferred direction and varies similarly to</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2014JPhCS.500c2001A','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2014JPhCS.500c2001A"><span>An equation of state for polyurea aerogel based on multi-<span class="hlt">shock</span> response</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Aslam, T. D.; Gustavsen, R. L.; Bartram, B. D.</p> <p>2014-05-01</p> <p>The equation of state (EOS) of polyurea aerogel (PUA) is examined through both single <span class="hlt">shock</span> Hugoniot data as well as more recent multi-<span class="hlt">shock</span> <span class="hlt">compression</span> experiments performed on the LANL 2-stage gas gun. A simple conservative Lagrangian numerical scheme, utilizing total variation diminishing (TVD) interpolation and an approximate Riemann solver, will be presented as well as the methodology of calibration. It will been demonstrated that a p-a model based on a Mie-Gruneisen fitting form for the solid material can reasonably replicate multi-<span class="hlt">shock</span> <span class="hlt">compression</span> response at a variety of initial densities; such a methodology will be presented for a commercially available polyurea aerogel.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018PhFl...30d1703H','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018PhFl...30d1703H"><span>Letter: Transient interaction between plasma jet and supersonic <span class="hlt">compression</span> ramp flow</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Huang, He-Xia; Tan, Hui-Jun; Sun, Shu; Zhang, Yu-Chao; Cheng, Lin</p> <p>2018-04-01</p> <p>The rapid flow evolution between a plasma jet and a 20° <span class="hlt">compression</span> ramp flow is captured by a high-speed schlieren system at Mach 2.0. Several interesting flow phenomena are observed for the first time. The pulsed jet, which generates strong perturbations, forces the crossflow boundary layer to separate and forms a forward moving <span class="hlt">shock</span>. A typical <span class="hlt">shock-on-shock</span> interaction occurs when the precursor <span class="hlt">shock</span> intersects with the original <span class="hlt">shock</span>. The interaction is initially regular, and then it transforms into an irregular one with a Mach stem connecting the precursor <span class="hlt">shock</span> and original ramp <span class="hlt">shock</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2013APS..SHK.O2005A','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2013APS..SHK.O2005A"><span>An Equation of State for Foamed Divinylbenzene (DVB) Based on Multi-<span class="hlt">Shock</span> Response</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Aslam, Tariq; Schroen, Diana; Gustavsen, Richard; Bartram, Brian</p> <p>2013-06-01</p> <p>The methodology for making foamed Divinylbenzene (DVB) is described. For a variety of initial densities, foamed DVB is examined through multi-<span class="hlt">shock</span> <span class="hlt">compression</span> and release experiments. Results from multi-<span class="hlt">shock</span> experiments on LANL's 2-stage gas gun will be presented. A simple conservative Lagrangian numerical scheme, utilizing total-variation-diminishing interpolation and an approximate Riemann solver, will be presented as well as the methodology of calibration. It has been previously demonstrated that a single Mie-Gruneisen fitting form can replicate foam multi-<span class="hlt">shock</span> <span class="hlt">compression</span> response at a variety of initial densities; such a methodology will be presented for foamed DVB.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19950011695','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19950011695"><span>Floating <span class="hlt">shock</span> fitting via Lagrangian adaptive meshes</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Vanrosendale, John</p> <p>1994-01-01</p> <p>In recent works we have formulated a new approach to <span class="hlt">compressible</span> flow simulation, combining the advantages of <span class="hlt">shock</span>-fitting and <span class="hlt">shock</span>-capturing. Using a cell-centered Roe scheme discretization on unstructured meshes, we warp the mesh while marching to steady state, so that mesh edges align with <span class="hlt">shocks</span> and other discontinuities. This new algorithm, the <span class="hlt">Shock</span>-fitting Lagrangian Adaptive Method (SLAM) is, in effect, a reliable <span class="hlt">shock</span>-capturing algorithm which yields <span class="hlt">shock</span>-fitted accuracy at convergence. <span class="hlt">Shock</span>-capturing algorithms like this, which warp the mesh to yield <span class="hlt">shock</span>-fitted accuracy, are new and relatively untried. However, their potential is clear. In the context of sonic booms, accurate calculation of near-field sonic boom signatures is critical to the design of the High Speed Civil Transport (HSCT). SLAM should allow computation of accurate N-wave pressure signatures on comparatively coarse meshes, significantly enhancing our ability to design low-boom configurations for high-speed aircraft.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017PhRvM...1d3606E','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017PhRvM...1d3606E"><span><span class="hlt">Shock</span>-wave propagation and reflection in semicrystalline polyethylene: A molecular-level investigation</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Elder, Robert M.; O'Connor, Thomas C.; Chantawansri, Tanya L.; Sliozberg, Yelena R.; Sirk, Timothy W.; Yeh, In-Chul; Robbins, Mark O.; Andzelm, Jan W.</p> <p>2017-09-01</p> <p>Semicrystalline polyethylene (PE) is attractive for a variety of mechanically demanding applications, where <span class="hlt">shock</span> <span class="hlt">compression</span> can occur. Although often highly crystalline, PE invariably contains nanoscale amorphous domains that influence <span class="hlt">shock</span> propagation. Our objective in this work is to study the effects of such domains. To this end, we adopt a novel approach wherein we parametrize a simple continuum-level theory based on the <span class="hlt">shock</span> impedance from molecular dynamics (MD) simulations. Using this theory, we predict how crystalline/amorphous interfaces attenuate <span class="hlt">shocks</span> via energy reflection due to the impedance mismatch between the phases. The theory predicts that these interfaces attenuate weak <span class="hlt">shocks</span> more effectively than strong <span class="hlt">shocks</span>. We compare the theory to explicit nonequilibrium MD simulations of <span class="hlt">compressive</span> <span class="hlt">shocks</span> in semicrystalline PE containing nanometer-scale amorphous regions of varying size, where we analyze the pressure response and reflection of energy. The theory and simulations show good agreement for strong <span class="hlt">shocks</span> (≥1.0 km /s ), but for weak <span class="hlt">shocks</span> (<1.0 km /s ) the simulations show enhanced energy reflection relative to the continuum predictions. Furthermore, the simulations show an effect not captured by the continuum theory: the size of amorphous regions is important. The theory assumes a sharp (discontinuous) interface between two bulk phases and a sharp change in thermodynamic and hydrodynamic quantities at the <span class="hlt">shock</span> front. However, the simulations show that when amorphous domains are narrow—with widths comparable to the <span class="hlt">shock</span> front—reflection is reduced compared to the predictions. We identify several nanoscale mechanisms that reduce the impedance mismatch, and thus reduce reflection, at thin amorphous domains. First, the two-wave elastic-plastic structure of <span class="hlt">shocks</span> in crystalline PE allows the faster-moving elastic precursor wave to <span class="hlt">compress</span> small amorphous domains before the plastic wave arrives. Second, confinement between stiff</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/1345616','SCIGOV-STC'); return false;" href="https://www.osti.gov/servlets/purl/1345616"><span>Pre-strain effect on frequency-based impact energy dissipation through a silicone foam pad for <span class="hlt">shock</span> mitigation [Pre-strain effect on the frequency response of <span class="hlt">shock</span> mitigation through a silicone foam pad</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Sanborn, Brett; Song, Bo; Smith, Scott</p> <p></p> <p>Silicone foams have been used in a variety of applications from gaskets to cushioning pads over a wide range of environments. Particularly, silicone foams are used as a <span class="hlt">shock</span> mitigation material for <span class="hlt">shock</span> and vibration applications. Understanding the <span class="hlt">shock</span> mitigation response, particularly in the frequency domain, is critical for optimal designs to protect internal devices and components more effectively and efficiently. The silicone foams may be subjected to pre-strains during the assembly process which may consequently influence the frequency response with respect to <span class="hlt">shock</span> mitigation performance. A Kolsky <span class="hlt">compression</span> bar was modified with pre-<span class="hlt">compression</span> capabilities to characterize the <span class="hlt">shock</span> mitigationmore » response of silicone foam in the frequency domain to determine the effect of pre-strain. Lastly, a silicone sample was also intentionally subjected to repeated pre-strain and dynamic loadings to explore the effect of repeated loading on the frequency response of <span class="hlt">shock</span> mitigation.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1345616-pre-strain-effect-frequency-based-impact-energy-dissipation-through-silicone-foam-pad-shock-mitigation-pre-strain-effect-frequency-response-shock-mitigation-through-silicone-foam-pad','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1345616-pre-strain-effect-frequency-based-impact-energy-dissipation-through-silicone-foam-pad-shock-mitigation-pre-strain-effect-frequency-response-shock-mitigation-through-silicone-foam-pad"><span>Pre-strain effect on frequency-based impact energy dissipation through a silicone foam pad for <span class="hlt">shock</span> mitigation [Pre-strain effect on the frequency response of <span class="hlt">shock</span> mitigation through a silicone foam pad</span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>Sanborn, Brett; Song, Bo; Smith, Scott</p> <p>2015-12-29</p> <p>Silicone foams have been used in a variety of applications from gaskets to cushioning pads over a wide range of environments. Particularly, silicone foams are used as a <span class="hlt">shock</span> mitigation material for <span class="hlt">shock</span> and vibration applications. Understanding the <span class="hlt">shock</span> mitigation response, particularly in the frequency domain, is critical for optimal designs to protect internal devices and components more effectively and efficiently. The silicone foams may be subjected to pre-strains during the assembly process which may consequently influence the frequency response with respect to <span class="hlt">shock</span> mitigation performance. A Kolsky <span class="hlt">compression</span> bar was modified with pre-<span class="hlt">compression</span> capabilities to characterize the <span class="hlt">shock</span> mitigationmore » response of silicone foam in the frequency domain to determine the effect of pre-strain. Lastly, a silicone sample was also intentionally subjected to repeated pre-strain and dynamic loadings to explore the effect of repeated loading on the frequency response of <span class="hlt">shock</span> mitigation.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/23126906','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/23126906"><span>A novel particle time of flight diagnostic for measurements of <span class="hlt">shock</span>- and <span class="hlt">compression</span>-bang times in D3He and DT implosions at the NIF.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Rinderknecht, H G; Johnson, M Gatu; Zylstra, A B; Sinenian, N; Rosenberg, M J; Frenje, J A; Waugh, C J; Li, C K; Sèguin, F H; Petrasso, R D; Rygg, J R; Kimbrough, J R; MacPhee, A; Collins, G W; Hicks, D; Mackinnon, A; Bell, P; Bionta, R; Clancy, T; Zacharias, R; Döppner, T; Park, H S; LePape, S; Landen, O; Meezan, N; Moses, E I; Glebov, V U; Stoeckl, C; Sangster, T C; Olson, R; Kline, J; Kilkenny, J</p> <p>2012-10-01</p> <p>The particle-time-of-flight (pTOF) diagnostic, fielded alongside a wedge range-filter (WRF) proton spectrometer, will provide an absolute timing for the <span class="hlt">shock</span>-burn weighted ρR measurements that will validate the modeling of implosion dynamics at the National Ignition Facility (NIF). In the first phase of the project, pTOF has recorded accurate bang times in cryogenic DT, DT exploding pusher, and D(3)He implosions using DD or DT neutrons with an accuracy better than ±70 ps. In the second phase of the project, a deflecting magnet will be incorporated into the pTOF design for simultaneous measurements of <span class="hlt">shock</span>- and <span class="hlt">compression</span>-bang times in D(3)He-filled surrogate implosions using D(3)He protons and DD-neutrons, respectively.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19980201093','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19980201093"><span>Performance of Low Dissipative High Order <span class="hlt">Shock</span>-Capturing Schemes for <span class="hlt">Shock</span>-Turbulence Interactions</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Sandham, N. D.; Yee, H. C.</p> <p>1998-01-01</p> <p>Accurate and efficient direct numerical simulation of turbulence in the presence of <span class="hlt">shock</span> waves represents a significant challenge for numerical methods. The objective of this paper is to evaluate the performance of high order compact and non-compact central spatial differencing employing total variation diminishing (TVD) <span class="hlt">shock</span>-capturing dissipations as characteristic based filters for two model problems combining <span class="hlt">shock</span> wave and shear layer phenomena. A vortex pairing model evaluates the ability of the schemes to cope with shear layer instability and eddy <span class="hlt">shock</span> waves, while a <span class="hlt">shock</span> wave impingement on a spatially-evolving mixing layer model studies the accuracy of computation of vortices passing through a sequence of <span class="hlt">shock</span> and expansion waves. A drastic increase in accuracy is observed if a suitable artificial <span class="hlt">compression</span> formulation is applied to the TVD dissipations. With this modification to the filter step the fourth-order non-compact scheme shows improved results in comparison to second-order methods, while retaining the good <span class="hlt">shock</span> resolution of the basic TVD scheme. For this characteristic based filter approach, however, the benefits of compact schemes or schemes with higher than fourth order are not sufficient to justify the higher complexity near the boundary and/or the additional computational cost.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19730012553','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19730012553"><span>The behavior of a <span class="hlt">compressible</span> turbulent boundary layer in a <span class="hlt">shock</span>-wave-induced adverse pressure gradient. Ph.D. Thesis - Washington Univ., Seattle, Aug. 1972</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Rose, W. C.</p> <p>1973-01-01</p> <p>The results of an experimental investigation of the mean- and fluctuating-flow properties of a <span class="hlt">compressible</span> turbulent boundary layer in a <span class="hlt">shock</span>-wave-induced adverse pressure gradient are presented. The turbulent boundary layer developed on the wall of an axially symmetric nozzle and test section whose nominal free-stream Mach number and boundary-layer thickness Reynolds number were 4 and 100,000, respectively. The adverse pressure gradient was induced by an externally generated conical <span class="hlt">shock</span> wave. Mean and time-averaged fluctuating-flow data, including the complete experimental Reynolds stress tensor and experimental turbulent mass- and heat-transfer rates are presented for the boundary layer and external flow, upstream, within and downstream of the pressure gradient. The mean-flow data include distributions of total temperature throughout the region of interest. The turbulent mixing properties of the flow were determined experimentally with a hot-wire anemometer. The calibration of the wires and the interpretation of the data are discussed. From the results of the investigation, it is concluded that the <span class="hlt">shock</span>-wave - boundary-layer interaction significantly alters the turbulent mixing characteristics of the boundary layer.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19740040232&hterms=shock+elastic&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D30%26Ntt%3Dshock%2Belastic','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19740040232&hterms=shock+elastic&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D30%26Ntt%3Dshock%2Belastic"><span><span class="hlt">Shock</span> <span class="hlt">compression</span> of a recrystallized anorthositic rock from Apollo 15</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Ahrens, T. J.; Gibbons, R. V.; O'Keefe, J. D.</p> <p>1973-01-01</p> <p>Hugoniot measurements on 15,418, a recrystallized and brecciated gabbroic anorthosite, yield a value of the Hugoniot elastic limit (HEL) varying from 45 to 70 kbar as the final <span class="hlt">shock</span> pressure is varied from 70 to 280 kbar. Above the HEL and to 150 kbar, the pressure-density Hugoniot is closely described by a hydrostatic equation of state constructed from ultrasonic data for single-crystal plagioclase and pyroxene. Above 150 kbar, the Hugoniot states indicate that a series of one or more <span class="hlt">shock</span>-induced phase changes are occurring in the plagioclase and pyroxene. From Hugoniot data for both the single-crystal minerals and the Frederick diabase, we infer that the <span class="hlt">shock</span>-induced high-pressure phases in 15,418 probably consists of a 3.71 g/cu cm density, high-pressure structure for plagioclase and a 4.70 g/cu cm perovskite-type structure for pyroxene.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2001APS..MARS15004G','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2001APS..MARS15004G"><span>First-principles simulations of <span class="hlt">shock</span> front propagation in liquid deuterium</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Gygi, Francois; Galli, Giulia</p> <p>2001-03-01</p> <p>We present large-scale first-principles molecular dynamics simulations of the formation and propagation of a <span class="hlt">shock</span> front in liquid deuterium. Molecular deuterium was subjected to supersonic impacts at velocities ranging from 10 to 30 km/s. We used Density Functional Theory in the local density approximation, and simulation cells containing 1320 deuterium atoms. The formation of a <span class="hlt">shock</span> front was observed and its velocity was measured and compared with the results of laser-driven <span class="hlt">shock</span> experiments [1]. The pressure and density in the <span class="hlt">compressed</span> fluid were also computed directly from statistical averages in appropriate regions of the simulation cell, and compared with previous first-principles calculations performed at equilibrium [2]. Details of the electronic structure at the <span class="hlt">shock</span> front, and their influence on the properties of the <span class="hlt">compressed</span> fluid will be discussed. [1] J.W.Collins et al. Science 281, 1178 (1998). [2] G.Galli, R.Q.Hood, A.U.Hazi and F.Gygi, Phys.Rev. B61, 909 (2000).</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_14");'>14</a></li> <li><a href="#" onclick='return showDiv("page_15");'>15</a></li> <li class="active"><span>16</span></li> <li><a href="#" onclick='return showDiv("page_17");'>17</a></li> <li><a href="#" onclick='return showDiv("page_18");'>18</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_16 --> <div id="page_17" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_15");'>15</a></li> <li><a href="#" onclick='return showDiv("page_16");'>16</a></li> <li class="active"><span>17</span></li> <li><a href="#" onclick='return showDiv("page_18");'>18</a></li> <li><a href="#" onclick='return showDiv("page_19");'>19</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="321"> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017JMEP...26..177D','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017JMEP...26..177D"><span>Influence of High-Current-Density Impulses on the <span class="hlt">Compression</span> Behavior: Experiments with <span class="hlt">Iron</span> and a Nickel-Based Alloy</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Demler, E.; Gerstein, G.; Dalinger, A.; Epishin, A.; Rodman, D.; Nürnberger, F.</p> <p>2017-01-01</p> <p>Difficulties of processing of high strength and/or brittle materials by plastic deformation, e.g., by forging, require to develop new industrial technologies. In particular, the feasible deformation rates are limited for low-ductile metallic materials. For this reason, processes were investigated to improve the deformability in which electrical impulses are to be applied to lower the yield strength. However, owing to the impulse duration and low current densities, concomitant effects always occur, e.g., as a result of Joule heating. Current developments in power electronics allow now to transmit high currents as short pulses. By reducing the impulse duration and increasing the current density, the plasticity of metallic materials can be correspondingly increased. Using the examples of polycrystalline <span class="hlt">iron</span> and a single-crystal, nickel-based alloy (PWA 1480), current advances in the development of methods for forming materials by means of high-current-density impulses are demonstrated. For this purpose, appropriate specimens were loaded in <span class="hlt">compression</span> and, using novel testing equipment, subjected to a current strength of 10 kA with an impulse duration of 2 ms. For a pre-defined strain, the test results show a significant decrease in the <span class="hlt">compressive</span> stress during the <span class="hlt">compression</span> test and a significant change in the dislocation distribution following the current impulse treatment.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2011M%26PS...46.1227Y','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2011M%26PS...46.1227Y"><span>Thermal and impact histories of reheated group IVA, IVB, and ungrouped <span class="hlt">iron</span> meteorites and their parent asteroids</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Yang, J.; Goldstein, J. I.; Scott, E. R. D.; Michael, J. R.; Kotula, P. G.; Pham, T.; McCoy, T. J.</p> <p>2011-09-01</p> <p>Abstract- The microstructures of six reheated <span class="hlt">iron</span> meteorites—two IVA <span class="hlt">irons</span>, Maria Elena (1935), Fuzzy Creek; one IVB <span class="hlt">iron</span>, Ternera; and three ungrouped <span class="hlt">irons</span>, Hammond, Babb’s Mill (Blake’s <span class="hlt">Iron</span>), and Babb’s Mill (Troost’s <span class="hlt">Iron</span>)—were characterized using scanning and transmission electron microscopy, electron-probe microanalysis, and electron backscatter diffraction techniques to determine their thermal and <span class="hlt">shock</span> history and that of their parent asteroids. Maria Elena and Hammond were heated below approximately 700-750 °C, so that kamacite was recrystallized and taenite was exsolved in kamacite and was spheroidized in plessite. Both meteorites retained a record of the original Widmanstätten pattern. The other four, which show no trace of their original microstructure, were heated above 600-700 °C and recrystallized to form 10-20 μm wide homogeneous taenite grains. On cooling, kamacite formed on taenite grain boundaries with their close-packed planes aligned. Formation of homogeneous 20 μm wide taenite grains with diverse orientations would have required as long as approximately 800 yr at 600 °C or approximately 1 h at 1300 °C. All six <span class="hlt">irons</span> contain approximately 5-10 μm wide taenite grains with internal microprecipitates of kamacite and nanometer-scale M-shaped Ni profiles that reach approximately 40% Ni indicating cooling over 100-10,000 yr. Un-decomposed high-Ni martensite (α2) in taenite—the first occurrence in irons—appears to be a characteristic of strongly reheated <span class="hlt">irons</span>. From our studies and published work, we identified four progressive stages of <span class="hlt">shock</span> and reheating in IVA <span class="hlt">irons</span> using these criteria: cloudy taenite, M-shaped Ni profiles in taenite, Neumann twin lamellae, martensite, <span class="hlt">shock</span>-hatched kamacite, recrystallization, microprecipitates of taenite, and <span class="hlt">shock</span>-melted troilite. Maria Elena and Fuzzy Creek represent stages 3 and 4, respectively. Although not all reheated <span class="hlt">irons</span> contain evidence for <span class="hlt">shock</span>, it was probably the main</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/1985ICRC....3..118B','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/1985ICRC....3..118B"><span>Selfsimilar time dependent <span class="hlt">shock</span> structures</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Beck, R.; Drury, L. O.</p> <p>1985-08-01</p> <p>Diffusive <span class="hlt">shock</span> acceleration as an astrophysical mechanism for accelerating charged particles has the advantage of being highly efficient. This means however that the theory is of necessity nonlinear; the reaction of the accelerated particles on the <span class="hlt">shock</span> structure and the acceleration process must be self-consistently included in any attempt to develop a complete theory of diffusive <span class="hlt">shock</span> acceleration. Considerable effort has been invested in attempting, at least partially, to do this and it has become clear that in general either the maximum particle energy must be restricted by introducing additional loss processes into the problem or the acceleration must be treated as a time dependent problem (Drury, 1984). It is concluded that stationary modified <span class="hlt">shock</span> structures can only exist for strong <span class="hlt">shocks</span> if additional loss processes limit the maximum energy a particle can attain. This is certainly possible and if it occurs the energy loss from the <span class="hlt">shock</span> will lead to much greater <span class="hlt">shock</span> <span class="hlt">compressions</span>. It is however equally possible that no such processes exist and we must then ask what sort of nonstationary <span class="hlt">shock</span> structure develops. The ame argument which excludes stationary structures also rules out periodic solutions and indeed any solution where the width of the <span class="hlt">shock</span> remains bounded. It follows that the width of the <span class="hlt">shock</span> must increase secularly with time and it is natural to examine the possibility of selfsimilar time dependent solutions.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19850026581','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19850026581"><span>Selfsimilar time dependent <span class="hlt">shock</span> structures</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Beck, R.; Drury, L. O.</p> <p>1985-01-01</p> <p>Diffusive <span class="hlt">shock</span> acceleration as an astrophysical mechanism for accelerating charged particles has the advantage of being highly efficient. This means however that the theory is of necessity nonlinear; the reaction of the accelerated particles on the <span class="hlt">shock</span> structure and the acceleration process must be self-consistently included in any attempt to develop a complete theory of diffusive <span class="hlt">shock</span> acceleration. Considerable effort has been invested in attempting, at least partially, to do this and it has become clear that in general either the maximum particle energy must be restricted by introducing additional loss processes into the problem or the acceleration must be treated as a time dependent problem (Drury, 1984). It is concluded that stationary modified <span class="hlt">shock</span> structures can only exist for strong <span class="hlt">shocks</span> if additional loss processes limit the maximum energy a particle can attain. This is certainly possible and if it occurs the energy loss from the <span class="hlt">shock</span> will lead to much greater <span class="hlt">shock</span> <span class="hlt">compressions</span>. It is however equally possible that no such processes exist and we must then ask what sort of nonstationary <span class="hlt">shock</span> structure develops. The ame argument which excludes stationary structures also rules out periodic solutions and indeed any solution where the width of the <span class="hlt">shock</span> remains bounded. It follows that the width of the <span class="hlt">shock</span> must increase secularly with time and it is natural to examine the possibility of selfsimilar time dependent solutions.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3768293','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3768293"><span>Safety and Efficacy of Defibrillator Charging During Ongoing Chest <span class="hlt">Compressions</span>: A Multicenter Study</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Edelson, Dana P.; Robertson-Dick, Brian J.; Yuen, Trevor C.; Eilevstjønn, Joar; Walsh, Deborah; Bareis, Charles J.; Vanden Hoek, Terry L.; Abella, Benjamin S.</p> <p>2013-01-01</p> <p>BACKGROUND Pauses in chest <span class="hlt">compressions</span> during cardiopulmonary resuscitation have been shown to correlate with poor outcomes. In an attempt to minimize these pauses, the American Heart Association recommends charging the defibrillator during chest <span class="hlt">compressions</span>. While simulation work suggests decreased pause times using this technique, little is known about its use in clinical practice. METHODS We conducted a multicenter, retrospective study of defibrillator charging at three US academic teaching hospitals between April 2006 and April 2009. Data were abstracted from CPR-sensing defibrillator transcripts. Pre-<span class="hlt">shock</span> pauses and total hands- off time preceding the defibrillation attempts were compared among techniques. RESULTS A total of 680 charge-cycles from 244 cardiac arrests were analyzed. The defibrillator was charged during ongoing chest <span class="hlt">compressions</span> in 448 (65.9%) instances with wide variability across the three sites. Charging during <span class="hlt">compressions</span> correlated with a decrease in median pre-<span class="hlt">shock</span> pause [2.6 (IQR 1.9–3.8) vs 13.3 (IQR 8.6–19.5) s; p < 0.001] and total hands-off time in the 30 s preceding defibrillation [10.3 (IQR 6.4–13.8) vs 14.8 (IQR 11.0–19.6) s; p < 0.001]. The improvement in hands-off time was most pronounced when rescuers charged the defibrillator in anticipation of the pause, prior to any rhythm analysis. There was no difference in inappropriate <span class="hlt">shocks</span> when charging during chest <span class="hlt">compressions</span> (20.0 vs 20.1%; p=0.97) and there was only one instance noted of inadvertent <span class="hlt">shock</span> administration during <span class="hlt">compressions</span>, which went unnoticed by the compressor. CONCLUSIONS Charging during <span class="hlt">compressions</span> is underutilized in clinical practice. The technique is associated with decreased hands-off time preceding defibrillation, with minimal risk to patients or rescuers. PMID:20807672</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=20060049071&hterms=elephants&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D70%26Ntt%3Delephants','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=20060049071&hterms=elephants&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D70%26Ntt%3Delephants"><span><span class="hlt">Shock</span>, Post-<span class="hlt">Shock</span> Annealing, and Post-Annealing <span class="hlt">Shock</span> in Ureilites</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Rubin, Alan E.</p> <p>2006-01-01</p> <p>The thermal and <span class="hlt">shock</span> histories of ureilites can be divided into four periods: 1) formation, 2) initial <span class="hlt">shock</span>, 3) post-<span class="hlt">shock</span> annealing, and 4) post-annealing <span class="hlt">shock</span>. Period 1 occurred approx.4.55 Ga ago when ureilites formed by melting chondritic material. Impact events during period 2 caused silicate darkening, undulose to mosaic extinction in olivines, and the formation of diamond, lonsdaleite, and chaoite from indigenous carbonaceous material. Alkali-rich fine-grained silicates may have been introduced by impact injection into ureilites during this period. About 57% of the ureilites were unchanged after period 2. During period 3 events, impact-induced annealing caused previously mosaicized olivine grains to become aggregates of small unstrained crystals. Some ureilites experienced reduction as FeO at the edges of olivine grains reacted with C from the matrix. Annealing may also be responsible for coarsening of graphite in a few ureilites, forming euhedral-appearing, idioblastic crystals. Orthopyroxene in Meteorite Hills (MET) 78008 may have formed from pigeonite by annealing during this period. The Rb-Sr internal isochron age of approx.4.0 Ga for MET 78008 probably dates the annealing event. At this late date, impacts are the only viable heat source. About 36% of ureilites experienced period 3 events, but remained unchanged afterwards. During period 4, approx.7% of the ureilites were <span class="hlt">shocked</span> again, as is evident in the polymict breccia, Elephant Moraine (EET) 83309. This rock contains annealed mosaicized olivine aggregates composed of small individual olivine crystals that exhibit undulose extinction. Ureilites may have formed by impact-melting chondritic material on a primitive body with heterogeneous O isotopes. Plagioclase was preferentially lost from the system due to its low impedance to <span class="hlt">shock</span> <span class="hlt">compression</span>. Brief melting and rapid burial minimized the escape of planetary-type noble gases from the ureilitic melts. Incomplete separation of metal from silicates</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017APS..MAR.R2009B','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017APS..MAR.R2009B"><span>High dynamic range spectroscopic studies of <span class="hlt">shocked</span> nitromethane</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Bhowmick, Mithun; Nissen, Erin J.; Dlott, Dana D.</p> <p></p> <p>In this talk we describe a tabletop apparatus that can reproducibly drive <span class="hlt">shocks</span> through tiny cells containing liquid arranged in an array for high-throughput <span class="hlt">shock</span> <span class="hlt">compression</span> studies. This talk will focus on nitromethane, a liquid reactive to <span class="hlt">shocks</span> and capable of detonation. In our studies, a laser-driven flyer plate was used to <span class="hlt">shock</span> nitromethane, and a spectrometer with high dynamic range was employed to measure emission spectra from nanosecond to millisecond time scales. Typically, 50 single-<span class="hlt">shock</span> experiments were performed per day with precisely controllable <span class="hlt">shock</span> speeds below, above, or equal to the detonation <span class="hlt">shock</span> speed. The emission spectra provide temperature histories using the graybody approximation. The ability to conveniently <span class="hlt">shock</span> nitromethane on a benchtop will be used with isotopically substituted and amine-sensitized nitromethane and in future will be combined with other spectroscopies such as infrared absorption. Multidisciplinary University Research Initiative (MURI), Office of Naval Research.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19720026627&hterms=cation&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D80%26Ntt%3Dcation','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19720026627&hterms=cation&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D80%26Ntt%3Dcation"><span>Cation disorder in <span class="hlt">shocked</span> orthopyroxene.</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Dundon, R. W.; Hafner, S. S.</p> <p>1971-01-01</p> <p>The study of cation distributions over nonequivalent lattice sites in minerals may reveal information on the history of temperature and pressure in rocks. Chemically homogeneous orthopyroxene specimens were <span class="hlt">shocked</span> under well-controlled conditions in the laboratory in order to provide a basis for the interpretation of more complex natural materials. As a result of the investigation it is concluded that the distribution of magnesium and <span class="hlt">iron</span> over the M1 and M2 positions in Bamle enstatite <span class="hlt">shocked</span> at 1 megabar is highly disordered. It corresponds to an equilibrium distribution of at least 1000 C.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017APS..SHK.B6004S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017APS..SHK.B6004S"><span>Multiphase Modeling of Secondary Atomization in a <span class="hlt">Shock</span> Environment</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>St. Clair, Jeffrey; McGrath, Thomas; Balachandar, Sivaramakrishnan</p> <p>2017-06-01</p> <p>Understanding and developing accurate modeling strategies for <span class="hlt">shock</span>-particulate interaction remains a challenging and important topic, with application to energetic materials development, volcanic eruptions, and safety/risk assessment. This work presents computational modeling of <span class="hlt">compressible</span> multiphase flows with <span class="hlt">shock</span>-induced droplet atomization. Droplet size has a strong influence on the interphase momentum and heat transfer. A test case is presented that is sensitive to this, requiring the dynamic modeling of the secondary atomization process occurring when the <span class="hlt">shock</span> impacts the droplets. An Eulerian-Eulerian computational model that treats all phases as <span class="hlt">compressible</span>, is hyperbolic and satisfies the 2nd Law of Thermodynamics is applied. Four different breakup models are applied to the test case in which a planar <span class="hlt">shock</span> wave encounters a cloud of water droplets. The numerical results are compared with both experimental and previously-generated modeling results. The effect of the drag relation used is also investigated. The computed results indicate the necessity of using a droplet breakup model for this application, and the relative accuracy of results obtained with the different droplet breakup and drag models is discussed.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017JPhCS.950d2037C','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017JPhCS.950d2037C"><span>Implementation of Hydrodynamic Simulation Code in <span class="hlt">Shock</span> Experiment Design for Alkali Metals</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Coleman, A. L.; Briggs, R.; Gorman, M. G.; Ali, S.; Lazicki, A.; Swift, D. C.; Stubley, P. G.; McBride, E. E.; Collins, G.; Wark, J. S.; McMahon, M. I.</p> <p>2017-10-01</p> <p><span class="hlt">Shock</span> <span class="hlt">compression</span> techniques enable the investigation of extreme P-T states. In order to probe off-Hugoniot regions of P-T space, target makeup and laser pulse parameters must be carefully designed. HYADES is a hydrodynamic simulation code which has been successfully utilised to simulate <span class="hlt">shock</span> <span class="hlt">compression</span> events and refine the experimental parameters required in order to explore new P-T states in alkali metals. Here we describe simulations and experiments on potassium, along with the techniques required to access off-Hugoniot states.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19950042225&hterms=makeup&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D90%26Ntt%3Dmakeup','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19950042225&hterms=makeup&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D90%26Ntt%3Dmakeup"><span><span class="hlt">Shock</span> recovery analogs and the origin of mesosiderites. [Abstract only</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Rowan, L. R.</p> <p>1994-01-01</p> <p>The origin of mesosiderites, which consist of approximately equal-weight proportions of Fe-Ni metal and silicates (gabbros, basalts, orthopyroxenites, dunites), remains an interesting and complex problem in meteoritics. There is general agreement that multiple impact events were probably involved in the formation of these brecciated stony-<span class="hlt">iron</span> meteorites, but given the heterogeneity of mesosiderites, additional processes have been invoked to explain the unique and intricate textural and compositional makeup of mesosiderites. We conducted a series of <span class="hlt">shock</span> recovery experiments to test the impact event(s) scenario. The results indicated significant similarities between the <span class="hlt">shocked</span> analogs and many mesosiderites. We have compared our analogs with a suite of thin sections of Barea mesosiderite. I have conducted a series of flash heating experiments in which equal-weight proportions of gabbro and stainless steel (SS304) powders were <span class="hlt">compressed</span> into small charges and heated under reducing conditions for short times. These experiments were used to bracket localized, peak postshock temperatures in our analog shots and to compare the mixing relations between the silicate and metal. The <span class="hlt">shock</span> recovery experiments used porous metal-silicate powder starting mixtures, therefore our experiments are most analogous to an impact scenario where the target is an asteroidal regolith surface composed of a loose mixture of Fe-Ni metal and heterogeneous silicates. Analog experiments may really describe a secondary impact process similar to the late-stage, localized impact melting event. This leaves one of the crucial questions about mesosiderite genesis unanswered, namely what is the source of the Fe-Ni metal that is so intimately distributed in these meteorites?</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2010AGUFMMR44A..06W','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2010AGUFMMR44A..06W"><span>Equation of state of molten fayalite (Fe2SiO4)</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Waller, C.; Liu, Q.; Agee, C. B.; Asimow, P. D.; Lange, R. A.</p> <p>2010-12-01</p> <p>We have conducted new equation of state measurements on liquid fayalite (Fe2SiO4) in a collaborative, multi-technique study. Using a shared bulk starting material, we have measured the liquid density, the bulk modulus (K), and its pressure derivative (K’) from 1 atm to 163 GPa using 1-atm double-bob Archimedean and ultrasonic, sink/float, and <span class="hlt">shock</span> wave techniques to form a coherent, internally consistent equation of state. Previous <span class="hlt">shock</span> studies of liquid fayalite were conducted up to pressures of 40 GPa1; we extended this data set with two additional pre-heated, molten (1573 K) fayalite <span class="hlt">shock</span> <span class="hlt">compression</span> experiments at 121 and 163 GPa. Linear fitting of this data in <span class="hlt">shock</span> velocity (US)-particle velocity (up) space defines a Hugoniot with an unconstrained zero-pressure intercept that crosses within error at the bulk sound speed (Co) determined by ultrasonic techniques. Fixing the intercept at this ultrasonic value reduces the error on the linear fit and yields the relation: US =1.65(0.02)up+ 2.4377(0.006) km/s. This relationship indicates that the behavior of the liquid is relaxed during <span class="hlt">shock</span> <span class="hlt">compression</span> and demonstrates consistency across experimental methods. Likewise, results from new static <span class="hlt">compression</span> sink/float experiments conducted in piston-cylinder and multi-anvil devices are in agreement with <span class="hlt">shock</span> wave and ultrasonic data, consistent with an isothermal K=19.4 and K’=5.57 at 1500°C. In solid materials, the Grüneisen parameter (γ) generally decreases upon <span class="hlt">compression</span>. However, preliminary calculations for γ of this liquid using additional initially solid <span class="hlt">shock</span> data from Chen et al.(2002) indicate that γ increases upon <span class="hlt">compression</span>. Using the functional form γ = γo(ρo/ρ)q at a density of 7.65 Mg/m3 yields a q value of -1.77 (γo = 0.41 is known from low-pressure data), which is similar to the reported q values of forsterite2, enstatite3, and anorthite-diopside liquids4. This result shows that <span class="hlt">iron</span>-bearing mafic to ultramafic silicate liquids</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/22317361','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/22317361"><span>Does team lifting increase the variability in peak lumbar <span class="hlt">compression</span> in ironworkers?</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Faber, Gert; Visser, Steven; van der Molen, Henk F; Kuijer, P Paul F M; Hoozemans, Marco J M; Van Dieën, Jaap H; Frings-Dresen, Monique H W</p> <p>2012-01-01</p> <p>Ironworkers frequently perform heavy lifting tasks in teams of two or four workers. Team lifting could potentially lead to a higher variation in peak lumbar <span class="hlt">compression</span> forces than lifts performed by one worker, resulting in higher maximal peak lumbar <span class="hlt">compression</span> forces. This study compared single-worker lifts (25-kg, <span class="hlt">iron</span> bar) to two-worker lifts (50-kg, two <span class="hlt">iron</span> bars) and to four-worker lifts (100-kg, <span class="hlt">iron</span> lattice). Inverse dynamics was used to calculate peak lumbar <span class="hlt">compression</span> forces. To assess the variability in peak lumbar loading, all three lifting tasks were performed six times. Results showed that the variability in peak lumbar loading was somewhat higher in the team lifts compared to the single-worker lifts. However, despite this increased variability, team lifts did not result in larger maximum peak lumbar <span class="hlt">compression</span> forces. Therefore, it was concluded that, from a biomechanical point of view, team lifting does not result in an additional risk for low back complaints in ironworkers.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017APS..SHK.L4003W','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017APS..SHK.L4003W"><span>100J Pulsed Laser <span class="hlt">Shock</span> Driver for Dynamic <span class="hlt">Compression</span> Research</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Wang, X.; Sethian, J.; Bromage, J.; Fochs, S.; Broege, D.; Zuegel, J.; Roides, R.; Cuffney, R.; Brent, G.; Zweiback, J.; Currier, Z.; D'Amico, K.; Hawreliak, J.; Zhang, J.; Rigg, P. A.; Gupta, Y. M.</p> <p>2017-06-01</p> <p>Logos Technologies and the Laboratory for Laser Energetics (LLE, University of Rochester) - in partnership with Washington State University - have designed, built and deployed a one of a kind 100J pulsed UV (351 nm) laser system to perform real-time, x-ray diffraction and imaging experiments in laser-driven <span class="hlt">compression</span> experiments at the Dynamic <span class="hlt">Compression</span> Sector (DCS) at the Advanced Photon Source, Argonne National Laboratory. The laser complements the other dynamic <span class="hlt">compression</span> drivers at DCS. The laser system features beam smoothing for 2-d spatially uniform loading of samples and four, highly reproducible, temporal profiles (total pulse duration: 5-15 ns) to accommodate a wide variety of scientific needs. Other pulse shapes can be achieved as the experimental needs evolve. Timing of the laser pulse is highly precise (<200 ps) to allow accurate synchronization of the x-rays with the dynamic <span class="hlt">compression</span> event. Details of the laser system, its operating parameters, and representative results will be presented. Work supported by DOE/NNSA.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2011ArRMA.200..491B','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2011ArRMA.200..491B"><span>Existence and Stability of Viscoelastic <span class="hlt">Shock</span> Profiles</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Barker, Blake; Lewicka, Marta; Zumbrun, Kevin</p> <p>2011-05-01</p> <p>We investigate existence and stability of viscoelastic <span class="hlt">shock</span> profiles for a class of planar models including the incompressible shear case studied by Antman and Malek-Madani. We establish that the resulting equations fall into the class of symmetrizable hyperbolic-parabolic systems, hence spectral stability implies linearized and nonlinear stability with sharp rates of decay. The new contributions are treatment of the <span class="hlt">compressible</span> case, formulation of a rigorous nonlinear stability theory, including verification of stability of small-amplitude Lax <span class="hlt">shocks</span>, and the systematic incorporation in our investigations of numerical Evans function computations determining stability of large-amplitude and nonclassical type <span class="hlt">shock</span> profiles.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1179624-luminescence-from-edge-fracture-shocked-lithium-fluoride-crystals','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1179624-luminescence-from-edge-fracture-shocked-lithium-fluoride-crystals"><span>Luminescence from edge fracture in <span class="hlt">shocked</span> lithium fluoride crystals</span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>Turley, W. D.; Stevens, G. D.; Capelle, G. A.; ...</p> <p>2013-04-03</p> <p>Light emitted from a [100] lithium fluoride crystal was characterized under <span class="hlt">shock</span> wave <span class="hlt">compression</span> to 28 GPa followed by complete stress release at the edges. We examined the light using time-gated optical spectrometry and imaging, time-resolved optical emission measurements, and hydrodynamic modeling. The <span class="hlt">shock</span> arrival at the circumference of the crystal was delayed relative to the center so that the two regions could be studied at different times. The majority of the light emission originated when the <span class="hlt">shock</span> waves released at the circumference of the crystal. Unlike previously reported results for <span class="hlt">shocked</span> lithium fluoride, we found that the light spectrummore » is not strictly broad band, but has spectral lines associated with atomic lithium in addition to a broad band background. Also, the emission spectrum depends strongly on the gas surrounding the sample. Based on our observations, the line emission appears to be related to fracture of the lithium fluoride crystal from the <span class="hlt">shock</span> wave releasing at the edges. Moreover, experimenters frequently utilize lithium fluoride crystals as transparent windows for observing <span class="hlt">shock</span> <span class="hlt">compressed</span> samples. Because of the experimental geometries used, the <span class="hlt">shock</span> wave in such cases often reaches the circumference of the window at nearly the same moment as when it reaches the center of the sample-window interface. Light generated at the circumference could contaminate the measurement at the interface when this light scatters into the observed region. Finally, this background light may be reduced or avoided using experimental geometries which delay the arrival of the <span class="hlt">shock</span> wave at the edges of the crystal.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/1996ApJ...473..347M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/1996ApJ...473..347M"><span>Renormalized Two-Fluid Hydrodynamics of Cosmic-Ray--modified <span class="hlt">Shocks</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Malkov, M. A.; Voelk, H. J.</p> <p>1996-12-01</p> <p>A simple two-fluid model of diffusive <span class="hlt">shock</span> acceleration, introduced by Axford, Leer, & Skadron and Drury & Völk, is revisited. This theory became a chief instrument in the studies of <span class="hlt">shock</span> modification due to particle acceleration. Unfortunately its most intriguing steady state prediction about a significant enhancement of the <span class="hlt">shock</span> <span class="hlt">compression</span> and a corresponding increase of the cosmic-ray production violates assumptions which are critical for the derivation of this theory. In particular, for strong <span class="hlt">shocks</span> the spectral flattening makes a cutoff-independent definition of pressure and energy density impossible and therefore causes an additional closure problem. Confining ourselves for simplicity to the case of plane <span class="hlt">shocks</span>, assuming reacceleration of a preexisting cosmic-ray population, we argue that also under these circumstances the kinetic solution has a rather simple form. It can be characterized by only a few parameters, in the simplest case by the slope and the magnitude of the momentum distribution at the upper momentum cutoff. We relate these parameters to standard hydrodynamic quantities like the overall <span class="hlt">shock</span> <span class="hlt">compression</span> ratio and the downstream cosmic-ray pressure. The two-fluid theory produced in this way has the traditional form but renormalized closure parameters. By solving the renormalized Rankine-Hugoniot equations, we show that for the efficient stationary solution, most significant for cosmic-ray acceleration, the renormalization is needed in the whole parameter range of astrophysical interest.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20100024367','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20100024367"><span>Micro-Ramps for External <span class="hlt">Compression</span> Low-Boom Inlets</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Rybalko, Michael; Loth, Eric; Chima, Rodrick V.; Hirt, Stefanie M.; DeBonis, James R.</p> <p>2010-01-01</p> <p>The application of vortex generators for flow control in an external <span class="hlt">compression</span>, axisymmetric, low-boom concept inlet was investigated using RANS simulations with three-dimensional (3-D), structured, chimera (overset) grids and the WIND-US code. The low-boom inlet design is based on previous scale model 1- by 1-ft wind tunnel tests and features a zero-angle cowl and relaxed isentropic <span class="hlt">compression</span> centerbody spike, resulting in defocused oblique <span class="hlt">shocks</span> and a weak terminating normal <span class="hlt">shock</span>. Validation of the methodology was first performed for micro-ramps in supersonic flow on a flat plate with and without oblique <span class="hlt">shocks</span>. For the inlet configuration, simulations with several types of vortex generators were conducted for positions both upstream and downstream of the terminating normal <span class="hlt">shock</span>. The performance parameters included incompressible axisymmetric shape factor, separation area, inlet pressure recovery, and massflow ratio. The design of experiments (DOE) methodology was used to select device size and location, analyze the resulting data, and determine the optimal choice of device geometry. The optimum upstream configuration was found to substantially reduce the post-<span class="hlt">shock</span> separation area but did not significantly impact recovery at the aerodynamic interface plane (AIP). Downstream device placement allowed for fuller boundary layer velocity profiles and reduced distortion. This resulted in an improved pressure recovery and massflow ratio at the AIP compared to the baseline solid-wall configuration.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1240056-radiative-shocks-produced-from-spherical-cryogenic-implosions-national-ignition-facility','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1240056-radiative-shocks-produced-from-spherical-cryogenic-implosions-national-ignition-facility"><span>Radiative <span class="hlt">shocks</span> produced from spherical cryogenic implosions at the National Ignition Facility</span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>Pak, A.; Divol, L.; Gregori, G.; ...</p> <p>2013-05-20</p> <p>Spherically expanding radiative <span class="hlt">shock</span> waves have been observed from inertially confined implosion experiments at the National Ignition Facility. In these experiments, a spherical fusion target, initially 2 mm in diameter, is <span class="hlt">compressed</span> via the pressure induced from the ablation of the outer target surface. At the peak <span class="hlt">compression</span> of the capsule, x-ray and nuclear diagnostics indicate the formation of a central core, with a radius and ion temperature of ~20 μm and ~ 2 keV, respectively. This central core is surrounded by a cooler <span class="hlt">compressed</span> shell of deuterium-tritium fuel that has an outer radius of ~40 μm and a densitymore » of >500 g/cm 3. Using inputs from multiple diagnostics, the peak pressure of the <span class="hlt">compressed</span> core has been inferred to be of order 100 Gbar for the implosions discussed here. Furthermore, the <span class="hlt">shock</span> front, initially located at the interface between the high pressure <span class="hlt">compressed</span> fuel shell and surrounding in-falling low pressure ablator plasma, begins to propagate outwards after peak <span class="hlt">compression</span> has been reached.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016APS..DPPN10144H','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016APS..DPPN10144H"><span>Measuring the properties of <span class="hlt">shock</span> released Quartz and Parylene-N</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Hawreliak, James; Karasik, Max; Oh, Jaechul; Aglitskiy, Yefim</p> <p>2016-10-01</p> <p>The high pressure and temperature properties of Quartz and hydrocarbons are important to high energy density (HED) research and inertial confinement fusion (ICF) science. The bulk of HED material research studies the single <span class="hlt">shock</span> Hugoniot. Here, we present experimental results from the NIKE laser where quartz and parylene-N are <span class="hlt">shock</span> <span class="hlt">compressed</span> to high pressure and temperature and the release state is measured through x-ray imaging. The <span class="hlt">shock</span> state is characterized by <span class="hlt">shock</span> front velocity measurements using VISAR and the release state is characterized by using side-on streaked x-ray radiography.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_15");'>15</a></li> <li><a href="#" onclick='return showDiv("page_16");'>16</a></li> <li class="active"><span>17</span></li> <li><a href="#" onclick='return showDiv("page_18");'>18</a></li> <li><a href="#" onclick='return showDiv("page_19");'>19</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_17 --> <div id="page_18" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_16");'>16</a></li> <li><a href="#" onclick='return showDiv("page_17");'>17</a></li> <li class="active"><span>18</span></li> <li><a href="#" onclick='return showDiv("page_19");'>19</a></li> <li><a href="#" onclick='return showDiv("page_20");'>20</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="341"> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018PhFl...30e6101D','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018PhFl...30e6101D"><span>Spectrum study on unsteadiness of <span class="hlt">shock</span> wave-vortex ring interaction</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Dong, Xiangrui; Yan, Yonghua; Yang, Yong; Dong, Gang; Liu, Chaoqun</p> <p>2018-05-01</p> <p><span class="hlt">Shock</span> oscillation with low-frequency unsteadiness commonly occurs in supersonic flows and is a top priority for the control of flow separation caused by <span class="hlt">shock</span> wave and boundary layer interaction. In this paper, the interaction of the <span class="hlt">shock</span> caused by the <span class="hlt">compression</span> ramp and the vortex rings generated by a micro-vortex generator (MVG) in a supersonic flow at Ma = 2.5 is simulated by the implicit large eddy simulation method. The analysis of observation and the frequency of both the vortex ring motion and the <span class="hlt">shock</span> oscillation is carried out. The results show that the <span class="hlt">shock</span> produced by a <span class="hlt">compression</span> ramp flow at Ma = 2.5 has a dominant non-dimensional low frequency, which is around St = 0.002, while the vortex rings behind the MVG have a dominant high frequency which is around St = 0.038. The dominant low frequency of the <span class="hlt">shock</span>, which is harmful, can be removed or weakened through the <span class="hlt">shock</span>-vortex ring interaction by the vortex rings which generate high frequency fluctuations. In the <span class="hlt">shock</span> and vortex ring interaction region, a dominant high frequency St = 0.037-0.038 has been detected rather than the low frequency St = 0.002, which indicates that the vortex ring is stiff enough to break or weaken the <span class="hlt">shock</span>. This analysis could provide an effective tool to remove or weaken the low frequency pressure fluctuation below 500 Hz, which has a negative effect on the flight vehicle structures and the environmental protection, through the high frequency vortex generation.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20030108295','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20030108295"><span>Magnetohydrodynamic Jump Conditions for Oblique Relativistic <span class="hlt">Shocks</span> with Gyrotropic Pressure</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Double, Glen P.; Baring, Matthew G.; Jones, Frank C.; Ellison, Donald C.</p> <p>2003-01-01</p> <p><span class="hlt">Shock</span> jump conditions, i.e., the specification of the downstream parameters of the gas in terms of the upstream parameters, are obtained for steady-state, plane <span class="hlt">shocks</span> with oblique magnetic fields and arbitrary flow speeds. This is done by combining the continuity of particle number flux and the electromagnetic boundary conditions at the <span class="hlt">shock</span> with the magnetohydrodynamic conservation laws derived from the stress-energy tensor. For ultrarelativistic and nonrelativistic <span class="hlt">shocks</span>, the jump conditions may be solved analytically. For mildly relativistic <span class="hlt">shocks</span>, analytic solutions are obtained for isotropic pressure using an approximation for the adiabatic index that is valid in high sonic Mach number cases. Examples assuming isotropic pressure illustrate how the <span class="hlt">shock</span> <span class="hlt">compression</span> ratio depends on the <span class="hlt">shock</span> speed and obliquity. In the more general case of gyrotropic pressure, the jump conditions cannot be solved analytically with- out additional assumptions, and the effects of gyrotropic pressure are investigated by parameterizing the distribution of pressure parallel and perpendicular to the magnetic field. Our numerical solutions reveal that relatively small departures from isotropy (e.g., approximately 20%) produce significant changes in the <span class="hlt">shock</span> <span class="hlt">compression</span> ratio, r , at all <span class="hlt">shock</span> Lorentz factors, including ultrarelativistic ones, where an analytic solution with gyrotropic pressure is obtained. In particular, either dynamically important fields or significant pressure anisotropies can incur marked departures from the canonical gas dynamic value of r = 3 for a <span class="hlt">shocked</span> ultrarelativistic flow and this may impact models of particle acceleration in gamma-ray bursts and other environments where relativistic <span class="hlt">shocks</span> are inferred. The jump conditions presented apply directly to test-particle acceleration, and will facilitate future self-consistent numerical modeling of particle acceleration at oblique, relativistic <span class="hlt">shocks</span>; such models include the modification of the fluid</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3708341','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3708341"><span><span class="hlt">Iron</span> Absorption in Drosophila melanogaster</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Mandilaras, Konstantinos; Pathmanathan, Tharse; Missirlis, Fanis</p> <p>2013-01-01</p> <p>The way in which Drosophila melanogaster acquires <span class="hlt">iron</span> from the diet remains poorly understood despite <span class="hlt">iron</span> absorption being of vital significance for larval growth. To describe the process of organismal <span class="hlt">iron</span> absorption, consideration needs to be given to cellular <span class="hlt">iron</span> import, storage, export and how intestinal epithelial cells sense and respond to <span class="hlt">iron</span> availability. Here we review studies on the Divalent Metal Transporter-1 homolog Malvolio (<span class="hlt">iron</span> import), the recent discovery that Multicopper Oxidase-1 has ferroxidase activity (<span class="hlt">iron</span> export) and the role of ferritin in the process of <span class="hlt">iron</span> acquisition (<span class="hlt">iron</span> storage). We also describe what is known about <span class="hlt">iron</span> regulation in insect cells. We then draw upon knowledge from mammalian <span class="hlt">iron</span> homeostasis to identify candidate genes in flies. Questions arise from the lack of conservation in Drosophila for key mammalian players, such as ferroportin, hepcidin and all the components of the hemochromatosis-related pathway. Drosophila and other insects also lack erythropoiesis. Thus, systemic <span class="hlt">iron</span> regulation is likely to be conveyed by different signaling pathways and tissue requirements. The significance of regulating intestinal <span class="hlt">iron</span> uptake is inferred from reports linking Drosophila developmental, immune, heat-<span class="hlt">shock</span> and behavioral responses to <span class="hlt">iron</span> sequestration. PMID:23686013</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19820022410','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19820022410"><span>Multidomain approach for calculating <span class="hlt">compressible</span> flows</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Cambier, L.; Chazzi, W.; Veuillot, J. P.; Viviand, H.</p> <p>1982-01-01</p> <p>A multidomain approach for calculating <span class="hlt">compressible</span> flows by using unsteady or pseudo-unsteady methods is presented. This approach is based on a general technique of connecting together two domains in which hyperbolic systems (that may differ) are solved with the aid of compatibility relations associated with these systems. Some examples of this approach's application to calculating transonic flows in ideal fluids are shown, particularly the adjustment of <span class="hlt">shock</span> waves. The approach is then applied to treating a <span class="hlt">shock</span>/boundary layer interaction problem in a transonic channel.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2013prpl.conf1K057G','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2013prpl.conf1K057G"><span>The diagnostic capability of <span class="hlt">iron</span> limes</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Giannini, Teresa; Nisini, Brunella; Antoniucci, Simone; Alcala, Juan; Bacciotti, Francesca; Bonito, Rosaria; Podio, Linda; Stelzer, Beate; Whelan, Emma</p> <p>2013-07-01</p> <p>We present the VLT/X-Shooter spectrum of two jets from young protostars of different luminosity and mass, ESO-Halpha 574 and Par-Lup 3-4. In the covered spectral range (350-2500 nm) we detected more than 100 [FeII] and [FeIII] lines, which are used to precisely probe the key physical parameters of the gas (electron density and temperature, ionization degree, visual extinction). These quantities have been compared with <span class="hlt">shock</span>-model predictions, which suggest that only the higher luminosity source (ESO-Ha 574) is able to drive a high-velocity and dissociative <span class="hlt">shock</span>. The diagnostic capability of <span class="hlt">Iron</span>, proven on the presented objects, represents a unique tool for the following reasons: 1) the large number of lines in the uv-infrared range makes possible to trace the physical conditions in a very large range of the parameter space; 2) at variance with the diagnostic commonly performed with other species, such as Oxygen, Nitrogen, and Sulphur, no assumption on the relative abundance is needed, since all the parameters are derived from line ratios of the same species; 3) in the unperturbed ISM, <span class="hlt">Iron</span> is locked on the grain surfaces, while it is released in gas-phase if gas-grain or grain-grain collisions occur within a <span class="hlt">shock</span>. Therefore the <span class="hlt">Iron</span> abundance (derivable from ratios of <span class="hlt">Iron</span> lines with those of other volatile species) is a direct probe of the presence of dust in the jet beam, an information crucial to understand whether jets originate close to the star or in the circumstellar disk.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017yCat..22290034S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017yCat..22290034S"><span>VizieR Online Data Catalog: Effects of preionization in radiative <span class="hlt">shocks</span> (Sutherland+, 2017)</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Sutherland, R. S.; Dopita, M. A.</p> <p>2017-06-01</p> <p>In this paper we treat the preionization problem in <span class="hlt">shocks</span> over the velocity range 10<vs<1500km/s in a self-consistent manner. We identify four distinct classes of solutions controlled by the value of the <span class="hlt">shock</span>-precursor parameter, {Psi}=Q/vs, where Q is the ionization parameter of the UV photons escaping upstream. This parameter determines both the temperature and the degree of ionization of the gas entering the <span class="hlt">shock</span>. In increasing velocity, the <span class="hlt">shock</span> solution regimes are cold neutral precursors (vs<~40km/s), warm neutral precursors (40<~vs<~75km/s), warm partly ionized precursors (75<~vs<~120km/s), and fast <span class="hlt">shocks</span> in which the preshock gas is in photoionization equilibrium and is fully ionized. The main effect of a magnetic field is to push these velocity ranges to higher values and to limit the postshock <span class="hlt">compression</span>. In order to facilitate comparison with observations of <span class="hlt">shocks</span>, we provide a number of convenient scaling relationships for parameters, such as postshock temperature, <span class="hlt">compression</span> factors, cooling lengths, and Hβ and X-ray luminosity. (4 data files).</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2010RScI...81l6103C','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2010RScI...81l6103C"><span>Note: A table-top blast driven <span class="hlt">shock</span> tube</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Courtney, Michael W.; Courtney, Amy C.</p> <p>2010-12-01</p> <p>The prevalence of blast-induced traumatic brain injury in conflicts in Iraq and Afghanistan has motivated laboratory scale experiments on biomedical effects of blast waves and studies of blast wave transmission properties of various materials in hopes of improving armor design to mitigate these injuries. This paper describes the design and performance of a table-top <span class="hlt">shock</span> tube that is more convenient and widely accessible than traditional <span class="hlt">compression</span> driven and blast driven <span class="hlt">shock</span> tubes. The design is simple: it is an explosive driven <span class="hlt">shock</span> tube employing a rifle primer that explodes when impacted by the firing pin. The firearm barrel acts as the <span class="hlt">shock</span> tube, and the <span class="hlt">shock</span> wave emerges from the muzzle. The small size of this <span class="hlt">shock</span> tube can facilitate localized application of a blast wave to a subject, tissue, or material under test.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/21198058','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/21198058"><span>Note: A table-top blast driven <span class="hlt">shock</span> tube.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Courtney, Michael W; Courtney, Amy C</p> <p>2010-12-01</p> <p>The prevalence of blast-induced traumatic brain injury in conflicts in Iraq and Afghanistan has motivated laboratory scale experiments on biomedical effects of blast waves and studies of blast wave transmission properties of various materials in hopes of improving armor design to mitigate these injuries. This paper describes the design and performance of a table-top <span class="hlt">shock</span> tube that is more convenient and widely accessible than traditional <span class="hlt">compression</span> driven and blast driven <span class="hlt">shock</span> tubes. The design is simple: it is an explosive driven <span class="hlt">shock</span> tube employing a rifle primer that explodes when impacted by the firing pin. The firearm barrel acts as the <span class="hlt">shock</span> tube, and the <span class="hlt">shock</span> wave emerges from the muzzle. The small size of this <span class="hlt">shock</span> tube can facilitate localized application of a blast wave to a subject, tissue, or material under test.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018ShWav..28..401R','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018ShWav..28..401R"><span>Comparison of geometrical <span class="hlt">shock</span> dynamics and kinematic models for <span class="hlt">shock</span>-wave propagation</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Ridoux, J.; Lardjane, N.; Monasse, L.; Coulouvrat, F.</p> <p>2018-03-01</p> <p>Geometrical <span class="hlt">shock</span> dynamics (GSD) is a simplified model for nonlinear <span class="hlt">shock</span>-wave propagation, based on the decomposition of the <span class="hlt">shock</span> front into elementary ray tubes. Assuming small changes in the ray tube area, and neglecting the effect of the post-<span class="hlt">shock</span> flow, a simple relation linking the local curvature and velocity of the front, known as the A{-}M rule, is obtained. More recently, a new simplified model, referred to as the kinematic model, was proposed. This model is obtained by combining the three-dimensional Euler equations and the Rankine-Hugoniot relations at the front, which leads to an equation for the normal variation of the <span class="hlt">shock</span> Mach number at the wave front. In the same way as GSD, the kinematic model is closed by neglecting the post-<span class="hlt">shock</span> flow effects. Although each model's approach is different, we prove their structural equivalence: the kinematic model can be rewritten under the form of GSD with a specific A{-}M relation. Both models are then compared through a wide variety of examples including experimental data or Eulerian simulation results when available. Attention is drawn to the simple cases of <span class="hlt">compression</span> ramps and diffraction over convex corners. The analysis is completed by the more complex cases of the diffraction over a cylinder, a sphere, a mound, and a trough.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1334509-ray-thomson-scattering-measurements-temperature-density-from-multi-shocked-ch-capsules','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1334509-ray-thomson-scattering-measurements-temperature-density-from-multi-shocked-ch-capsules"><span>X-ray Thomson scattering measurements of temperature and density from multi-<span class="hlt">shocked</span> CH capsules</span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>Fletcher, L. B.; Glenzer, S. H.; Kritcher, A.; ...</p> <p>2013-05-24</p> <p>Proof-of-principle measurements of the electron densities, temperatures, and ionization states of spherically <span class="hlt">compressed</span> multi-<span class="hlt">shocked</span> CH (polystyrene) capsules have been achieved using spectrally resolved x-ray Thomson scattering. A total energy of 13.5 kJ incident on target is used to <span class="hlt">compress</span> a 70 μm thick CH shell above solid-mass density using three coalescing <span class="hlt">shocks</span>. Separately, a laser-produced zinc He-α x-ray source at 9 keV delayed 200 ps-800 ps after maximum <span class="hlt">compression</span> is used to probe the plasma in the non-collective scattering regime. The data show that x-ray Thomson scattering enables a complete description of the time-dependent hydrodynamic evolution of <span class="hlt">shock-compressed</span> CH capsules,more » with a maximum measured density of ρ > 6 g cm –3. Additionally, the results demonstrate that accurate measurements of x-ray scattering from bound-free transitions in the CH plasma demonstrate strong evidence that continuum lowering is the primary ionization mechanism of carbon L-shell electrons.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017APS..SHK.K3001B','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017APS..SHK.K3001B"><span>Studies in <span class="hlt">shocked</span> nitromethane through High dynamic range spectroscopy</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Bhowmick, Mithun; Nissen, Erin; Matveev, Sergey; Dlott, Dana</p> <p>2017-06-01</p> <p>In this talk we describe a tabletop apparatus that can reproducibly drive <span class="hlt">shocks</span> through tiny cells containing liquid arranged in an array for high-throughput <span class="hlt">shock</span> <span class="hlt">compression</span> studies. This talk will focus on nitromethane, a liquid reactive to <span class="hlt">shocks</span> and capable of detonation. In our studies, a laser-driven ?yer plate was used to <span class="hlt">shock</span> nitromethane, and a spectrometer with high dynamic range was employed to measure emission spectra from nanosecond to millisecond time scales. Typically, 50 single-<span class="hlt">shock</span> experiments were performed per day with precisely controllable <span class="hlt">shock</span> speeds below, above, or equal to the detonation <span class="hlt">shock</span> speed. The emission spectra provide temperature histories using the grey body approximation. The ability to conveniently <span class="hlt">shock</span> nitromethane on a benchtop was used with isotopically substituted and amine-sensitized nitromethane and in future will be combined with other spectroscopies such as infrared absorption. Multidisciplinary University Research Initiative (MURI), Office of Naval Research.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2011APS..SHK.T6002A','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2011APS..SHK.T6002A"><span>An Equation of State for Polymethylpentene (TPX) including Multi-<span class="hlt">Shock</span> Response</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Aslam, Tariq; Gustavsen, Richard; Sanchez, Nathaniel; Bartram, Brian</p> <p>2011-06-01</p> <p>The equation of state (EOS) of polymethylpentene (TPX) is examined through both single <span class="hlt">shock</span> Hugoniot data as well as more recent multi-<span class="hlt">shock</span> <span class="hlt">compression</span> and release experiments. Results from the recent multi-<span class="hlt">shock</span> experiments on LANL's 2-stage gas gun will be presented. A simple conservative Lagrangian numerical scheme utilizing total-variation-diminishing interpolation and an approximate Riemann solver will be presented as well as the methodology of calibration. It is shown that a simple Mie-Gruneisen EOS based off a Keane fitting form for the isentrope can replicate both the single <span class="hlt">shock</span> and multi-<span class="hlt">shock</span> experiments.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2012AIPC.1426..767A','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2012AIPC.1426..767A"><span>An equation of state for polymethylpentene (TPX) including multi-<span class="hlt">shock</span> response</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Aslam, Tariq D.; Gustavsen, Rick; Sanchez, Nathaniel; Bartram, Brian D.</p> <p>2012-03-01</p> <p>The equation of state (EOS) of polymethylpentene (TPX) is examined through both single <span class="hlt">shock</span> Hugoniot data as well as more recent multi-<span class="hlt">shock</span> <span class="hlt">compression</span> and release experiments. Results from the recent multi-<span class="hlt">shock</span> experiments on LANL's two-stage gas gun will be presented. A simple conservative Lagrangian numerical scheme utilizing total variation diminishing interpolation and an approximate Riemann solver will be presented as well as the methodology of calibration. It is shown that a simple Mie-Grüneisen EOS based on a Keane fitting form for the isentrope can replicate both the single <span class="hlt">shock</span> and multi-<span class="hlt">shock</span> experiments.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19760004931','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19760004931"><span>Normal- and oblique-<span class="hlt">shock</span> flow parameters in equilibrium air including attached-<span class="hlt">shock</span> solutions for surfaces at angles of attack, sweep, and dihedral</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Hunt, J. L.; Souders, S. W.</p> <p>1975-01-01</p> <p>Normal- and oblique-<span class="hlt">shock</span> flow parameters for air in thermochemical equilibrium are tabulated as a function of <span class="hlt">shock</span> angle for altitudes ranging from 15.24 km to 91.44 km in increments of 7.62 km at selected hypersonic speeds. Post-<span class="hlt">shock</span> parameters tabulated include flow-deflection angle, velocity, Mach number, <span class="hlt">compressibility</span> factor, isentropic exponent, viscosity, Reynolds number, entropy difference, and static pressure, temperature, density, and enthalpy ratios across the <span class="hlt">shock</span>. A procedure is presented for obtaining oblique-<span class="hlt">shock</span> flow properties in equilibrium air on surfaces at various angles of attack, sweep, and dihedral by use of the two-dimensional tabulations. Plots of the flow parameters against flow-deflection angle are presented at altitudes of 30.48, 60.96, and 91.44 km for various stream velocities.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19850040699&hterms=mediation&qs=N%3D0%26Ntk%3DAll%26Ntx%3Dmode%2Bmatchall%26Ntt%3Dmediation','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19850040699&hterms=mediation&qs=N%3D0%26Ntk%3DAll%26Ntx%3Dmode%2Bmatchall%26Ntt%3Dmediation"><span>Monte Carlo simulation of steady state <span class="hlt">shock</span> structure including cosmic ray mediation and particle escape</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Ellison, D. C.; Jones, F. C.; Eichler, D.</p> <p>1983-01-01</p> <p>Both hydrodynamic calculations (Drury and Volk, 1981, and Axford et al., 1982) and kinetic simulations imply the existence of thermal subshocks in high-Mach-number cosmic-ray-mediated <span class="hlt">shocks</span>. The injection efficiency of particles from the thermal background into the diffusive <span class="hlt">shock</span>-acceleration process is determined in part by the sharpness and <span class="hlt">compression</span> ratio of these subshocks. Results are reported for a Monte Carlo simulation that includes both the back reaction of accelerated particles on the inflowing plasma, producing a smoothing of the <span class="hlt">shock</span> transition, and the free escape of particles allowing arbitrarily large overall <span class="hlt">compression</span> ratios in high-Mach-number steady-state <span class="hlt">shocks</span>. Energy spectra and estimates of the proportion of thermal ions accelerated to high energy are obtained.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/1983ICRC....2..271E','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/1983ICRC....2..271E"><span>Monte Carlo simulation of steady state <span class="hlt">shock</span> structure including cosmic ray mediation and particle escape</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Ellison, D. C.; Jones, F. C.; Eichler, D.</p> <p>1983-08-01</p> <p>Both hydrodynamic calculations (Drury and Volk, 1981, and Axford et al., 1982) and kinetic simulations imply the existence of thermal subshocks in high-Mach-number cosmic-ray-mediated <span class="hlt">shocks</span>. The injection efficiency of particles from the thermal background into the diffusive <span class="hlt">shock</span>-acceleration process is determined in part by the sharpness and <span class="hlt">compression</span> ratio of these subshocks. Results are reported for a Monte Carlo simulation that includes both the back reaction of accelerated particles on the inflowing plasma, producing a smoothing of the <span class="hlt">shock</span> transition, and the free escape of particles allowing arbitrarily large overall <span class="hlt">compression</span> ratios in high-Mach-number steady-state <span class="hlt">shocks</span>. Energy spectra and estimates of the proportion of thermal ions accelerated to high energy are obtained.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/1992PhFlA...4.2700F','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/1992PhFlA...4.2700F"><span><span class="hlt">Shock</span> wave propagation in a magnetic flux tube</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Ferriz-Mas, A.; Moreno-Insertis, F.</p> <p>1992-12-01</p> <p>The propagation of a <span class="hlt">shock</span> wave in a magnetic flux tube is studied within the framework of the Brinkley-Kirkwood theory adapted to a radiating gas. Simplified thermodynamic paths along which the <span class="hlt">compressed</span> plasma returns to its initial state are considered. It is assumed that the undisturbed medium is uniform and that the flux tube is optically thin. The <span class="hlt">shock</span> waves investigated, which are described with the aid of the thin flux-tube approximation, are essentially slow magnetohydrodynamic <span class="hlt">shocks</span> modified by the constraint of lateral pressure balance between the flux tube and the surrounding field-free fluid; the confining external pressure must be balanced by the internal gas plus magnetic pressures. Exact analytical solutions giving the evolution of the <span class="hlt">shock</span> wave are obtained for the case of weak <span class="hlt">shocks</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2011APS..SHK.F1182S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2011APS..SHK.F1182S"><span>Electrical conductivity of MgH2 at multiple <span class="hlt">shock</span> <span class="hlt">compression</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Shakhray, Denis; Molodets, Alexander; Fortov, Vladimir</p> <p>2011-06-01</p> <p>The electrical conductivity of MgH2 has been studied under multishock <span class="hlt">compression</span>. Earlier we had been experimentally studied metallization possibility of alane at high pressures in conditions quasiisentropic <span class="hlt">compression</span> up to 100 GPa. A study of thermodynamic properties of MgH2 under multishock <span class="hlt">compression</span> has been carried out also. High pressures and temperatures were obtained with an explosive device, which accelerates the metallic impactor up to 3 km/s. Identification of the hydride in experiments was made on the basis of calculations of phase trajectories loading a material in the area of existence of polymorphic phases including high-pressure phases of magnesium hydride (α and γ MgH2, hP1 and hP2). It is shown that occurrence of magnesium hydride electrical conductivity occurs in the field of existence of high-pressure hP2 phase This work was partially supported by the Presidium of the Russian Academy of Sciences within the Program of Basic Research ``Thermal Physics and Mechanics of Extreme Energy Effects and Physics of Strongly <span class="hlt">Compressed</span> Matter and Russian Foundation for Basic Research Grant No. 10-02-01078.''</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017AGUFMSH51A2482H','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017AGUFMSH51A2482H"><span>Dispersive MHD <span class="hlt">Shock</span> Properties and Interactions with Alfven Solitons</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Hamilton, R.; Toll, K.; Ellis, C.</p> <p>2017-12-01</p> <p>The weakly nonlinear, weakly dispersive limit of Hall MHD with resistivity for 1D waves travelling nearly parallel to the ambient magnetic field reduces to the derivative nonlinear Schrödinger-Burgers (DNLSB) equation. This model equation describes the coupling between the Alfvenic and magnetosonic modes for a low b plasma. Without dissipation this model equation reduces to the DNLS which can be solved as an initial value problem using the Inverse Scattering Transformation through which the nonlinear component of the magnetic field profile can be represented as a combination of one-parameter bright and dark solitons as well as two-parameter solitons. The one-parameter solitons are constrained to travel at speeds ranging between the Alfvenic and magnetosonic characteristic speeds of the ambient field. We have found that these one-parameter solitons are effectively bound to a 1-2 Fast <span class="hlt">Shock</span> and will pass back and forth across the <span class="hlt">shock</span> until they are damped away with no apparent effect on the Fast <span class="hlt">Shock</span>. A similar mechanism is expected for a sufficiently <span class="hlt">compressive</span> Intermediate <span class="hlt">Shock</span> as it arises simply from two effects: damping of a one-parameter soliton causes it to speed up and, if it does not damp away, it will eventually overtake the <span class="hlt">shock</span>; passing forwards through a <span class="hlt">compressive</span> <span class="hlt">shock</span> the decrease of the field strength leads to a slowing of the soliton. We also discuss an extension of results [C. F. Kennel, R. D. Blandford, C. C. Wu, Phys. Fluids B 2(2), 1990] related to the time dependence of Intermediate <span class="hlt">Shocks</span> in the presence of dispersion.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2007AIPC..955..443G','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2007AIPC..955..443G"><span>AB INITIO Molecular Dynamics Simulations of Water Under Static and <span class="hlt">Shock</span> <span class="hlt">Compressed</span> Conditions</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Goldman, Nir; Fried, Laurence E.; Mundy, Christopher J.; Kuo, I.-F. William; Curioni, Alessandro; Reed, Evan J.</p> <p>2007-12-01</p> <p>We report herein a series of ab initio simulations of water under both static and <span class="hlt">shocked</span> conditions. We have calculated the coherent x-ray scattering intensity of several phases of water under high pressure, using ab initio Density Functional Theory (DFT). We provide new atomic scattering form factors for water at extreme conditions, which take into account frequently neglected changes in ionic charge and electron delocalization. We have also simulated liquid water undergoing <span class="hlt">shock</span> loading of velocities from 5-11 km/s using the Multi-Scale <span class="hlt">Shock</span> Technique (MSST). We show that Density Functional Theory (DFT) molecular dynamics results compare extremely well to experiments on the water <span class="hlt">shock</span> Hugoniot.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_16");'>16</a></li> <li><a href="#" onclick='return showDiv("page_17");'>17</a></li> <li class="active"><span>18</span></li> <li><a href="#" onclick='return showDiv("page_19");'>19</a></li> <li><a href="#" onclick='return showDiv("page_20");'>20</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_18 --> <div id="page_19" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_17");'>17</a></li> <li><a href="#" onclick='return showDiv("page_18");'>18</a></li> <li class="active"><span>19</span></li> <li><a href="#" onclick='return showDiv("page_20");'>20</a></li> <li><a href="#" onclick='return showDiv("page_21");'>21</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="361"> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19930045777&hterms=Increased+entropy&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D60%26Ntt%3DIncreased%2Bentropy','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19930045777&hterms=Increased+entropy&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D60%26Ntt%3DIncreased%2Bentropy"><span>Finite element computation of <span class="hlt">compressible</span> flows with the SUPG formulation</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Le Beau, G. J.; Tezduyar, T. E.</p> <p>1991-01-01</p> <p>Finite element computation of <span class="hlt">compressible</span> Euler equations is presented in the context of the streamline-upwind/Petrov-Galerkin (SUPG) formulation. The SUPG formulation, which is based on adding stabilizing terms to the Galerkin formulation, is further supplemented with a <span class="hlt">shock</span> capturing operator which addresses the difficulty in maintaining a satisfactory solution near discontinuities in the solution field. The <span class="hlt">shock</span> capturing operator, which has been derived from work done in entropy variables for a similar operator, is shown to lead to an appropriate level of additional stabilization near <span class="hlt">shocks</span>, without resulting in excessive numerical diffusion. An implicit treatment of the impermeable wall boundary condition is also presented. This treatment of the no-penetration condition offers increased stability for large Courant numbers, and accelerated convergence of the computations for both implicit and explicit applications. Several examples are presented to demonstrate the ability of this method to solve the equations governing <span class="hlt">compressible</span> fluid flow.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2013APS..SHK.C1005C','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2013APS..SHK.C1005C"><span>On the residual yield stress of <span class="hlt">shocked</span> metals</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Chapman, David; Eakins, Daniel; Savinykh, Andrey; Garkushin, Gennady; Kanel, Gennady; Razorenov, Sergey</p> <p>2013-06-01</p> <p>The measurement of the free-surface velocity is commonly employed in planar <span class="hlt">shock-compression</span> experiments. It is known that the peak free-surface velocity of a <span class="hlt">shocked</span> elastic-plastic material should be slightly less than twice the particle velocity behind <span class="hlt">shock</span> front; this difference being proportional to the yield stress. Precise measurement of the free-surface velocity can be a rich source of information on the effects of time and strain on material hardening or softening. With this objective, we performed comparative measurements of the free-surface velocity of <span class="hlt">shock</span> loaded aluminium AD1 and magnesium alloy Ma2 samples of various thicknesses in the range 0.2 mm to 5 mm. We observed the expected hysteresis in the elastic-plastic <span class="hlt">compression</span>-unloading cycle for both AD1 and Ma2; where qualitatively the peak free-surface velocity increased with increasing specimen thickness. However, the relative change in magnitude of hysteresis as function of specimen thickness observed for the Ma2 alloy was smaller than expected given the large observed change in precursor magnitude. We propose that softening due to multiplication of dislocations is relatively large in Ma2 and results in a smaller hysteresis in the elastic-plastic cycle.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2013APS..SHK.O2003L','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2013APS..SHK.O2003L"><span>International <span class="hlt">Shock</span>-Wave Database: Current Status</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Levashov, Pavel</p> <p>2013-06-01</p> <p><span class="hlt">Shock</span>-wave and related dynamic material response data serve for calibrating, validating, and improving material models over very broad regions of the pressure-temperature-density phase space. Since the middle of the 20th century vast amount of <span class="hlt">shock</span>-wave experimental information has been obtained. To systemize it a number of compendiums of <span class="hlt">shock</span>-wave data has been issued by LLNL, LANL (USA), CEA (France), IPCP and VNIIEF (Russia). In mid-90th the drawbacks of the paper handbooks became obvious, so the first version of the online <span class="hlt">shock</span>-wave database appeared in 1997 (http://www.ficp.ac.ru/rusbank). It includes approximately 20000 experimental points on <span class="hlt">shock</span> <span class="hlt">compression</span>, adiabatic expansion, measurements of sound velocity behind the <span class="hlt">shock</span> front and free-surface-velocity for more than 650 substances. This is still a useful tool for the <span class="hlt">shock</span>-wave community, but it has a number of serious disadvantages which can't be easily eliminated: (i) very simple data format for points and references; (ii) minimalistic user interface for data addition; (iii) absence of history of changes; (iv) bad feedback from users. The new International <span class="hlt">Shock</span>-Wave database (ISWdb) is intended to solve these and some other problems. The ISWdb project objectives are: (i) to develop a database on thermodynamic and mechanical properties of materials under conditions of <span class="hlt">shock</span>-wave and other dynamic loadings, selected related quantities of interest, and the meta-data that describes the provenance of the measurements and material models; and (ii) to make this database available internationally through the Internet, in an interactive form. The development and operation of the ISWdb is guided by an advisory committee. The database will be installed on two mirrored web-servers, one in Russia and the other in USA (currently only one server is available). The database provides access to original experimental data on <span class="hlt">shock</span> <span class="hlt">compression</span>, non-<span class="hlt">shock</span> dynamic loadings, isentropic expansion, measurements of sound</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2011APS..MARJ31003B','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2011APS..MARJ31003B"><span>Transport of particulate matter from a <span class="hlt">shocked</span> interface</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Buttler, W. T.; Hammerberg, J. E.; Oro, D.; Morris, C.; Mariam, F.; Rousculp, C.</p> <p>2011-03-01</p> <p>We have performed a series of <span class="hlt">shock</span> experiments to measure the evolution and transport of micron and sub-micron Tungsten particles from a 40 micron thick layer deposited on an Aluminum substrate. Densities and velocity distributions were measured using proton radiography at the Los Alamos Neutron Science Center for vacuum conditions and with contained Argon and Xenon gas atmospheres at initial pressures of 9.5 bar and room temperature. A common <span class="hlt">shock</span> drive resulted in free surface velocities of 1.25 km/s. An analysis of the time dependence of Lithium Niobate piezo-electric pin pressure profiles is given in terms of solutions to the particulate drag equations and the evolution equation for the particulate distribution function. The spatial and temporal fore-shortening in the <span class="hlt">shocked</span> gas can be accounted for using reasonable values for the <span class="hlt">compressed</span> gas shear viscosities and the vacuum distributions. The detailed form of the pin pressure data for Xenon indicates particulate breakup in the hot <span class="hlt">compressed</span> gas. This work supported by the U.S. Department of Energy under contract DE-AC52-06NA25396.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2011APS..SHK.U4002B','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2011APS..SHK.U4002B"><span>Transport of Particulate Matter from a <span class="hlt">Shocked</span> Interface</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Buttler, W. T.; Hammerberg, J. E.; Oro, D.; Mariam, F.; Rousculp, C.</p> <p>2011-06-01</p> <p>We have performed a series of <span class="hlt">shock</span> experiments to measure the evolution and transport of micron and sub-micron Tungsten particles from a 40 μm thick layer deposited on an Aluminum substrate. Densities and velocity distributions were measured using proton radiography at the Los Alamos Neutron Science Center for vacuum conditions and with contained Argon and Xenon gas atmospheres at initial pressures of 9.5 bar and room temperature. A common <span class="hlt">shock</span> drive resulted in free surface velocities of 1.25 km/s. An analysis of the time dependence of Lithium Niobate piezo-electric pin pressure profiles is given in terms of solutions to the particulate drag equations and the evolution equation for the particulate distribution function. The spatial and temporal fore-shortening in the <span class="hlt">shocked</span> gas can be accounted for using reasonable values for the <span class="hlt">compressed</span> gas shear viscosities and the vacuum distributions. The detailed form of the pin pressure data for Xenon indicates particulate breakup in the hot <span class="hlt">compressed</span> gas. This work supported by the U.S. Department of Energy under contract DE-AC52-06NA25396.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017AGUFMSH31B2734K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017AGUFMSH31B2734K"><span>Investigating the ability of solar coronal <span class="hlt">shocks</span> to accelerate solar energetic particles</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Kwon, R. Y.; Vourlidas, A.</p> <p>2017-12-01</p> <p>We estimate the density <span class="hlt">compression</span> ratio of <span class="hlt">shocks</span> associated with coronal mass ejections (CMEs) and investigate whether they can accelerate solar energetic particles (SEPs). Using remote-sensing, multi-viewpoint coronagraphic observations, we have developed a method to extract the sheath electron density profiles along the <span class="hlt">shock</span> normal and estimate the density <span class="hlt">compression</span> ratio. Our method uses the ellipsoid model to derive the 3D geometry of the sheaths, including the line-of-sight (LOS) depth. The sheath density profiles along the <span class="hlt">shock</span> normal are modeled with double-Gaussian functions, and the modeled densities are integrated along the LOSs to be compared with the observed brightness in STEREO COR2-Ahead. The upstream densities are derived from either the pB-inversion of the brightness in a pre-event image or an empirical model. We analyze two fast halo CMEs observed on 2011 March 7 and 2014 February 25 that are associated with SEP events detected by multiple spacecraft located over a broad range of heliolongitudes. We find that the density <span class="hlt">compression</span> peaks around the CME nose and decreases at larger position angles. Interestingly, we find that the supercritical region extends over a large area of the <span class="hlt">shock</span> and lasts longer (several tens of minutes) than past reports. This finding implies that CME <span class="hlt">shocks</span> may be capable of accelerating energetic particles in the corona over extended spatial and temporal scales and may, therefore, be responsible for the wide longitudinal distribution of these particles in the inner heliosphere.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015JGRA..120.2409L','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015JGRA..120.2409L"><span><span class="hlt">Shocks</span> inside CMEs: A survey of properties from 1997 to 2006</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Lugaz, N.; Farrugia, C. J.; Smith, C. W.; Paulson, K.</p> <p>2015-04-01</p> <p>We report on 49 fast-mode forward <span class="hlt">shocks</span> propagating inside coronal mass ejections (CMEs) as measured by Wind and ACE at 1 AU from 1997 to 2006. Compared to typical CME-driven <span class="hlt">shocks</span>, these <span class="hlt">shocks</span> propagate in different upstream conditions, where the median upstream Alfvén speed is 85 km s-1, the proton β = 0.08 and the magnetic field strength is 8 nT. These <span class="hlt">shocks</span> are fast with a median speed of 590 km s-1 but weak with a median Alfvénic Mach number of 1.9. They typically <span class="hlt">compress</span> the magnetic field and density by a factor of 2-3. The most extreme upstream conditions found were a fast magnetosonic speed of 230 km s-1, a plasma β of 0.02, upstream solar wind speed of 740 km s-1 and density of 0.5 cm-3. Nineteen of these complex events were associated with an intense geomagnetic storm (peak Dst under -100 nT) within 12 h of the <span class="hlt">shock</span> detection at Wind, and 15 were associated with a drop of the storm time Dst index of more than 50 nT between 3 and 9 h after <span class="hlt">shock</span> detection. We also compare them to a sample of 45 <span class="hlt">shocks</span> propagating in more typical upstream conditions. We show the average property of these <span class="hlt">shocks</span> through a superposed epoch analysis, and we present some analytical considerations regarding the <span class="hlt">compression</span> ratios of <span class="hlt">shocks</span> in low β regimes. As most of these <span class="hlt">shocks</span> are measured in the back half of a CME, we conclude that about half the <span class="hlt">shocks</span> may not remain fast-mode <span class="hlt">shocks</span> as they propagate through an entire CME due to the large upstream and magnetosonic speeds.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19890052291&hterms=Glasses+SiO2&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D30%26Ntt%3DGlasses%2BSiO2','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19890052291&hterms=Glasses+SiO2&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D30%26Ntt%3DGlasses%2BSiO2"><span><span class="hlt">Shock</span> temperatures in silica glass - Implications for modes of <span class="hlt">shock</span>-induced deformation, phase transformation, and melting with pressure</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Schmitt, Douglas R.; Ahrens, Thomas J.</p> <p>1989-01-01</p> <p>Observations of <span class="hlt">shock</span>-induced radiative thermal emissions are used to determine the gray body temperatures and emittances of silica glass under <span class="hlt">shock</span> <span class="hlt">compression</span> between 10 and 30 GPa. The results suggest that fused quartz deforms heterogeneously in this <span class="hlt">shock</span> pressure range. It is shown that the 10-16 GPa range coincides with the permanent densification region, while the 16-30 GPa range coincides with the inferred mixed phase region along the silica glass Hugoniot. Low emittances in the mixed phase region are thought to represent the melting temperature of the high-pressure phase, stishovite. Also, consideration is given to the effects of pressure on melting relations for the system SiO2-Mg2SiO4.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015AGUFMDI33A2625T','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015AGUFMDI33A2625T"><span><span class="hlt">Compression</span> behavior of Fe-Si-H alloys</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Tagawa, S.; Ohta, K.; Hirose, K.; Ohishi, Y.</p> <p>2015-12-01</p> <p>Although the light elements in the Earth's core are still enigmatic, hydrogen has recently been receiving much attention. Planetary formation theory suggested that a large amount of water, much more than is in the oceans, could have been brought to the Earth during its accretion. Hydrogen is a strong siderophile element and could be incorporated into the core as a consequence of a reaction between water and molten <span class="hlt">iron</span> in a magma ocean [Okuchi, 1997 Science]. Nevertheless, the effect of hydrogen on the property of <span class="hlt">iron</span> is not well known so far. Here, we have experimentally examined the <span class="hlt">compression</span> behavior of hcp Fe0.88Si0.12Hx (6.5 wt.% Si) at two different hydrogen concentrations (x = 0.7 and 0.9). Fe0.88Si0.12 foil was loaded into a diamond-anvil cell, and then liquid hydrogen was introduced to a sample chamber below 20 K. Hydrogenation occurred upon thermal annealing below 1500 K at 25-62 GPa, and hcp Fe0.88Si0.12Hx was obtained as a single phase. Unlike the Fe-H alloy, hydrogen did not fully occupy the octahedral sites even under hydrogen-saturated conditions. Two <span class="hlt">compression</span> curves, one from 25 to 136 GPa, and the other from 62 to 128 GPa, were obtained at room temperature. While the effect of hydrogen on the <span class="hlt">compressibility</span> of <span class="hlt">iron</span> has been controversial in earlier experimental studies [Hirao et al., 2004 GRL; Pépin et al., 2014 PRL], our data indicate that the <span class="hlt">compressibility</span> of Fe0.88Si0.12Hx alloy does not change with changing hydrogen content from x = 0 to 0.9. Such <span class="hlt">compression</span> behavior observed is consistent with the recent ab initio calculations for hcp Fe-H alloys by Caracas[2015 GRL]. The extrapolation of present data to the outer core pressure and temperature range, assuming thermal expansivity is the same as that for <span class="hlt">iron</span> and there is no density difference between solid and liquid, shows that the density of Fe0.88Si0.12H0.3 matches the PREM in the whole outer core within 1%.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016PhyA..463..123M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016PhyA..463..123M"><span>Molecular dynamics study of strain-induced diffusivity of nitrogen in pure <span class="hlt">iron</span> nanocrystalline</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Mohammadzadeh, Roghayeh; Razmara, Naiyer; Razmara, Fereshteh</p> <p>2016-12-01</p> <p>In the present study, the self-diffusion process of nitrogen in pure <span class="hlt">iron</span> nanocrystalline under strain conditions has been investigated by Molecular Dynamics (MD). The interactions between particles are modeled using Modified Embedded Atom Method (MEAM). Mean Square Displacement (MSD) of nitrogen in <span class="hlt">iron</span> structure under strain is calculated. Strain is applied along [ 11 2 ¯ 0 ] and [ 0001 ] directions in both tensile and <span class="hlt">compression</span> conditions. The activation energy and pre-exponential diffusion factor for nitrogen diffusion is comparatively high along [ 0001 ] direction of <span class="hlt">compressed</span> structure of <span class="hlt">iron</span>. The strain-induced diffusion coefficient at 973 K under the <span class="hlt">compression</span> rate of 0.001 Å/ps along [ 0001 ] direction is about 6.72E-14 m2/s. The estimated activation energy of nitrogen under <span class="hlt">compression</span> along [ 0001 ] direction is equal to 12.39 kcal/mol. The higher activation energy might be due to the fact that the system transforms into a more dense state when <span class="hlt">compressive</span> stress is applied.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20060008908','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20060008908"><span>User Guide for <span class="hlt">Compressible</span> Flow Toolbox Version 2.1 for Use With MATLAB(Registered Trademark); Version 7</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Melcher, Kevin J.</p> <p>2006-01-01</p> <p>This report provides a user guide for the <span class="hlt">Compressible</span> Flow Toolbox, a collection of algorithms that solve almost 300 linear and nonlinear classical <span class="hlt">compressible</span> flow relations. The algorithms, implemented in the popular MATLAB programming language, are useful for analysis of one-dimensional steady flow with constant entropy, friction, heat transfer, or <span class="hlt">shock</span> discontinuities. The solutions do not include any gas dissociative effects. The toolbox also contains functions for comparing and validating the equation-solving algorithms against solutions previously published in the open literature. The classical equations solved by the <span class="hlt">Compressible</span> Flow Toolbox are: isentropic-flow equations, Fanno flow equations (pertaining to flow of an ideal gas in a pipe with friction), Rayleigh flow equations (pertaining to frictionless flow of an ideal gas, with heat transfer, in a pipe of constant cross section.), normal-<span class="hlt">shock</span> equations, oblique-<span class="hlt">shock</span> equations, and Prandtl-Meyer expansion equations. At the time this report was published, the <span class="hlt">Compressible</span> Flow Toolbox was available without cost from the NASA Software Repository.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19920034412&hterms=jump&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D50%26Ntt%3Djump','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19920034412&hterms=jump&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D50%26Ntt%3Djump"><span>Electrostatic potential jump across fast-mode collisionless <span class="hlt">shocks</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Mandt, M. E.; Kan, J. R.</p> <p>1991-01-01</p> <p>The electrostatic potential jump across fast-mode collisionless <span class="hlt">shocks</span> is examined by comparing published observations, hybrid simulations, and a simple model, in order to better characterize its dependence on the various <span class="hlt">shock</span> parameters. In all three, it is assumed that the electrons can be described by an isotropic power-law equation of state. The observations show that the cross-<span class="hlt">shock</span> potential jump correlates well with the <span class="hlt">shock</span> strength but shows very little correlation with other <span class="hlt">shock</span> parameters. Assuming that the electrons obey an isotropic power law equation of state, the correlation of the potential jump with the <span class="hlt">shock</span> strength follows naturally from the increased <span class="hlt">shock</span> <span class="hlt">compression</span> and an apparent dependence of the power law exponent on the Mach number which the observations indicate. It is found that including a Mach number dependence for the power law exponent in the electron equation of state in the simple model produces a potential jump which better fits the observations. On the basis of the simulation results and theoretical estimates of the cross-<span class="hlt">shock</span> potential, it is discussed how the cross-<span class="hlt">shock</span> potential might be expected to depend on the other <span class="hlt">shock</span> parameters.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2012JPlPh..78..295H','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2012JPlPh..78..295H"><span>Nonlinear waves and <span class="hlt">shocks</span> in relativistic two-fluid hydrodynamics</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Haim, L.; Gedalin, M.; Spitkovsky, A.; Krasnoselskikh, V.; Balikhin, M.</p> <p>2012-06-01</p> <p>Relativistic <span class="hlt">shocks</span> are present in a number of objects where violent processes are accompanied by relativistic outflows of plasma. The magnetization parameter σ = B2/4πnmc2 of the ambient medium varies in wide range. <span class="hlt">Shocks</span> with low σ are expected to substantially enhance the magnetic fields in the <span class="hlt">shock</span> front. In non-relativistic <span class="hlt">shocks</span> the magnetic <span class="hlt">compression</span> is limited by nonlinear effects related to the deceleration of flow. Two-fluid analysis of perpendicular relativistic <span class="hlt">shocks</span> shows that the nonlinearities are suppressed for σ<<1 and the magnetic field reaches nearly equipartition values when the magnetic energy density is of the order of the ion energy density, Beq2 ~ 4πnmic2γ. A large cross-<span class="hlt">shock</span> potential eφ/mic2γ0 ~ B2/Beq2 develops across the electron-ion <span class="hlt">shock</span> front. This potential is responsible for electron energization.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015JSV...349..177B','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015JSV...349..177B"><span>A <span class="hlt">shock</span> absorber model for structure-borne noise analyses</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Benaziz, Marouane; Nacivet, Samuel; Thouverez, Fabrice</p> <p>2015-08-01</p> <p><span class="hlt">Shock</span> absorbers are often responsible for undesirable structure-borne noise in cars. The early numerical prediction of this noise in the automobile development process can save time and money and yet remains a challenge for industry. In this paper, a new approach to predicting <span class="hlt">shock</span> absorber structure-borne noise is proposed; it consists in modelling the <span class="hlt">shock</span> absorber and including the main nonlinear phenomena responsible for discontinuities in the response. The model set forth herein features: <span class="hlt">compressible</span> fluid behaviour, nonlinear flow rate-pressure relations, valve mechanical equations and rubber mounts. The piston, base valve and complete <span class="hlt">shock</span> absorber model are compared with experimental results. Sensitivity of the <span class="hlt">shock</span> absorber response is evaluated and the most important parameters are classified. The response envelope is also computed. This <span class="hlt">shock</span> absorber model is able to accurately reproduce local nonlinear phenomena and improves our state of knowledge on potential noise sources within the <span class="hlt">shock</span> absorber.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018ApJ...856...33K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018ApJ...856...33K"><span>Effects of Alfvénic Drift on Diffusive <span class="hlt">Shock</span> Acceleration at Weak Cluster <span class="hlt">Shocks</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Kang, Hyesung; Ryu, Dongsu</p> <p>2018-03-01</p> <p>Non-detection of γ-ray emission from galaxy clusters has challenged diffusive <span class="hlt">shock</span> acceleration (DSA) of cosmic-ray (CR) protons at weak collisionless <span class="hlt">shocks</span> that are expected to form in the intracluster medium. As an effort to address this problem, we here explore possible roles of Alfvén waves self-excited via resonant streaming instability during the CR acceleration at parallel <span class="hlt">shocks</span>. The mean drift of Alfvén waves may either increase or decrease the scattering center <span class="hlt">compression</span> ratio, depending on the postshock cross-helicity, leading to either flatter or steeper CR spectra. We first examine such effects at planar <span class="hlt">shocks</span>, based on the transport of Alfvén waves in the small amplitude limit. For the <span class="hlt">shock</span> parameters relevant to cluster <span class="hlt">shocks</span>, Alfvénic drift flattens the CR spectrum slightly, resulting in a small increase of the CR acceleration efficiency, η. We then consider two additional, physically motivated cases: (1) postshock waves are isotropized via MHD and plasma processes across the <span class="hlt">shock</span> transition, and (2) postshock waves contain only forward waves propagating along with the flow due to a possible gradient of CR pressure behind the <span class="hlt">shock</span>. In these cases, Alfvénic drift could reduce η by as much as a factor of five for weak cluster <span class="hlt">shocks</span>. For the canonical parameters adopted here, we suggest η ∼ 10‑4–10‑2 for <span class="hlt">shocks</span> with sonic Mach number M s ≈ 2–3. The possible reduction of η may help ease the tension between non-detection of γ-rays from galaxy clusters and DSA predictions.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2013APS..SHK.W5001K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2013APS..SHK.W5001K"><span>Probing planetary interiors: <span class="hlt">Shock</span> <span class="hlt">compression</span> of water to 700 GPa and 3.8 g/cc, and recent high precision Hugoniot measurements of deuterium</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Knudson, Marcus</p> <p>2013-06-01</p> <p>The past several years have seen tremendous increase in the number of identified extra-solar planetary systems. Our understanding of the formation of these systems is tied to our understanding of the internal structure of these exoplanets, which in turn rely upon equations of state of light elements and compounds such as water and hydrogen. Here we present <span class="hlt">shock</span> <span class="hlt">compression</span> data for water with unprecedented accuracy that shows commonly used models for water in planetary modeling significantly overestimate the <span class="hlt">compressibility</span> at conditions relevant to planetary interiors. Furthermore, we show that its behavior at these conditions, including reflectivity and isentropic response, is well described by a recent first-principles based equation of state. These findings advocate the use of this model as the standard for modeling Neptune, Uranus, and ``hot Neptune'' exoplanets, and should contribute to improved understanding of the interior structure of these planets, and perhaps improved understanding of formation mechanisms of planetary systems. We also present very recent experiments on deuterium that have taken advantage of continued improvements in both experimental configuration and the understanding of the quartz <span class="hlt">shock</span> standard to obtain Hugoniot data with a significant increase in precision. These data will prove to provide a stringent test for the equation of state of hydrogen and its isotopes. Sandia is a multiprogram laboratory managed and operated by Sandia Corporation, a wholly owned subsidiary of Lockheed Martin Company, for the US Department of Energy's National Nuclear Security Administration under Contract No. DE-ACO4-94AL85000.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018JDBM....4..231S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018JDBM....4..231S"><span><span class="hlt">Shock</span> Response of Lightweight Adobe Masonry</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Sauer, C.; Bagusat, F.; Heine, A.; Riedel, W.</p> <p>2018-06-01</p> <p>The behavior of a low density and low-strength building material under <span class="hlt">shock</span> loading is investigated. The considered material is lightweight adobe masonry characterized by a density of 1.2 g/cm3 and a quasi-static uniaxial <span class="hlt">compressive</span> strength of 2.8 MPa. Planar-plate-impact (PPI) tests with velocities in between 295 and 950 m/s are performed in order to obtain Hugoniot data and to derive parameters for an equation of state (EOS) that captures the occurring phenomenology of porous compaction and subsequent unloading. The resulting EOS description is validated by comparing the experimental free surface velocity time curves with those obtained by numerical simulations of the performed PPI tests. The non-linear <span class="hlt">compression</span> behavior, including the pore compaction mechanism, constitutes a main ingredient for modelling the response of adobe to blast and high-velocity impact loading. We hence present a modeling approach for lightweight adobe which can be applied to such high rate loading scenarios in future studies. In general, this work shows that PPI tests on lightweight and low-strength geological materials can be used to extract Hugoniot data despite significant material inhomogeneity. Furthermore, we demonstrate that a homogenous material model is able to numerically describe such a material under <span class="hlt">shock</span> <span class="hlt">compression</span> and release with a reasonable accuracy.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018JBDM..tmp...19S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018JBDM..tmp...19S"><span><span class="hlt">Shock</span> Response of Lightweight Adobe Masonry</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Sauer, C.; Bagusat, F.; Heine, A.; Riedel, W.</p> <p>2018-04-01</p> <p>The behavior of a low density and low-strength building material under <span class="hlt">shock</span> loading is investigated. The considered material is lightweight adobe masonry characterized by a density of 1.2 g/cm3 and a quasi-static uniaxial <span class="hlt">compressive</span> strength of 2.8 MPa. Planar-plate-impact (PPI) tests with velocities in between 295 and 950 m/s are performed in order to obtain Hugoniot data and to derive parameters for an equation of state (EOS) that captures the occurring phenomenology of porous compaction and subsequent unloading. The resulting EOS description is validated by comparing the experimental free surface velocity time curves with those obtained by numerical simulations of the performed PPI tests. The non-linear <span class="hlt">compression</span> behavior, including the pore compaction mechanism, constitutes a main ingredient for modelling the response of adobe to blast and high-velocity impact loading. We hence present a modeling approach for lightweight adobe which can be applied to such high rate loading scenarios in future studies. In general, this work shows that PPI tests on lightweight and low-strength geological materials can be used to extract Hugoniot data despite significant material inhomogeneity. Furthermore, we demonstrate that a homogenous material model is able to numerically describe such a material under <span class="hlt">shock</span> <span class="hlt">compression</span> and release with a reasonable accuracy.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/873833','DOE-PATENT-XML'); return false;" href="https://www.osti.gov/servlets/purl/873833"><span><span class="hlt">Compressed</span> gas fuel storage system</span></a></p> <p><a target="_blank" href="http://www.osti.gov/doepatents">DOEpatents</a></p> <p>Wozniak, John J.; Tiller, Dale B.; Wienhold, Paul D.; Hildebrand, Richard J.</p> <p>2001-01-01</p> <p>A <span class="hlt">compressed</span> gas vehicle fuel storage system comprised of a plurality of <span class="hlt">compressed</span> gas pressure cells supported by <span class="hlt">shock</span>-absorbing foam positioned within a shape-conforming container. The container is dimensioned relative to the <span class="hlt">compressed</span> gas pressure cells whereby a radial air gap surrounds each <span class="hlt">compressed</span> gas pressure cell. The radial air gap allows pressure-induced expansion of the pressure cells without resulting in the application of pressure to adjacent pressure cells or physical pressure to the container. The pressure cells are interconnected by a gas control assembly including a thermally activated pressure relief device, a manual safety shut-off valve, and means for connecting the fuel storage system to a vehicle power source and a refueling adapter. The gas control assembly is enclosed by a protective cover attached to the container. The system is attached to the vehicle with straps to enable the chassis to deform as intended in a high-speed collision.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2012EPJWC..2601026C','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2012EPJWC..2601026C"><span>Polymorphic transition of tin under <span class="hlt">shock</span> wave <span class="hlt">compression</span>: Experimental results</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Chauvin, C.; Petit, J.; Sinatti, F.</p> <p>2012-08-01</p> <p>In this work, the β-bct polymorphic transition in tin is investigated by means of plate impact experiments. The Sn target surface is observed in a partially released state obtained thanks to a transparent lithium fluoride (LiF) anvil. We report both measurements of interface velocity and temperature obtained using Photon Doppler Velocimetry and IR optical pyrometer on <span class="hlt">shock</span>-loaded tin from 8 to 16 GPa. We show that the Mabire Model EOS associated to the SCG plasticity model provides an overall good estimate of the velocity profiles. However, depnding on the <span class="hlt">shock</span> amplitude, its prediction of the temperature profile may be less satisfactory, hence underlining the need for future improvements in terms of phase transition kinetics description.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_17");'>17</a></li> <li><a href="#" onclick='return showDiv("page_18");'>18</a></li> <li class="active"><span>19</span></li> <li><a href="#" onclick='return showDiv("page_20");'>20</a></li> <li><a href="#" onclick='return showDiv("page_21");'>21</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_19 --> <div id="page_20" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_18");'>18</a></li> <li><a href="#" onclick='return showDiv("page_19");'>19</a></li> <li class="active"><span>20</span></li> <li><a href="#" onclick='return showDiv("page_21");'>21</a></li> <li><a href="#" onclick='return showDiv("page_22");'>22</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="381"> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018ShWav.tmp....3B','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018ShWav.tmp....3B"><span>Evolution of scalar and velocity dynamics in planar <span class="hlt">shock</span>-turbulence interaction</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Boukharfane, R.; Bouali, Z.; Mura, A.</p> <p>2018-01-01</p> <p>Due to the short residence time of air in supersonic combustors, achieving efficient mixing in <span class="hlt">compressible</span> turbulent reactive flows is crucial for the design of supersonic ramjet (Scramjet) engines. In this respect, improving the understanding of <span class="hlt">shock</span>-scalar mixing interactions is of fundamental importance for such supersonic combustion applications. In these <span class="hlt">compressible</span> flows, the interaction between the turbulence and the <span class="hlt">shock</span> wave is reciprocal, and the coupling between them is very strong. A basic understanding of the physics of such complex interactions has already been obtained through the analysis of relevant simplified flow configurations, including propagation of the <span class="hlt">shock</span> wave in density-stratified media, <span class="hlt">shock</span>-wave-mixing-layer interaction, and <span class="hlt">shock</span>-wave-vortex interaction. Amplification of velocity fluctuations and substantial changes in turbulence characteristic length scales are the most well-known outcomes of <span class="hlt">shock</span>-turbulence interaction, which may also deeply influence scalar mixing between fuel and oxidizer. The effects of the <span class="hlt">shock</span> wave on the turbulence have been widely characterized through the use of so-called amplification factors, and similar quantities are introduced herein to characterize the influence of the <span class="hlt">shock</span> wave on scalar mixing. One of the primary goals of the present study is indeed to extend previous analyses to the case of <span class="hlt">shock</span>-scalar mixing interaction, which is directly relevant to supersonic combustion applications. It is expected that the <span class="hlt">shock</span> wave will affect the scalar dissipation rate (SDR) dynamics. Special emphasis is placed on the modification of the so-called turbulence-scalar interaction as a leading-order contribution to the production of mean SDR, i.e., a quantity that defines the mixing rate and efficiency. To the best of the authors' knowledge, this issue has never been addressed in detail in the literature, and the objective of the present study is to scrutinize this influence. The turbulent mixing of a</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2011APS..SHK.F1041C','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2011APS..SHK.F1041C"><span>Index of Refraction Measurements and Window Corrections for PMMA under <span class="hlt">Shock</span> <span class="hlt">Compression</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Chapman, David; Eakins, Daniel; Williamson, David; Proud, William</p> <p>2011-06-01</p> <p>Symmetric plate impact experiments were performed to investigate the change in the refractive index of PMMA under <span class="hlt">shock</span> loading. Flyer and target geometries allowed the measurement of <span class="hlt">shock</span> velocity, particle velocity, and refractive index in the <span class="hlt">shocked</span> state, using the simultaneous application of VISAR (532 nm) and Het-V (1550 nm). The change in refractive index of PMMA as a function of density is generally considered to be well described by the Gladstone-Dale relationship, meaning that the ``apparent'' velocity measured by a laser velocity interferometer is the ``true'' velocity, and hence there is no window correction. The results presented characterise the accuracy of this assumption at peak stresses up to 2 GPa.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/22275518-molecular-dynamics-simulation-shock-induced-ejection-fused-silica-surface','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/22275518-molecular-dynamics-simulation-shock-induced-ejection-fused-silica-surface"><span>Molecular dynamics simulation of <span class="hlt">shock</span> induced ejection on fused silica surface</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Su, Rui; Xiang, Meizhen; Jiang, Shengli</p> <p>2014-05-21</p> <p><span class="hlt">Shock</span> response and surface ejection behaviors of fused silica are studied by using non-equilibrium molecular dynamics combining with the Tersoff potential. First, bulk structure and Hugoniot curves of fused silica are calculated and compared with experimental results. Then, the dynamical process of surface ejection behavior is simulated under different loading velocities ranging from 3.5 to 5.0 km∕s, corresponding to <span class="hlt">shock</span> wave velocities from 7.1 to 8.8 km∕s. The local atomistic shear strain parameter is used to describe the local plastic deformation under conditions of <span class="hlt">shock</span> <span class="hlt">compression</span> or releasing. Our result shows that the shear strain is localized in the bottom area ofmore » groove under the <span class="hlt">shock</span> <span class="hlt">compression</span>. Surface ejection is observed when the loading velocity exceeds 4.0 km∕s. Meanwhile, the temperature of the micro-jet is ∼5574.7 K, which is close to experiment measurement. Several kinds of structural defects including non-bridging oxygen are found in the bulk area of the sample after ejection.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/1326076','SCIGOV-STC'); return false;" href="https://www.osti.gov/servlets/purl/1326076"><span>Transient <span class="hlt">shocks</span> beyond the heliopause</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Fermo, R. L.; Pogorelov, N. V.; Burlaga, L. F.</p> <p></p> <p>The heliopause is a rich, dynamic surface affected by the time-dependent solar wind. Stream interactions due to coronal mass ejections (CMEs), corotating interaction regions (CIRs), and other transient phenomena are known to merge producing global merged interaction regions (GMIRs). Numerical simulations of the solar wind interaction with the local interstellar medium (LISM) show that GMIRs, as well other time-dependent structures in the solar wind, may produce <span class="hlt">compression</span>/rarefaction waves and <span class="hlt">shocks</span> in the LISM behind the heliopause. These <span class="hlt">shocks</span> may initiate wave activity observed by the Voyager spacecraft. The magnetometer onboard Voyager 1 indeed observed a few structures that may bemore » interpreted as <span class="hlt">shocks</span>. We present numerical simulations of such <span class="hlt">shocks</span> in the year of 2000, when both Voyager spacecraft were in the supersonic solar wind region, and in 2012, when Voyager 1 observed traveling <span class="hlt">shocks</span>. In the former case, Voyager observations themselves provide time- dependent boundary conditions in the solar wind. In the latter case, we use OMNI data at 1 AU to analyze the plasma and magnetic field behavior after Voyager 1 crossed the heliospheric boundary. Numerical results are compared with spacecraft observations.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1326076-transient-shocks-beyond-heliopause','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1326076-transient-shocks-beyond-heliopause"><span>Transient <span class="hlt">shocks</span> beyond the heliopause</span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>Fermo, R. L.; Pogorelov, N. V.; Burlaga, L. F.</p> <p>2015-09-30</p> <p>The heliopause is a rich, dynamic surface affected by the time-dependent solar wind. Stream interactions due to coronal mass ejections (CMEs), corotating interaction regions (CIRs), and other transient phenomena are known to merge producing global merged interaction regions (GMIRs). Numerical simulations of the solar wind interaction with the local interstellar medium (LISM) show that GMIRs, as well other time-dependent structures in the solar wind, may produce <span class="hlt">compression</span>/rarefaction waves and <span class="hlt">shocks</span> in the LISM behind the heliopause. These <span class="hlt">shocks</span> may initiate wave activity observed by the Voyager spacecraft. The magnetometer onboard Voyager 1 indeed observed a few structures that may bemore » interpreted as <span class="hlt">shocks</span>. We present numerical simulations of such <span class="hlt">shocks</span> in the year of 2000, when both Voyager spacecraft were in the supersonic solar wind region, and in 2012, when Voyager 1 observed traveling <span class="hlt">shocks</span>. In the former case, Voyager observations themselves provide time- dependent boundary conditions in the solar wind. In the latter case, we use OMNI data at 1 AU to analyze the plasma and magnetic field behavior after Voyager 1 crossed the heliospheric boundary. Numerical results are compared with spacecraft observations.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017APS..SHK.L8002C','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017APS..SHK.L8002C"><span>Modeling the <span class="hlt">Shock</span> Hugoniot in Porous Materials</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Cochrane, Kyle R.; Shulenburger, Luke; Mattsson, Thomas R.; Lane, J. Matthew D.; Weck, Philippe F.; Vogler, Tracy J.; Desjarlais, Michael P.</p> <p>2017-06-01</p> <p>Porous materials are present in many scenarios from planetary science to ICF. Understanding how porosity modifies the behavior of the <span class="hlt">shock</span> Hugoniot in an equation of state is key to being able to predictively simulate experiments. For example, modeling <span class="hlt">shocks</span> in under-dense <span class="hlt">iron</span> oxide can aid in understanding planetary formation and silica aerogel can be used to approximate the <span class="hlt">shock</span> response of deuterium. Simulating the <span class="hlt">shock</span> response of porous materials presents a variety of theoretical challenges, but by combining ab initio calculations with a surface energy and porosity model, we are able to accurately represent the <span class="hlt">shock</span> Hugoniot. Finally, we show that this new approach can be used to calculate the Hugoniot of porous materials using existing tabular equations of state. Sandia National Laboratories is a multi-mission laboratory managed and operated by Sandia Corporation, a wholly owned subsidiary of Lockheed Martin Corporation, for the U.S. Department of Energy's National Nuclear Security Administration under contract DE-AC04-94AL85000.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/1998AIPC..429..819F','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/1998AIPC..429..819F"><span>Picosecond vibrational spectroscopy of <span class="hlt">shocked</span> energetic materials</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Franken, Jens; Hambir, Selezion A.; Dlott, Dana D.</p> <p>1998-07-01</p> <p>The dynamic response of a thin film of the insensitive high explosive 5-nitro-2,4-dihydro-3H-1,2,4-triazol-3-one (NTO) to ultrafast <span class="hlt">shock</span> <span class="hlt">compression</span> has been investigated by picosecond coherent anti-Stokes Raman spectroscopy (CARS). Vibrational spectra were obtained in the 1200 cm-1 to 1450 cm-1 region with a time resolution on the order of 100 ps. The frequency shifts and widths of the two vibrational transitions in this region show an entirely different behavior when subjected to a <span class="hlt">shock</span> load of about 5 GPa. An additional weak band at 1293 cm-1 appears temporarily while the <span class="hlt">shock</span> front is within the NTO layer.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/19624226','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/19624226"><span><span class="hlt">Shock</span>-induced transformations in crystalline RDX: a uniaxial constant-stress Hugoniostat molecular dynamics simulation study.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Bedrov, Dmitry; Hooper, Justin B; Smith, Grant D; Sewell, Thomas D</p> <p>2009-07-21</p> <p>Molecular dynamics (MD) simulations of uniaxial <span class="hlt">shock</span> <span class="hlt">compression</span> along the [100] and [001] directions in the alpha polymorph of hexahydro-1,3,5-trinitro-1,3,5-triazine (alpha-RDX) have been conducted over a wide range of <span class="hlt">shock</span> pressures using the uniaxial constant stress Hugoniostat method [Ravelo et al., Phys. Rev. B 70, 014103 (2004)]. We demonstrate that the Hugoniostat method is suitable for studying <span class="hlt">shock</span> <span class="hlt">compression</span> in atomic-scale models of energetic materials without the necessity to consider the extremely large simulation cells required for an explicit <span class="hlt">shock</span> wave simulation. Specifically, direct comparison of results obtained using the Hugoniostat approach to those reported by Thompson and co-workers [Phys. Rev. B 78, 014107 (2008)] based on large-scale MD simulations of <span class="hlt">shocks</span> using the <span class="hlt">shock</span> front absorbing boundary condition (SFABC) approach indicates that Hugoniostat simulations of systems containing several thousand molecules reproduced the salient features observed in the SFABC simulations involving roughly a quarter-million molecules, namely, nucleation and growth of nanoscale shear bands for <span class="hlt">shocks</span> propagating along the [100] direction and the polymorphic alpha-gamma phase transition for <span class="hlt">shocks</span> directed along the [001] direction. The Hugoniostat simulations yielded predictions of the Hugoniot elastic limit for the [100] <span class="hlt">shock</span> direction consistent with SFABC simulation results.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/27078450','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/27078450"><span><span class="hlt">Shock</span> waves: The Maxwell-Cattaneo case.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Uribe, F J</p> <p>2016-03-01</p> <p>Several continuum theories for <span class="hlt">shock</span> waves give rise to a set of differential equations in which the analysis of the underlying vector field can be done using the tools of the theory of dynamical systems. We illustrate the importance of the divergences associated with the vector field by considering the ideas by Maxwell and Cattaneo and apply them to study <span class="hlt">shock</span> waves in dilute gases. By comparing the predictions of the Maxwell-Cattaneo equations with <span class="hlt">shock</span> wave experiments we are lead to the following conclusions: (a) For low <span class="hlt">compressions</span> (low Mach numbers: M) the results from the Maxwell-Cattaneo equations provide profiles that are in fair agreement with the experiments, (b) as the Mach number is increased we find a range of Mach numbers (1.27 ≈ M(1) < M < M(2) ≈ 1.90) such that numerical <span class="hlt">shock</span> wave solutions to the Maxwell-Cattaneo equations cannot be found, and (c) for greater Mach numbers (M>M_{2}) <span class="hlt">shock</span> wave solutions can be found though they differ significantly from experiments.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2015APS..SHK.P2001L','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2015APS..SHK.P2001L"><span>Modeling the <span class="hlt">Shock</span> Ignition of a Copper Oxide Aluminum Thermite</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Lee, Kibaek; Stewart, D. Scott; Clemenson, Michael; Glumac, Nick; Murzyn, Christopher</p> <p>2015-06-01</p> <p>An experimental ``striker confinement'' <span class="hlt">shock</span> <span class="hlt">compression</span> test was developed in the Glumac-group at the University of Illinois to study ignition and reaction in composite reactive materials. These include thermitic and intermetallic reactive powders. The test places a sample of materials such as a thermite mixture of copper oxide and aluminum powders that are initially <span class="hlt">compressed</span> to about 80 percent full density. Two RP-80 detonators simultaneously push steel bars into reactive material and the resulting <span class="hlt">compression</span> causes <span class="hlt">shock</span> compaction of the material and rapid heating. At that point one observes significant reaction and propagation of fronts. But the fronts are peculiar in that they are comprised of reactive events that can be traced to the reaction/diffusion of the initially separated reactants of copper oxide and aluminum that react at their mutual interfaces that nominally make copper liquid and aluminum oxide products. We discuss our model of the <span class="hlt">shock</span> ignition of the copper oxide aluminum thermite in the context of the striker experiment and how a Gibbs formulation model, that includes multi-components for liquid and solid phases of aluminum, copper oxide, copper and aluminum oxide can predict the events observed at the particle scale in the experiments. Supported by HDTRA1-10-1-0020 (DTRA), N000014-12-1-0555 (ONR).</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://images.nasa.gov/#/details-PIA20062.html','SCIGOVIMAGE-NASA'); return false;" href="https://images.nasa.gov/#/details-PIA20062.html"><span>Bow <span class="hlt">Shocks</span> in Space</span></a></p> <p><a target="_blank" href="https://images.nasa.gov/">NASA Image and Video Library</a></p> <p></p> <p>2016-01-05</p> <p>Bow <span class="hlt">shocks</span> thought to mark the paths of massive, speeding stars are highlighted in these images from NASA's Spitzer Space Telescope and Wide-field Infrared Survey Explorer, or WISE. Cosmic bow <span class="hlt">shocks</span> occur when massive stars zip through space, pushing material ahead of them in the same way that water piles up in front of a race boat. The stars also produce high-speed winds that smack into this <span class="hlt">compressed</span> material. The end result is pile-up of heated material that glows in infrared light. In these images, infrared light has been assigned the colored red. Green shows wispy dust in the region and blue shows stars. The two images at left are from Spitzer, and the one on the right is from WISE. The speeding stars thought to be creating the bow <span class="hlt">shocks</span> can be seen at the center of each arc-shaped feature. The image at right actually consists of two bow <span class="hlt">shocks</span> and two speeding stars. All the speeding stars are massive, ranging from about 8 to 30 times the mass of our sun. http://photojournal.jpl.nasa.gov/catalog/PIA20062</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=20020041016&hterms=theoretical+physics&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D50%26Ntt%3Dtheoretical%2Bphysics','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=20020041016&hterms=theoretical+physics&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D50%26Ntt%3Dtheoretical%2Bphysics"><span>The Physics of Molecular <span class="hlt">Shocks</span> in Star-Forming Regions</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Hollenbach, David; Cuzzi, Jeffrey (Technical Monitor)</p> <p>1996-01-01</p> <p>Molecular <span class="hlt">shocks</span> are produced by the impact of the supersonic infall of gas and dust onto protostars and by the interaction of the supersonic outflow from the protostar with the circumstellar material. Infalling gas creates an accretion <span class="hlt">shock</span> around the circumstellar disk which emits a unique infrared spectrum and which processes the interstellar dust as it enters the disk. The winds and jets from protostars also impact the disk, the infalling material, and the ambient molecular cloud core creating <span class="hlt">shocks</span> whose spectrum and morphology diagnose the mass loss processes of the protostar and the orientation and structure of the star forming system. We discuss the physics of these <span class="hlt">shocks</span>, the model spectra derived from theoretical models, and comparisons with observations of H2O masers, H2 emission, as well as other <span class="hlt">shocks</span> tracers. We show the strong effect of magnetic fields on molecular <span class="hlt">shock</span> structure, and elucidate the chemical changes induced by the <span class="hlt">shock</span> heating and <span class="hlt">compression</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2006AIPC..845..998P','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2006AIPC..845..998P"><span>Effect of <span class="hlt">Shock</span> Precompression on the Critical Diameter of Liquid Explosives</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Petel, Oren E.; Higgins, Andrew J.; Yoshinaka, Akio C.; Zhang, Fan</p> <p>2006-07-01</p> <p>The critical diameter of both ambient and <span class="hlt">shock</span>-precompressed liquid nitromethane confined in PVC tubing are measured experimentally. The experiment was conducted for both amine sensitized and neat NM. In the precompression experiments, the explosive is <span class="hlt">compressed</span> by a strong <span class="hlt">shock</span> wave generated by a donor explosive and reflected from a high impedance anvil prior to being detonated by a secondary event. The pressures reached in the test sections prior to detonation propagation was approximately 7 and 8 GPa for amine sensitized and neat NM respectively. The results demonstrated a 30% - 65% decrease in the critical diameter for the <span class="hlt">shock-compressed</span> explosives. This critical diameter decrease is observed despite a significant decrease in the predicted Von Neumann temperature of the detonation in the precompressed explosive. The results are discussed in the context of theoretical predictions based on thermal ignition theory and previous critical diameter measurements.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2011APS..DPPTI3004M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2011APS..DPPTI3004M"><span>Dynamic <span class="hlt">compression</span> of water to 700 GPa: single- and double <span class="hlt">shock</span> experiments on Sandia's Z machine, first principles simulations, and structure of water planets</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Mattsson, Thomas R.</p> <p>2011-11-01</p> <p>Significant progress has over the last few years been made in high energy density physics (HEDP) by executing high-precision multi-Mbar experiments and performing first-principles simulations for elements ranging from carbon [1] to xenon [2]. The properties of water under HEDP conditions are of particular importance in planetary science due to the existence of ice-giants like Neptune and Uranus. Modeling the two planets, as well as water-rich exoplanets, requires knowing the equation of state (EOS), the pressure as a function of density and temperature, of water with high accuracy. Although extensive density functional theory (DFT) simulations have been performed for water under planetary conditions [3] experimental validation has been lacking. Accessing thermodynamic states along planetary isentropes in dynamic <span class="hlt">compression</span> experiments is challenging because the principal Hugoniot follows a significantly different path in the phase diagram. In this talk, we present experimental data for dynamic <span class="hlt">compression</span> of water up to 700 GPa, including in a regime of the phase-diagram intersected by the Neptune isentrope and water-rich models for the exoplanet GJ436b. The data was obtained on the Z-accelerator at Sandia National Laboratories by performing magnetically accelerated flyer plate impact experiments measuring both the <span class="hlt">shock</span> and re-<span class="hlt">shock</span> in the sample. The high accuracy makes it possible for the data to be used for detailed model validation: the results validate first principles based thermodynamics as a reliable foundation for planetary modeling and confirm the fine effect of including nuclear quantum effects on the <span class="hlt">shock</span> pressure. Sandia National Laboratories is a multiprogram laboratory managed and operated by Sandia Corporation, a wholly owned subsidiary of Lockheed Martin Corporation, for the U.S. Department of Energy's National Nuclear Security Administration under Contract No. DE-AC04-94AL85000. [4pt] [1] M.D. Knudson, D.H. Dolan, and M.P. Desjarlais, SCIENCE</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/1997APS..SHK..H302F','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/1997APS..SHK..H302F"><span>Picosecond Vibrational Spectroscopy of <span class="hlt">Shocked</span> Energetic Materials</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Franken, Jens; Hare, David; Hambir, Selezion; Tas, Guray; Dlott, Dana</p> <p>1997-07-01</p> <p>We present a new technique which allows the study of the properties of <span class="hlt">shock</span> <span class="hlt">compressed</span> energetic materials via vibrational spectroscopy with a time resolution on the order of 25 ps. <span class="hlt">Shock</span> waves are generated using a near-IR laser at a repetition rate of 80 <span class="hlt">shocks</span> per second. <span class="hlt">Shock</span> pressures up to 5 GPa are obtained; <span class="hlt">shock</span> risetimes are as short as 25 ps. This technique enables us to estimate <span class="hlt">shock</span> pressures and temperatures as well as to monitor <span class="hlt">shock</span> induced chemistry. The <span class="hlt">shock</span> effects are probed by ps coherent anti-Stokes Raman spectroscopy (CARS). The sample consists of four layers, a glass plate, a thin polycrystalline layer of an energetic material, a buffer layer and the <span class="hlt">shock</span> generating layer. The latter is composed of a polymer, a near-IR absorbing dye and a high explosive (RDX) as a pressure booster. The main purpose of the buffer layer, which consists of an inert polymer, is to delay the arrival of the <span class="hlt">shock</span> wave at the sample by more than 1 ns until after the <span class="hlt">shock</span> generating layer has ablated away. High quality, high resolution (1 cm-1) low-background vibrational spectra could be obtained. So far this technique has been applied to rather insensitive high explosives such as TATB and NTO. In the upcoming months we are hoping to actually observe chemistry in real time by <span class="hlt">shocking</span> more sensitive materials. This work was supported by the NSF, the ARO and the AFOSR</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018MMTB..tmp..953P','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018MMTB..tmp..953P"><span>Effects of Powder Carrier on the Morphology and <span class="hlt">Compressive</span> Strength of <span class="hlt">Iron</span> Foams: Water vs Camphene</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Park, Hyeji; Um, Teakyung; Hong, Kicheol; Kang, Jin Soo; Nam, Ho-Seok; Kwon, Kyungjung; Sung, Yung-Eun; Choe, Heeman</p> <p>2018-06-01</p> <p>With its well-known popularity in structural applications, considerable attention has recently been paid to <span class="hlt">iron</span> (Fe) and its oxides for its promising functional applications such as biodegradable implants, water-splitting electrodes, and the anode of lithium-ion batteries. For these applications, <span class="hlt">iron</span> and its oxides can be even further utilized in the form of porous structures. In order to control the pore size, shape, and amount, we synthesized Fe foams using suspensions of micrometric Fe2O3 powder reduced to Fe via freeze casting in water or liquid camphene as a solvent through sublimation of either ice or camphene under 5 pct H2/Ar gas and sintering. We then compared them and found that the resulting Fe foam using water as a solvent (p = 71.7 pct) showed aligned lamellar macropores replicating ice dendrite colonies, while Fe foam using camphene as a solvent (p = 68.0 pct) exhibited interconnected equiaxed macropores replicating camphene dendrites. For all directions with respect to the loading axis, the <span class="hlt">compressive</span> behavior of the water-based Fe foam with a directional elongated wall pore structure was anisotropic (11.6 ± 0.9 MPa vs 7.8 ± 0.8 MPa), whereas that of the camphene-based Fe foam with a random round pore structure was nearly isotropic (12.0 ± 1.1 MPa vs 11.6 ± 0.4 MPa).</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017MSMSE..25f5016S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017MSMSE..25f5016S"><span>Dynamic response and residual stress fields of Ti6Al4V alloy under <span class="hlt">shock</span> wave induced by laser <span class="hlt">shock</span> peening</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Sun, Rujian; Li, Liuhe; Zhu, Ying; Zhang, Lixin; Guo, Wei; Peng, Peng; Li, Bo; Guo, Chao; Liu, Lei; Che, Zhigang; Li, Weidong; Sun, Jianfei; Qiao, Hongchao</p> <p>2017-09-01</p> <p>Laser <span class="hlt">shock</span> peening (LSP), an innovative surface treatment technique, generates <span class="hlt">compressive</span> residual stress on the surface of metallic components to improve their fatigue performance, wear resistance and corrosion resistance. To illustrate the dynamic response during LSP and residual stress fields after LSP, this study conducted FEM simulations of LSP in a Ti6Al4V alloy. Results showed that when power density was 7 GW cm-2, a plastic deformation occurred at 10 ns during LSP and increased until the <span class="hlt">shock</span> pressure decayed below the dynamic yield strength of Ti6Al4V after 60 ns. A maximum tensile region appeared beneath the surface at around 240 ns, forming a <span class="hlt">compressive-tensile-compressive</span> stress sandwich structure with a thickness of 98, 1020 and 606 μm for each layer. After the model became stabilized, the value of the surface residual <span class="hlt">compressive</span> stress was 564 MPa at the laser spot center. Higher value of residual stress across the surface and thicker <span class="hlt">compressive</span> residual stress layers were achieved by increasing laser power density, impact times and spot sizes during LSP. A ‘Residual stress hole’ occurred with a high laser power density of 9 GW cm-2 when laser pulse duration was 10 ns, or with a long laser pulse duration of 20 ns when laser power density was 7 GW cm-2 for Ti6Al4V. This phenomenon occurred because of the permanent reverse plastic deformation generated at laser spot center.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016APS..MARX21016Z','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016APS..MARX21016Z"><span><span class="hlt">Compressible</span> Heating in the Condense Phase due to Pore Collapse in HMX</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Zhang, Ju; Jackson, Thomas</p> <p></p> <p>Axisymmetric pore collapse in HMX is studied numerically by solving multi-phase reactive Euler equations. The generation of hot spots in the condense phase due to <span class="hlt">compressible</span> heating is examined. The motivation is to improve the understanding of the role of embedded cavities in the initiation of reaction in explosives, and to investigate the effect of hot spots in the condense phase due to <span class="hlt">compressible</span> heating alone, complementing previous study on hot spots due to the reaction in the gas phase and at the interface. It is found that the <span class="hlt">shock</span>-cavity interaction results in pressures and thus temperatures that are substantially higher than the post-<span class="hlt">shock</span> values in the condense phase. However, these hot spots in the condense phase due to <span class="hlt">compressible</span> heating alone do not seem to be sufficiently hot to lead to ignition at <span class="hlt">shock</span> pressures of 1-3 GPa. Thus, <span class="hlt">compressible</span> heating in the condense phase may be excluded as a mechanism for initiation of explosives. It should be pointed out that the ignition threshold for the temperature, the so-called ``switch-on'' temperature, of hot spots depend on chemistry kinetics parameters. Switch-on temperature is lower for faster reaction rate. The current chemistry kinetics parameters are based on previous experimental work. This work was supported in part by the Defense Threat Reduction Agency and by the U.S. Department of Energy.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19950058991&hterms=mediation&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D20%26Ntt%3Dmediation','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19950058991&hterms=mediation&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D20%26Ntt%3Dmediation"><span>Steady state and dynamical structure of a cosmic-ray-modified termination <span class="hlt">shock</span></span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Donohue, D. J.; Zank, G. P.</p> <p>1993-01-01</p> <p>A hydrodynamic model is developed for the structure of a cosmic-ray-modified termination <span class="hlt">shock</span>. The model is based on the two-fluid equations of diffuse <span class="hlt">shock</span> acceleration (Drury and Volk, 1981). Both the steady state structure of the <span class="hlt">shock</span> and its interaction with outer heliospheric disturbances are considered. Under the assumption that the solar wind is decelerated by diffusing interstellar cosmic rates, it is shown that the natural state of the termination <span class="hlt">shock</span> is a gradual deceleration and <span class="hlt">compression</span>, followed by a discontinuous jump to a downstream state which is dominated by the pressure contribution of the cosmic rays. A representative model is calculated for the steady state which incorporates both interstellar cosmic ray mediation and diffusively accelerated anomalous ions through a proposed thermal leakage mechanism. The interaction of large-scale disturbances with the equilibrium termination <span class="hlt">shock</span> model is shown to result in some unusual downstream structure, including transmitted <span class="hlt">shocks</span> and cosmic-ray-modified contact discontinuities. The structure observed may be connected to the 2-kHz outer heliospheric radio emission (Cairns et al., 1992a, b). The time-dependent simulations also demonstrate that interaction with solar wind <span class="hlt">compressible</span> turbulence (e.g., traveling interplanetary <span class="hlt">shocks</span>, etc.) could induce the termination <span class="hlt">shock</span> to continually fluctuate between cosmic-ray-dominated and gas-dynamic states. This fluctuation may represent a partial explanation of the galactic cosmic ray modulation effect and illustrates that the Pioneer and Voyager satellites will encounter an evolving <span class="hlt">shock</span> whose structure and dynamic properties are strongly influence by the mediation of interstellar and anomalous cosmic rays.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/1993JGR....9819005D','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/1993JGR....9819005D"><span>Steady state and dynamical structure of a cosmic-ray-modified termination <span class="hlt">shock</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Donohue, D. J.; Zank, G. P.</p> <p>1993-11-01</p> <p>A hydrodynamic model is developed for the structure of a cosmic-ray-modified termination <span class="hlt">shock</span>. The model is based on the two-fluid equations of diffuse <span class="hlt">shock</span> acceleration (Drury and Volk, 1981). Both the steady state structure of the <span class="hlt">shock</span> and its interaction with outer heliospheric disturbances are considered. Under the assumption that the solar wind is decelerated by diffusing interstellar cosmic rates, it is shown that the natural state of the termination <span class="hlt">shock</span> is a gradual deceleration and <span class="hlt">compression</span>, followed by a discontinuous jump to a downstream state which is dominated by the pressure contribution of the cosmic rays. A representative model is calculated for the steady state which incorporates both interstellar cosmic ray mediation and diffusively accelerated anomalous ions through a proposed thermal leakage mechanism. The interaction of large-scale disturbances with the equilibrium termination <span class="hlt">shock</span> model is shown to result in some unusual downstream structure, including transmitted <span class="hlt">shocks</span> and cosmic-ray-modified contact discontinuities. The structure observed may be connected to the 2-kHz outer heliospheric radio emission (Cairns et al., 1992a, b). The time-dependent simulations also demonstrate that interaction with solar wind <span class="hlt">compressible</span> turbulence (e.g., traveling interplanetary <span class="hlt">shocks</span>, etc.) could induce the termination <span class="hlt">shock</span> to continually fluctuate between cosmic-ray-dominated and gas-dynamic states. This fluctuation may represent a partial explanation of the galactic cosmic ray modulation effect and illustrates that the Pioneer and Voyager satellites will encounter an evolving <span class="hlt">shock</span> whose structure and dynamic properties are strongly influence by the mediation of interstellar and anomalous cosmic rays.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_18");'>18</a></li> <li><a href="#" onclick='return showDiv("page_19");'>19</a></li> <li class="active"><span>20</span></li> <li><a href="#" onclick='return showDiv("page_21");'>21</a></li> <li><a href="#" onclick='return showDiv("page_22");'>22</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_20 --> <div id="page_21" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_19");'>19</a></li> <li><a href="#" onclick='return showDiv("page_20");'>20</a></li> <li class="active"><span>21</span></li> <li><a href="#" onclick='return showDiv("page_22");'>22</a></li> <li><a href="#" onclick='return showDiv("page_23");'>23</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="401"> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2008PhDT.......300M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2008PhDT.......300M"><span>Microscale <span class="hlt">shock</span> tube</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Mirshekari, Gholamreza</p> <p></p> <p>This project aims at the simulation, design, fabrication and testing of a microscale <span class="hlt">shock</span> tube. A step by step procedure has been followed to develop the different components of the microscale <span class="hlt">shock</span> tube and then combine them together to realize the final device. The document reports on the numerical simulation of flows in a microscale <span class="hlt">shock</span> tube, the experimental study of gas flow in microchannels, the design, microfabrication, and the test of a microscale <span class="hlt">shock</span> tube. In the first step, a one-dimensional numerical model for simulation of transport effects at small-scale, appeared in low Reynolds number <span class="hlt">shock</span> tubes is developed. The conservation equations have been integrated in the lateral directions and three-dimensional effects have been introduced as carefully controlled sources of mass, momentum and energy, into the one-dimensional model. The unsteady flow of gas behind the <span class="hlt">shock</span> wave is reduced to a quasi-steady laminar flow solution, similar to the Blasius solution. The resulting one-dimensional equations are solved numerically and the simulations are performed for previously reported low Reynolds number <span class="hlt">shock</span> tube experiments. Good agreement between the <span class="hlt">shock</span> structure simulation and the attenuation due to the boundary layers has been observed. The simulation for predicting the performance of a microscale <span class="hlt">shock</span> tube shows the large attenuation of <span class="hlt">shock</span> wave at low pressure ratios. In the next step the steady flow inside microchannels has been experimentally studied. A set of microchannels with different geometries were fabricated. These microchannels have been used to measure the pressure drop as a function of flow rate in a steady <span class="hlt">compressible</span> flow. The results of the experiments confirm that the flow inside the microscale <span class="hlt">shock</span> tube follows the laminar model over the experiment's range of Knudsen number. The microscale <span class="hlt">shock</span> tube is fabricated by deposition and patterning of different thin layers of selected materials on the silicon substrate. The direct</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/23003273','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/23003273"><span>Precision <span class="hlt">shock</span> tuning on the national ignition facility.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Robey, H F; Celliers, P M; Kline, J L; Mackinnon, A J; Boehly, T R; Landen, O L; Eggert, J H; Hicks, D; Le Pape, S; Farley, D R; Bowers, M W; Krauter, K G; Munro, D H; Jones, O S; Milovich, J L; Clark, D; Spears, B K; Town, R P J; Haan, S W; Dixit, S; Schneider, M B; Dewald, E L; Widmann, K; Moody, J D; Döppner, T D; Radousky, H B; Nikroo, A; Kroll, J J; Hamza, A V; Horner, J B; Bhandarkar, S D; Dzenitis, E; Alger, E; Giraldez, E; Castro, C; Moreno, K; Haynam, C; LaFortune, K N; Widmayer, C; Shaw, M; Jancaitis, K; Parham, T; Holunga, D M; Walters, C F; Haid, B; Malsbury, T; Trummer, D; Coffee, K R; Burr, B; Berzins, L V; Choate, C; Brereton, S J; Azevedo, S; Chandrasekaran, H; Glenzer, S; Caggiano, J A; Knauer, J P; Frenje, J A; Casey, D T; Johnson, M Gatu; Séguin, F H; Young, B K; Edwards, M J; Van Wonterghem, B M; Kilkenny, J; MacGowan, B J; Atherton, J; Lindl, J D; Meyerhofer, D D; Moses, E</p> <p>2012-05-25</p> <p>Ignition implosions on the National Ignition Facility [J. D. Lindl et al., Phys. Plasmas 11, 339 (2004)] are underway with the goal of <span class="hlt">compressing</span> deuterium-tritium fuel to a sufficiently high areal density (ρR) to sustain a self-propagating burn wave required for fusion power gain greater than unity. These implosions are driven with a very carefully tailored sequence of four <span class="hlt">shock</span> waves that must be timed to very high precision to keep the fuel entropy and adiabat low and ρR high. The first series of precision tuning experiments on the National Ignition Facility, which use optical diagnostics to directly measure the strength and timing of all four <span class="hlt">shocks</span> inside a hohlraum-driven, cryogenic liquid-deuterium-filled capsule interior have now been performed. The results of these experiments are presented demonstrating a significant decrease in adiabat over previously untuned implosions. The impact of the improved <span class="hlt">shock</span> timing is confirmed in related deuterium-tritium layered capsule implosions, which show the highest fuel <span class="hlt">compression</span> (ρR~1.0 g/cm(2)) measured to date, exceeding the previous record [V. Goncharov et al., Phys. Rev. Lett. 104, 165001 (2010)] by more than a factor of 3. The experiments also clearly reveal an issue with the 4th <span class="hlt">shock</span> velocity, which is observed to be 20% slower than predictions from numerical simulation.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017APS..SHK.P4004M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017APS..SHK.P4004M"><span><span class="hlt">Shock</span> chemistry in SX358 foams</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Maerzke, Katie; Coe, Joshua; Fredenburg, Anthony; Lang, John; Dattelbaum, Dana</p> <p>2017-06-01</p> <p>We have developed new equation of state models for SX358, a cross-linked PDMS polymer. Recent experiments on SX358 over a range of initial densities (0-65% porous) have yielded new data that allow for a more thorough calibration of the equations of state. SX358 chemically decomposes under <span class="hlt">shock</span> <span class="hlt">compression</span>, as evidenced by a cusp in the <span class="hlt">shock</span> locus. We therefore treat this material using two equations of state, specifically a SESAME model for the unreacted material and a free energy minimization assuming full chemical and thermodynamic equilibrium for the decomposition products. The <span class="hlt">shock</span> locus of porous SX358 is found to be ``anomalous'' in that the decomposition reaction causes a volume expansion, rather than a volume collapse. Similar behavior has been observed in other polymer foams, notably polyurethane.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017AIPC.1793n0007J','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017AIPC.1793n0007J"><span>Properties and <span class="hlt">shock</span> response of PMMA</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Jordan, Jennifer L.; Casem, Daniel; Moy, Paul; Walter, Timothy</p> <p>2017-01-01</p> <p>Polymethylmethacrylate (PMMA) is used widely in <span class="hlt">shock</span> experiments as a window material and in explosive characterization tests, e.g. gap tests, as a <span class="hlt">shock</span> mitigation material. In order to simulate the complex loading present in a gap test, the constitutive response of the PMMA must be well understood. However, it is not clear what characterization must be done when the PMMA material is changed, e.g. changing supplier, and the Rohm and Haas Type II UVA PMMA, which was used for many of the calibration experiments, is no longer available. In this paper, we will present characterization results on legacy Rohm and Haas Type II UVA in comparison with a new PMMA grade proposed for use in gap tests. Planar <span class="hlt">shock</span> experiments are performed to determine the <span class="hlt">compression</span> and release response.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2013APS..SHK.C1001C','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2013APS..SHK.C1001C"><span><span class="hlt">Shock</span> structures at ultrahigh strain rates: what can they tell us about material behavior on very fast time scales?</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Crowhurst, Jonathan</p> <p>2013-06-01</p> <p>In recent years, techniques based on table-top laser systems have shown promise for investigating dynamic material behavior at high rates of both <span class="hlt">compressive</span> and tensile strain. Common to these techniques is a laser pulse that is used in some manner to rapidly deliver energy to the sample; while the energy itself is often comparatively very small, the intensity can be made high by tightly focusing the pump light. In this way pressures or stresses can be obtained that are sufficiently large to have relevance to a wide range of basic and applied fields. Also, when combined with established ultrafast diagnostics these experiments provide very high time resolution which is particularly desirable when studying, for example <span class="hlt">shock</span> waves, in which the time for the material to pass from undisturbed to fully <span class="hlt">compressed</span> (the ``rise time'') can be extremely short (order 10 ps or less) even at fairly small peak stresses. Since much of the most interesting physics comes into play during this process it is important to be able to adequately resolve the <span class="hlt">shock</span> rise. In this context I will discuss our measurements on aluminum and <span class="hlt">iron</span> thin films and compare the results with known behavior observed at lower strain rates. Specifically, for aluminum, I will compare our assumed steady wave data at strain rates of up to 1010 s-1 to literature data up to ~107 s-1 and show that the well-known fourth power scaling relation of strain rate to <span class="hlt">shock</span> stress is maintained even at these very high strain rates. For <span class="hlt">iron</span>, I will show how we have used our nonsteady data (up to ~109 s-1) to infer a number of important properties of the alpha to epsilon polymorphic transition: 1. The transition can occur on the tens of ps time scale at sufficiently high strain rates and corresponding very large deviatoric stresses, and 2, most of the material appears to transform at a substantially higher stress than the nominal value usually inferred from <span class="hlt">shock</span> wave experiments of about 13 GPa. This work was</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/24672620','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/24672620"><span>The effect of compressor-administered defibrillation on peri-<span class="hlt">shock</span> pauses in a simulated cardiac arrest scenario.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Glick, Joshua; Lehman, Erik; Terndrup, Thomas</p> <p>2014-03-01</p> <p>Coordination of the tasks of performing chest <span class="hlt">compressions</span> and defibrillation can lead to communication challenges that may prolong time spent off the chest. The purpose of this study was to determine whether defibrillation provided by the provider performing chest <span class="hlt">compressions</span> led to a decrease in peri-<span class="hlt">shock</span> pauses as compared to defibrillation administered by a second provider, in a simulated cardiac arrest scenario. This was a randomized, controlled study measuring pauses in chest <span class="hlt">compressions</span> for defibrillation in a simulated cardiac arrest model. We approached hospital providers with current CPR certification for participation between July, 2011 and October, 2011. Volunteers were randomized to control (facilitator-administered defibrillation) or experimental (compressor-administered defibrillation) groups. All participants completed one minute of chest <span class="hlt">compressions</span> on a mannequin in a shockable rhythm prior to administration of defibrillation. We measured and compared pauses for defibrillation in both groups. Out of 200 total participants, we analyzed data from 197 defibrillations. Compressor-initiated defibrillation resulted in a significantly lower pre-<span class="hlt">shock</span> hands-off time (0.57 s; 95% CI: 0.47-0.67) compared to facilitator-initiated defibrillation (1.49 s; 95% CI: 1.35-1.64). Furthermore, compressor-initiated defibrillation resulted in a significantly lower peri-<span class="hlt">shock</span> hands-off time (2.77 s; 95% CI: 2.58-2.95) compared to facilitator-initiated defibrillation (4.25 s; 95% CI: 4.08-4.43). Assigning the responsibility for <span class="hlt">shock</span> delivery to the provider performing <span class="hlt">compressions</span> encourages continuous <span class="hlt">compressions</span> throughout the charging period and decreases total time spent off the chest. However, as this was a simulation-based study, clinical implementation is necessary to further evaluate these potential benefits.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3019584','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=3019584"><span>A Multi-Mode <span class="hlt">Shock</span> Tube for Investigation of Blast-Induced Traumatic Brain Injury</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Reneer, Dexter V.; Hisel, Richard D.; Hoffman, Joshua M.; Kryscio, Richard J.; Lusk, Braden T.</p> <p>2011-01-01</p> <p>Abstract Blast-induced mild traumatic brain injury (bTBI) has become increasingly common in recent military conflicts. The mechanisms by which non-impact blast exposure results in bTBI are incompletely understood. Current small animal bTBI models predominantly utilize <span class="hlt">compressed</span> air-driven membrane rupture as their blast wave source, while large animal models use chemical explosives. The pressure-time signature of each blast mode is unique, making it difficult to evaluate the contributions of the different components of the blast wave to bTBI when using a single blast source. We utilized a multi-mode <span class="hlt">shock</span> tube, the McMillan blast device, capable of utilizing <span class="hlt">compressed</span> air- and <span class="hlt">compressed</span> helium-driven membrane rupture, and the explosives oxyhydrogen and cyclotrimethylenetrinitramine (RDX, the primary component of C-4 plastic explosives) as the driving source. At similar maximal blast overpressures, the positive pressure phase of <span class="hlt">compressed</span> air-driven blasts was longer, and the positive impulse was greater, than those observed for shockwaves produced by other driving sources. Helium-driven shockwaves more closely resembled RDX blasts, but by displacing air created a hypoxic environment within the <span class="hlt">shock</span> tube. Pressure-time traces from oxyhydrogen-driven shockwaves were very similar those produced by RDX, although they resulted in elevated carbon monoxide levels due to combustion of the polyethylene bag used to contain the gases within the <span class="hlt">shock</span> tube prior to detonation. Rats exposed to <span class="hlt">compressed</span> air-driven blasts had more pronounced vascular damage than those exposed to oxyhydrogen-driven blasts of the same peak overpressure, indicating that differences in blast wave characteristics other than peak overpressure may influence the extent of bTBI. Use of this multi-mode <span class="hlt">shock</span> tube in small animal models will enable comparison of the extent of brain injury with the pressure-time signature produced using each blast mode, facilitating evaluation of the blast wave</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/21083431','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/21083431"><span>A multi-mode <span class="hlt">shock</span> tube for investigation of blast-induced traumatic brain injury.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Reneer, Dexter V; Hisel, Richard D; Hoffman, Joshua M; Kryscio, Richard J; Lusk, Braden T; Geddes, James W</p> <p>2011-01-01</p> <p>Blast-induced mild traumatic brain injury (bTBI) has become increasingly common in recent military conflicts. The mechanisms by which non-impact blast exposure results in bTBI are incompletely understood. Current small animal bTBI models predominantly utilize <span class="hlt">compressed</span> air-driven membrane rupture as their blast wave source, while large animal models use chemical explosives. The pressure-time signature of each blast mode is unique, making it difficult to evaluate the contributions of the different components of the blast wave to bTBI when using a single blast source. We utilized a multi-mode <span class="hlt">shock</span> tube, the McMillan blast device, capable of utilizing <span class="hlt">compressed</span> air- and <span class="hlt">compressed</span> helium-driven membrane rupture, and the explosives oxyhydrogen and cyclotrimethylenetrinitramine (RDX, the primary component of C-4 plastic explosives) as the driving source. At similar maximal blast overpressures, the positive pressure phase of <span class="hlt">compressed</span> air-driven blasts was longer, and the positive impulse was greater, than those observed for shockwaves produced by other driving sources. Helium-driven shockwaves more closely resembled RDX blasts, but by displacing air created a hypoxic environment within the <span class="hlt">shock</span> tube. Pressure-time traces from oxyhydrogen-driven shockwaves were very similar those produced by RDX, although they resulted in elevated carbon monoxide levels due to combustion of the polyethylene bag used to contain the gases within the <span class="hlt">shock</span> tube prior to detonation. Rats exposed to <span class="hlt">compressed</span> air-driven blasts had more pronounced vascular damage than those exposed to oxyhydrogen-driven blasts of the same peak overpressure, indicating that differences in blast wave characteristics other than peak overpressure may influence the extent of bTBI. Use of this multi-mode <span class="hlt">shock</span> tube in small animal models will enable comparison of the extent of brain injury with the pressure-time signature produced using each blast mode, facilitating evaluation of the blast wave components</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017ShWav..27..457F','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017ShWav..27..457F"><span><span class="hlt">Shock</span>-jump conditions in a general medium: weak-solution approach</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Forbes, L. K.; Krzysik, O. A.</p> <p>2017-05-01</p> <p>General conservation laws are considered, and the concept of a weak solution is extended to the case of an equation involving three space variables and time. Four-dimensional vector calculus is used to develop general jump conditions at a <span class="hlt">shock</span> wave in the material. To illustrate the use of this result, jump conditions at a <span class="hlt">shock</span> in unsteady three-dimensional <span class="hlt">compressible</span> gas flow are presented. It is then proved rigorously that these reduce to the commonly assumed conditions in coordinates normal and tangential to the <span class="hlt">shock</span> face. A similar calculation is also outlined for an unsteady three-dimensional <span class="hlt">shock</span> in magnetohydrodynamics, and in a chemically reactive fluid. The technique is available for determining <span class="hlt">shock</span>-jump conditions in quite general continuous media.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/29352795','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/29352795"><span>Impact of surface energy on the <span class="hlt">shock</span> properties of granular explosives.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Bidault, X; Pineau, N</p> <p>2018-01-21</p> <p>This paper presents the first part of a two-fold molecular dynamics study of the impact of the granularity on the <span class="hlt">shock</span> properties of high explosives. Recent experimental studies show that the granularity can have a substantial impact on the properties of detonation products {i.e., variations in the size distributions of detonation nanodiamonds [V. Pichot et al., Sci. Rep. 3, 2159 (2013)]}. These variations can have two origins: the surface energy, which is a priori enhanced from micro- to nano-scale, and the porosity induced by the granular structure. In this first report, we study the impact of the surface-energy contribution on the inert <span class="hlt">shock</span> <span class="hlt">compression</span> of TATB, TNT, α-RDX, and β-HMX nano-grains (triaminotrinitrobenzene, trinitrotoluene, hexogen and octogen, respectively). We compute the radius-dependent surface energy and combine it with an ab initio-based equation of state in order to obtain the resulting <span class="hlt">shock</span> properties through the Rankine-Hugoniot relations. We find that the enhancement of the surface energy results in a moderate overheating under <span class="hlt">shock</span> <span class="hlt">compression</span>. This contribution is minor with respect to porosity, when compared to a simple macroscopic model. This result motivates further atomistic studies on the impact of nanoporosity networks on the <span class="hlt">shock</span> properties.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018JChPh.148c4704B','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018JChPh.148c4704B"><span>Impact of surface energy on the <span class="hlt">shock</span> properties of granular explosives</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Bidault, X.; Pineau, N.</p> <p>2018-01-01</p> <p>This paper presents the first part of a two-fold molecular dynamics study of the impact of the granularity on the <span class="hlt">shock</span> properties of high explosives. Recent experimental studies show that the granularity can have a substantial impact on the properties of detonation products {i.e., variations in the size distributions of detonation nanodiamonds [V. Pichot et al., Sci. Rep. 3, 2159 (2013)]}. These variations can have two origins: the surface energy, which is a priori enhanced from micro- to nano-scale, and the porosity induced by the granular structure. In this first report, we study the impact of the surface-energy contribution on the inert <span class="hlt">shock</span> <span class="hlt">compression</span> of TATB, TNT, α-RDX, and β-HMX nano-grains (triaminotrinitrobenzene, trinitrotoluene, hexogen and octogen, respectively). We compute the radius-dependent surface energy and combine it with an ab initio-based equation of state in order to obtain the resulting <span class="hlt">shock</span> properties through the Rankine-Hugoniot relations. We find that the enhancement of the surface energy results in a moderate overheating under <span class="hlt">shock</span> <span class="hlt">compression</span>. This contribution is minor with respect to porosity, when compared to a simple macroscopic model. This result motivates further atomistic studies on the impact of nanoporosity networks on the <span class="hlt">shock</span> properties.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20120000915','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20120000915"><span>Quasi 1D Modeling of Mixed <span class="hlt">Compression</span> Supersonic Inlets</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Kopasakis, George; Connolly, Joseph W.; Paxson, Daniel E.; Woolwine, Kyle J.</p> <p>2012-01-01</p> <p>The AeroServoElasticity task under the NASA Supersonics Project is developing dynamic models of the propulsion system and the vehicle in order to conduct research for integrated vehicle dynamic performance. As part of this effort, a nonlinear quasi 1-dimensional model of the 2-dimensional bifurcated mixed <span class="hlt">compression</span> supersonic inlet is being developed. The model utilizes computational fluid dynamics for both the supersonic and subsonic diffusers. The oblique <span class="hlt">shocks</span> are modeled utilizing <span class="hlt">compressible</span> flow equations. This model also implements variable geometry required to control the normal <span class="hlt">shock</span> position. The model is flexible and can also be utilized to simulate other mixed <span class="hlt">compression</span> supersonic inlet designs. The model was validated both in time and in the frequency domain against the legacy LArge Perturbation INlet code, which has been previously verified using test data. This legacy code written in FORTRAN is quite extensive and complex in terms of the amount of software and number of subroutines. Further, the legacy code is not suitable for closed loop feedback controls design, and the simulation environment is not amenable to systems integration. Therefore, a solution is to develop an innovative, more simplified, mixed <span class="hlt">compression</span> inlet model with the same steady state and dynamic performance as the legacy code that also can be used for controls design. The new nonlinear dynamic model is implemented in MATLAB Simulink. This environment allows easier development of linear models for controls design for <span class="hlt">shock</span> positioning. The new model is also well suited for integration with a propulsion system model to study inlet/propulsion system performance, and integration with an aero-servo-elastic system model to study integrated vehicle ride quality, vehicle stability, and efficiency.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19850026419','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19850026419"><span>First-order <span class="hlt">shock</span> acceleration in solar flares</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Ellison, D. C.; Ramaty, R.</p> <p>1985-01-01</p> <p>The first order Fermi <span class="hlt">shock</span> acceleration model is compared with specific observations where electron, proton, and alpha particle spectra are available. In all events, it is found that a single <span class="hlt">shock</span> with a <span class="hlt">compression</span> ratio as inferred from the low energy proton spectra can reasonably produce the full proton, electron, and alpha particle spectra. The model predicts that the acceleration time to a given energy will be approximately equal for electrons and protons and, for reasonable solar parameters, can be less than 1 sec to 100 MeV.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19780015250','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19780015250"><span>The role of thermal <span class="hlt">shock</span> in cyclic oxidation</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Lowell, C. E.; Deadmore, D. L.</p> <p>1978-01-01</p> <p>The effect of thermal <span class="hlt">shock</span> on the spalling of oxides from the surfaces of several commercial alloys was determined. The average cooling rate was varied from approximately 240 C per second to less than 1.0 C per second during cyclic oxidation tests in air. The tests consisted of one hundred cycles of one hour at the maximum temperature (1100 or 1200 C). The alloys were HOS-875, TD-Ni, TD-NiCrAl, IN-601, IN-702, and B-1900 plus Hf. All of these alloys exhibited partial spalling within the oxide rather than total oxide loss down to bare metal. Thermal <span class="hlt">shock</span> resulted in deformation of the metal which in turn resulted, in most cases, in changing the oxide failure mode from <span class="hlt">compressive</span> to tensile. Tensile failures were characterized by cracking of the oxide and little loss, while <span class="hlt">compressive</span> failures were characterized by explosive loss of platelets of oxide. This behavior was confirmed by examination of mechanically stressed oxide scales. The thermally <span class="hlt">shocked</span> oxides spalled less than the slow cooled samples with the exception of TD-NiCrAl. This material failed in a brittle manner rather than by plastic deformation.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017PhRvL.119i8001S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017PhRvL.119i8001S"><span><span class="hlt">Compression</span> and Reswelling of Microgel Particles after an Osmotic <span class="hlt">Shock</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Sleeboom, Jelle J. F.; Voudouris, Panayiotis; Punter, Melle T. J. J. M.; Aangenendt, Frank J.; Florea, Daniel; van der Schoot, Paul; Wyss, Hans M.</p> <p>2017-09-01</p> <p>We use dedicated microfluidic devices to expose soft hydrogel particles to a rapid change in the externally applied osmotic pressure and observe a surprising, nonmonotonic response: After an initial rapid <span class="hlt">compression</span>, the particle slowly reswells to approximately its original size. We theoretically account for this behavior, enabling us to extract important material properties from a single microfluidic experiment, including the <span class="hlt">compressive</span> modulus, the gel permeability, and the diffusivity of the osmolyte inside the gel. We expect our approach to be relevant to applications such as controlled release, chromatography, and responsive materials.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4278991','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=4278991"><span>Spinal Cord Ischemia Secondary to Hypovolemic <span class="hlt">Shock</span></span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Kapoor, Siddhant; Koh, Roy KM; Yang, Eugene WR; Hee, Hwan-Tak</p> <p>2014-01-01</p> <p>A 44-year-old male presented with symptoms of spinal cord <span class="hlt">compression</span> secondary to metastatic prostate cancer. An urgent decompression at the cervical-thoracic region was performed, and there were no complications intraoperatively. Three hours postoperatively, the patient developed acute bilateral lower-limb paralysis (motor grade 0). Clinically, he was in class 3 hypovolemic <span class="hlt">shock</span>. An urgent magnetic resonance imaging (MRI) was performed, showing no epidural hematoma. He was managed aggressively with medical therapy to improve his spinal cord perfusion. The patient improved significantly, and after one week, he was able to regain most of his motor functions. Although not commonly reported, spinal cord ischemia post-surgery should be recognized early, especially in the presence of hypovolemic <span class="hlt">shock</span>. MRI should be performed to exclude other potential causes of <span class="hlt">compression</span>. Spinal cord ischemia needs to be managed aggressively with medical treatment to improve spinal cord perfusion. The prognosis depends on the severity of deficits, and is usually favorable. PMID:25558328</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19930061501&hterms=free-piston&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D50%26Ntt%3Dfree-piston','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19930061501&hterms=free-piston&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D50%26Ntt%3Dfree-piston"><span>Performance data of the new free-piston <span class="hlt">shock</span> tunnel T5 at GALCIT</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Hornung, H.; Sturtevant, B.; Belanger, J.; Sanderson, S.; Brouillette, M.; Jenkins, M.</p> <p>1992-01-01</p> <p>A new free piston <span class="hlt">shock</span> tunnel has been constructed at the Graduate Aeronautical Laboratories at Caltec. <span class="hlt">Compression</span> tube length is 30 m and diameter 300 mm. <span class="hlt">Shock</span> tube length is 12 m and diameter 90 mm. Piston mass is 150 kg and maximum diaphragm burst pressure is 130 MPa. Special features of this facility are that the pressure in the driver gas is monitored throughout the <span class="hlt">compression</span> process until well after diaphragm rupture, and that the diaphragm burst pressure can be measured dynamically. An analysis of initial performance data including transient behavior of the flow over models is presented.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2012APS..DPPKI3001P','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2012APS..DPPKI3001P"><span>Supernova dynamics in the laboratory: Radiative <span class="hlt">shocks</span> produced by ultra-high pressure implosion experiments on the National Ignition Facility</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Pak, Arthur</p> <p>2012-10-01</p> <p>Thermonuclear fuel experiments on the National Ignition Facility implode 2-mm diameter capsules with a cryogenic deuterium-tritium ice layer to 1000x liquid density and pressures exceeding 100 Gbar (10^11 atm). About 200 ps after peak <span class="hlt">compression</span>, a spherical supernova-like radiative <span class="hlt">shock</span> wave is observed that expands with <span class="hlt">shock</span> velocities of uS = 300 km/s, temperatures of order 1 keV at densities of 1 g/cc resulting in a radiation strength parameter of Q ˜uS^5 = 10^4. Radiation-hydrodynamic simulations indicate that the <span class="hlt">shock</span> launched at stagnation first goes down a strong density gradient while propagating outward from the highly <span class="hlt">compressed</span> DT fuel (˜ 1000g/cc) to the ablation front (˜ 1 g/cc). Similar to what happens inside a star, the <span class="hlt">shock</span> pressure drops as it accelerates and heats. The radiative <span class="hlt">shock</span> emission is first observed when it breaks out of the dense <span class="hlt">compressed</span> fuel shell into the low-density inflowing plasma at the ablation front mimicking the supernova situation where the <span class="hlt">shock</span> breaks out through the star surface into surrounding in-falling matter [1,2]; the <span class="hlt">shock</span> is subsequently approaching the supercritical state with a strong pre-cursor followed by rapid cooling. These observations are consistent with the rapid vanishing of the radiation ring 400 ps after peak <span class="hlt">compression</span> due to strong radiation losses and spherical expansion. The evolution and brightness of the radiative <span class="hlt">shock</span> provides insight into the performance of these implosions that have the goal to produce burning fusion plasmas in the laboratory. By modifying the capsule ablator composition and thickness, the stagnation pressure, density gradients, <span class="hlt">shock</span> velocity and radiative properties could be tailored to study various regimes related to supernovae radiative remnants.[4pt] [1] W. David Arnett, Supernovae as phenomena of high-energy astrophysics, Ann NY Aca. Science 302, 90 (1977).[0pt] [2] L. Ensman and A. Burrows, <span class="hlt">Shock</span> breakout in SN1987A, ApJ 393, 742.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19900011634','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19900011634"><span>Effects of nose bluntness and <span class="hlt">shock-shock</span> interactions on blunt bodies in viscous hypersonic flows</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Singh, D. J.; Tiwari, S. N.</p> <p>1990-01-01</p> <p>A numerical study was conducted to investigate the effects of blunt leading edges on the viscous flow field around a hypersonic vehicle such as the proposed National Aero-Space Plane. Attention is focused on two specific regions of the flow field. In the first region, effects of nose bluntness on the forebody flow field are investigated. The second region of the flow considered is around the leading edges of the scramjet inlet. In this region, the interaction of the forebody <span class="hlt">shock</span> with the <span class="hlt">shock</span> produced by the blunt leading edges of the inlet <span class="hlt">compression</span> surfaces is analyzed. Analysis of these flow regions is required to accurately predict the overall flow field as well as to get necessary information on localized zones of high pressure and intense heating. The results for the forebody flow field are discussed first, followed by the results for the <span class="hlt">shock</span> interaction in the inlet leading edge region.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20070018211','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20070018211"><span>Experimental <span class="hlt">Shock</span> Decomposition of Siderite and the Origin of Magnetite in Martian Meteorite ALH84001</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Bell, Mary Sue</p> <p>2007-01-01</p> <p><span class="hlt">Shock</span> recovery experiments to determine whether magnetite could be produced by the decomposition of <span class="hlt">iron</span>-carbonate were initiated. Naturally occurring siderite was first characterized by electron microprobe (EMP), transmission electron microscopy (TEM), Mossbauer spectroscopy, and magnetic susceptibility measurements to be sure that the starting material did not contain detectable magnetite. Samples were <span class="hlt">shocked</span> in tungsten-alloy holders (W=90%, Ni=6%, Cu=4%) to further insure that any <span class="hlt">iron</span> phases in the <span class="hlt">shock</span> products were contributed by the siderite rather than the sample holder. Each sample was <span class="hlt">shocked</span> to a specific pressure between 30 to 49 GPa. Previously reported results of TEM analyses on 49 GPa experiments indicated the presence of nano-phase spinel-structured <span class="hlt">iron</span> oxide. Transformation of siderite to magnetite as characterized by TEM was found in the 49 GPa <span class="hlt">shock</span> experiment. Compositions of most magnetites are greater than 50% Fe sup(+2) in the octahedral site of the inverse spinel structure. Magnetites produced in <span class="hlt">shock</span> experiments display the same range of single-domain, superparamagnetic sizes (approx. 50 100 nm), compositions (100% magnetite to 80% magnetite-20% magnesioferrite), and morphologies (equant, elongated, euhedral to subhedral) as magnetites synthesized by Golden et al. (2001) or magnetites grown naturally by MV1 magnetotactic bacteria, and as the magnetites in Martian meteorite ALH84001. Fritz et al. (2005) previously concluded that ALH84001 experienced approx. 32 GPa pressure and a resultant thermal pulse of approx. 100 - 110 C. However, ALH84001 contains evidence of local temperature excursions high enough to 1 melt feldspar, pyroxene, and a silica-rich phase. This 49 GPa experiment demonstrates that magnetite can be produced by the <span class="hlt">shock</span> decomposition of siderite as a result of local heating to greater than 470 C. Therefore, magnetite in the rims of carbonates in Martian meteorite ALH84001 could be a product of <span class="hlt">shock</span> devolatilization of</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_19");'>19</a></li> <li><a href="#" onclick='return showDiv("page_20");'>20</a></li> <li class="active"><span>21</span></li> <li><a href="#" onclick='return showDiv("page_22");'>22</a></li> <li><a href="#" onclick='return showDiv("page_23");'>23</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_21 --> <div id="page_22" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_20");'>20</a></li> <li><a href="#" onclick='return showDiv("page_21");'>21</a></li> <li class="active"><span>22</span></li> <li><a href="#" onclick='return showDiv("page_23");'>23</a></li> <li><a href="#" onclick='return showDiv("page_24");'>24</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="421"> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/22599139-converging-shock-wave-focusing-interaction-target','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/22599139-converging-shock-wave-focusing-interaction-target"><span>Converging <span class="hlt">shock</span> wave focusing and interaction with a target</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Nitishinskiy, M.; Efimov, S.; Antonov, O.</p> <p>2016-04-15</p> <p>Converging <span class="hlt">shock</span> waves in liquids can be used efficiently in the research of the extreme state of matter and in various applications. In this paper, the recent results related to the interaction of a <span class="hlt">shock</span> wave with plasma preliminarily formed in the vicinity of the <span class="hlt">shock</span> wave convergence are presented. The <span class="hlt">shock</span> wave is produced by the underwater electrical explosion of a spherical wire array. The plasma is generated prior to the <span class="hlt">shock</span> wave's arrival by a low-pressure gas discharge inside a quartz capillary placed at the equatorial plane of the array. Analysis of the Stark broadening of H{sub α}more » and H{sub β} spectral lines and line-to-continuum ratio, combined with the ratio of the relative intensities of carbon C III/C II and silicon Si III/Si II lines, were used to determine the plasma density and temperature evolution. It was found that during the first ∼200 ns with respect to the beginning of the plasma <span class="hlt">compression</span> by the <span class="hlt">shock</span> wave and when the spectral lines are resolved, the plasma density increases from 2 × 10{sup 17 }cm{sup −3} to 5 × 10{sup 17 }cm{sup −3}, while the temperature remains at the same value of 3–4 eV. Further, following the model of an adiabatically imploding capillary, the plasma density increases >10{sup 19 }cm{sup −3}, leading to the continuum spectra obtained experimentally, and the plasma temperature >30 eV at radii of <span class="hlt">compression</span> of ≤20 μm. The data obtained indicate that the <span class="hlt">shock</span> wave generated by the underwater electrical explosion of a spherical wire array retains its uniformity during the main part of its convergence.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018ShWav..28..863M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018ShWav..28..863M"><span>Thermofluidic <span class="hlt">compression</span> effects to achieve combustion in a low-<span class="hlt">compression</span> scramjet engine</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Moura, A. F.; Wheatley, V.; Jahn, I.</p> <p>2018-07-01</p> <p>The <span class="hlt">compression</span> provided by a scramjet inlet is an important parameter in its design. It must be low enough to limit thermal and structural loads and stagnation pressure losses, but high enough to provide the conditions favourable for combustion. Inlets are typically designed to achieve sufficient <span class="hlt">compression</span> without accounting for the fluidic, and subsequently thermal, <span class="hlt">compression</span> provided by the fuel injection, which can enable robust combustion in a low-<span class="hlt">compression</span> engine. This is investigated using Reynolds-averaged Navier-Stokes numerical simulations of a simplified scramjet engine designed to have insufficient <span class="hlt">compression</span> to auto-ignite fuel in the absence of thermofluidic <span class="hlt">compression</span>. The engine was designed with a wide rectangular combustor and a single centrally located injector, in order to reduce three-dimensional effects of the walls on the fuel plume. By varying the injected mass flow rate of hydrogen fuel (equivalence ratios of 0.22, 0.17, and 0.13), it is demonstrated that higher equivalence ratios lead to earlier ignition and more rapid combustion, even though mean conditions in the combustor change by no more than 5% for pressure and 3% for temperature with higher equivalence ratio. By supplementing the lower equivalence ratio with helium to achieve a higher mass flow rate, it is confirmed that these benefits are primarily due to the local <span class="hlt">compression</span> provided by the extra injected mass. Investigation of the conditions around the fuel plume indicated two connected mechanisms. The higher mass flow rate for higher equivalence ratios generated a stronger injector bow <span class="hlt">shock</span> that <span class="hlt">compresses</span> the free-stream gas, increasing OH radical production and promoting ignition. This was observed both in the higher equivalence ratio case and in the case with helium. This earlier ignition led to increased temperature and pressure downstream and, consequently, stronger combustion. The heat release from combustion provided thermal <span class="hlt">compression</span> in the combustor, further</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017ShWav.tmp..132M','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017ShWav.tmp..132M"><span>Thermofluidic <span class="hlt">compression</span> effects to achieve combustion in a low-<span class="hlt">compression</span> scramjet engine</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Moura, A. F.; Wheatley, V.; Jahn, I.</p> <p>2017-12-01</p> <p>The <span class="hlt">compression</span> provided by a scramjet inlet is an important parameter in its design. It must be low enough to limit thermal and structural loads and stagnation pressure losses, but high enough to provide the conditions favourable for combustion. Inlets are typically designed to achieve sufficient <span class="hlt">compression</span> without accounting for the fluidic, and subsequently thermal, <span class="hlt">compression</span> provided by the fuel injection, which can enable robust combustion in a low-<span class="hlt">compression</span> engine. This is investigated using Reynolds-averaged Navier-Stokes numerical simulations of a simplified scramjet engine designed to have insufficient <span class="hlt">compression</span> to auto-ignite fuel in the absence of thermofluidic <span class="hlt">compression</span>. The engine was designed with a wide rectangular combustor and a single centrally located injector, in order to reduce three-dimensional effects of the walls on the fuel plume. By varying the injected mass flow rate of hydrogen fuel (equivalence ratios of 0.22, 0.17, and 0.13), it is demonstrated that higher equivalence ratios lead to earlier ignition and more rapid combustion, even though mean conditions in the combustor change by no more than 5% for pressure and 3% for temperature with higher equivalence ratio. By supplementing the lower equivalence ratio with helium to achieve a higher mass flow rate, it is confirmed that these benefits are primarily due to the local <span class="hlt">compression</span> provided by the extra injected mass. Investigation of the conditions around the fuel plume indicated two connected mechanisms. The higher mass flow rate for higher equivalence ratios generated a stronger injector bow <span class="hlt">shock</span> that <span class="hlt">compresses</span> the free-stream gas, increasing OH radical production and promoting ignition. This was observed both in the higher equivalence ratio case and in the case with helium. This earlier ignition led to increased temperature and pressure downstream and, consequently, stronger combustion. The heat release from combustion provided thermal <span class="hlt">compression</span> in the combustor, further</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/8354759','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/8354759"><span>Propagation of <span class="hlt">shock</span> waves in elastic solids caused by cavitation microjet impact. II: Application in extracorporeal <span class="hlt">shock</span> wave lithotripsy.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Zhong, P; Chuong, C J; Preminger, G M</p> <p>1993-07-01</p> <p>To better understand the mechanism of stone fragmentation during extracorporeal <span class="hlt">shock</span> wave lithotripsy (ESWL), the model developed in Part I [P. Zhong and C.J. Chuong, J. Acoust. Soc. Am. 94, 19-28 (1993)] is applied to study cavitation microjet impingement and its resultant <span class="hlt">shock</span> wave propagation in renal calculi. Impact pressure at the stone boundary and stress, strain at the propagating <span class="hlt">shock</span> fronts in the stone were calculated for typical ESWL loading conditions. At the anterior surface of the stone, the jet induced <span class="hlt">compressive</span> stress can vary from 0.82 approximately 4 times that of the water hammer pressure depending on the contact angles; whereas the jet-induced shear stress can achieve its maximum, with a magnitude of 30% approximately 54% of the water hammer pressure, near the detachment of the longitudinal (or P) wave in the solid. Comparison of model predictions with material failure strengths of renal calculi suggests that jet impact can lead to stone surface erosion by combined <span class="hlt">compressive</span> and shear loadings at the jet impacting surface, and spalling failure by tensile forces at the distal surface of the stone. Comparing responses from four different stone types suggests that cystine is the most difficult stone to fragment in ESWL, as observed from clinical experience.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017Natur.550..496W','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017Natur.550..496W"><span>In situ X-ray diffraction measurement of <span class="hlt">shock</span>-wave-driven twinning and lattice dynamics</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Wehrenberg, C. E.; McGonegle, D.; Bolme, C.; Higginbotham, A.; Lazicki, A.; Lee, H. J.; Nagler, B.; Park, H.-S.; Remington, B. A.; Rudd, R. E.; Sliwa, M.; Suggit, M.; Swift, D.; Tavella, F.; Zepeda-Ruiz, L.; Wark, J. S.</p> <p>2017-10-01</p> <p>Pressure-driven <span class="hlt">shock</span> waves in solid materials can cause extreme damage and deformation. Understanding this deformation and the associated defects that are created in the material is crucial in the study of a wide range of phenomena, including planetary formation and asteroid impact sites, the formation of interstellar dust clouds, ballistic penetrators, spacecraft shielding and ductility in high-performance ceramics. At the lattice level, the basic mechanisms of plastic deformation are twinning (whereby crystallites with a mirror-image lattice form) and slip (whereby lattice dislocations are generated and move), but determining which of these mechanisms is active during deformation is challenging. Experiments that characterized lattice defects have typically examined the microstructure of samples after deformation, and so are complicated by post-<span class="hlt">shock</span> annealing and reverberations. In addition, measurements have been limited to relatively modest pressures (less than 100 gigapascals). In situ X-ray diffraction experiments can provide insights into the dynamic behaviour of materials, but have only recently been applied to plasticity during <span class="hlt">shock</span> <span class="hlt">compression</span> and have yet to provide detailed insight into competing deformation mechanisms. Here we present X-ray diffraction experiments with femtosecond resolution that capture in situ, lattice-level information on the microstructural processes that drive <span class="hlt">shock</span>-wave-driven deformation. To demonstrate this method we <span class="hlt">shock-compress</span> the body-centred-cubic material tantalum—an important material for high-energy-density physics owing to its high <span class="hlt">shock</span> impedance and high X-ray opacity. Tantalum is also a material for which previous <span class="hlt">shock</span> <span class="hlt">compression</span> simulations and experiments have provided conflicting information about the dominant deformation mechanism. Our experiments reveal twinning and related lattice rotation occurring on the timescale of tens of picoseconds. In addition, despite the common association between twinning</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2010AAS...21541525K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2010AAS...21541525K"><span>Galactic Spiral <span class="hlt">Shocks</span> with Thermal Instability in Vertically Stratified Disks</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Kim, Chang-Goo; Kim, W.; Ostriker, E. C.</p> <p>2010-01-01</p> <p>Galactic spiral <span class="hlt">shocks</span> are dominant morphological features and believed to be responsible for substructure formation of spiral arms in disk galaxies. They can also provide a large amount of kinetic energy for the interstellar gas by tapping the rotational energy. We use numerical hydrodynamic simulations to investigate dynamics and structure of spiral <span class="hlt">shocks</span> with thermal instability in vertically stratified galactic disks. We initially consider an isothermal disk in vertical hydrostatic equilibrium and let it evolve under interstellar cooling and heating. Due to cooling and heating, the disk rapidly turns to a dense slab near the midplane surrounded by rarefied gas at high-altitude regions. The imposed stellar spiral potential develops a vertically curved <span class="hlt">shock</span> that exhibits strong flapping motions along the direction perpendicular to the arm. The flows across the spiral <span class="hlt">shock</span> are characterized by transitions from rarefied to dense phases at the <span class="hlt">shock</span> and from dense to rarefied phases at the postshock expansion zone. The <span class="hlt">shock</span> flapping motions stirs the disk, supplying the gas with random kinetic energy. For a model resembling the galactic disk near the solar neighborhood, the density-weighted vertical velocity dispersions are 2 km/s for the rarefied gas and 1 km/s for the dense gas. The <span class="hlt">shock</span> <span class="hlt">compression</span> in this model reduces an amount of the rarefied gas from 29% to 19% by mass. Despite the flapping motions, the time-averaged profiles of surface density are similar to those of the one-dimensional counterparts, and the vertical density distribution is overall consistent with effective hydrostatic equilibrium. When self-gravity is included, the <span class="hlt">shock</span> <span class="hlt">compression</span> forms large gravitationally bound condensations with virial ratio of about 2 and typical masses of 0.5 to one million solar masses, comparable to the Jeans mass.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2012AIPC.1426..442C','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2012AIPC.1426..442C"><span>Index of refraction measurements and window corrections for PMMA under <span class="hlt">shock</span> <span class="hlt">compression</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Chapman, David James; Eakins, Daniel E.; Williamson, David Martin; Proud, William</p> <p>2012-03-01</p> <p>Symmetric plate impact experiments were performed to investigate the change in the refractive index of Polymethylmethacrylate (PMMA) under <span class="hlt">shock</span> loading. Flyer and target geometries allowed the measurement of <span class="hlt">shock</span> velocity, particle velocity, and refractive index in the <span class="hlt">shocked</span> state, using a Het-V system (1550 nm). The change in refractive index of PMMA as a function of density is generally considered to be well described by the Gladstone-Dale relationship, meaning that the "apparent" velocity measured by a laser velocity interferometer is the "true" velocity, and hence there is no window correction. The results presented here demonstrate that the behaviour of PMMA deviates from an ideal Gladstone-Dale description, requiring a small velocity correction of order 1% at peak stresses up to 1.9 GPa. These results are consistent with literature values measured using a wavelength of 632.8 nm by [1].</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017APS..DFD.L2001D','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017APS..DFD.L2001D"><span>Simulating <span class="hlt">compressible</span>-incompressible two-phase flows</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Denner, Fabian; van Wachem, Berend</p> <p>2017-11-01</p> <p>Simulating <span class="hlt">compressible</span> gas-liquid flows, e.g. air-water flows, presents considerable numerical issues and requires substantial computational resources, particularly because of the stiff equation of state for the liquid and the different Mach number regimes. Treating the liquid phase (low Mach number) as incompressible, yet concurrently considering the gas phase (high Mach number) as <span class="hlt">compressible</span>, can improve the computational performance of such simulations significantly without sacrificing important physical mechanisms. A pressure-based algorithm for the simulation of two-phase flows is presented, in which a <span class="hlt">compressible</span> and an incompressible fluid are separated by a sharp interface. The algorithm is based on a coupled finite-volume framework, discretised in conservative form, with a <span class="hlt">compressive</span> VOF method to represent the interface. The bulk phases are coupled via a novel acoustically-conservative interface discretisation method that retains the acoustic properties of the <span class="hlt">compressible</span> phase and does not require a Riemann solver. Representative test cases are presented to scrutinize the proposed algorithm, including the reflection of acoustic waves at the <span class="hlt">compressible</span>-incompressible interface, <span class="hlt">shock</span>-drop interaction and gas-liquid flows with surface tension. Financial support from the EPSRC (Grant EP/M021556/1) is gratefully acknowledged.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/29629250','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/29629250"><span>Factors Affecting the Geo-effectiveness of <span class="hlt">Shocks</span> and Sheaths at 1 AU.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Lugaz, N; Farrugia, C J; Winslow, R M; Al-Haddad, N; Kilpua, E K J; Riley, P</p> <p>2016-11-01</p> <p>We identify all fast-mode forward <span class="hlt">shocks</span>, whose sheath regions resulted in a moderate (56 cases) or intense (38 cases) geomagnetic storm during 18.5 years from January 1997 to June 2015. We study their main properties, interplanetary causes and geo-effects. We find that half (49/94) such <span class="hlt">shocks</span> are associated with interacting coronal mass ejections (CMEs), as they are either <span class="hlt">shocks</span> propagating into a preceding CME (35 cases) or a <span class="hlt">shock</span> propagating into the sheath region of a preceding <span class="hlt">shock</span> (14 cases). About half (22/45) of the <span class="hlt">shocks</span> driven by isolated transients and which have geo-effective sheaths <span class="hlt">compress</span> pre-existing southward B z . Most of the remaining sheaths appear to have planar structures with southward magnetic fields, including some with planar structures consistent with field line draping ahead of the magnetic ejecta. A typical (median) geo-effective <span class="hlt">shock</span>-sheath structure drives a geomagnetic storm with peak Dst of -88 nT, pushes the subsolar magnetopause location to 6.3 R E , i.e. below geosynchronous orbit and is associated with substorms with a peak AL-index of -1350 nT. There are some important differences between sheaths associated with CME-CME interaction (stronger storms) and those associated with isolated CMEs (stronger <span class="hlt">compression</span> of the magnetosphere). We detail six case studies of different types of geo-effective <span class="hlt">shock</span>-sheaths, as well as two events for which there was no geomagnetic storm but other magnetospheric effects. Finally, we discuss our results in terms of space weather forecasting, and potential effects on Earth's radiation belts.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5882492','PMC'); return false;" href="https://www.pubmedcentral.nih.gov/articlerender.fcgi?tool=pmcentrez&artid=5882492"><span>Factors Affecting the Geo-effectiveness of <span class="hlt">Shocks</span> and Sheaths at 1 AU</span></a></p> <p><a target="_blank" href="http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pmc">PubMed Central</a></p> <p>Lugaz, N.; Farrugia, C. J.; Winslow, R. M.; Al-Haddad, N.; Kilpua, E. K. J.; Riley, P.</p> <p>2018-01-01</p> <p>We identify all fast-mode forward <span class="hlt">shocks</span>, whose sheath regions resulted in a moderate (56 cases) or intense (38 cases) geomagnetic storm during 18.5 years from January 1997 to June 2015. We study their main properties, interplanetary causes and geo-effects. We find that half (49/94) such <span class="hlt">shocks</span> are associated with interacting coronal mass ejections (CMEs), as they are either <span class="hlt">shocks</span> propagating into a preceding CME (35 cases) or a <span class="hlt">shock</span> propagating into the sheath region of a preceding <span class="hlt">shock</span> (14 cases). About half (22/45) of the <span class="hlt">shocks</span> driven by isolated transients and which have geo-effective sheaths <span class="hlt">compress</span> pre-existing southward Bz. Most of the remaining sheaths appear to have planar structures with southward magnetic fields, including some with planar structures consistent with field line draping ahead of the magnetic ejecta. A typical (median) geo-effective <span class="hlt">shock</span>-sheath structure drives a geomagnetic storm with peak Dst of −88 nT, pushes the subsolar magnetopause location to 6.3 RE, i.e. below geosynchronous orbit and is associated with substorms with a peak AL-index of −1350 nT. There are some important differences between sheaths associated with CME-CME interaction (stronger storms) and those associated with isolated CMEs (stronger <span class="hlt">compression</span> of the magnetosphere). We detail six case studies of different types of geo-effective <span class="hlt">shock</span>-sheaths, as well as two events for which there was no geomagnetic storm but other magnetospheric effects. Finally, we discuss our results in terms of space weather forecasting, and potential effects on Earth’s radiation belts. PMID:29629250</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/16090745','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/16090745"><span><span class="hlt">Shock</span> wave interaction with laser-generated single bubbles.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Sankin, G N; Simmons, W N; Zhu, S L; Zhong, P</p> <p>2005-07-15</p> <p>The interaction of a lithotripter <span class="hlt">shock</span> wave (LSW) with laser-generated single vapor bubbles in water is investigated using high-speed photography and pressure measurement via a fiber-optic probe hydrophone. The interaction leads to nonspherical collapse of the bubble with secondary <span class="hlt">shock</span> wave emission and microjet formation along the LSW propagation direction. The maximum pressure amplification is produced during the collapse phase of the bubble oscillation when the <span class="hlt">compressive</span> pulse duration of the LSW matches with the forced collapse time of the bubble.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2013APS..SHK.K2005X','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2013APS..SHK.K2005X"><span>A new method to study he effective shear modulus of <span class="hlt">shocked</span> material</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Xiaojuan, Ma; Fusheng, Liu</p> <p>2013-06-01</p> <p>Shear modulus is a crucial material parameter for description of mechanical behavior. However, at strong <span class="hlt">shock</span> <span class="hlt">compression</span>, it is generally deduced from the longitudinal and bulk sound velocity evaluated by unloading wave profile measurement. Here, a new method called the disturbed amplitude damping method of <span class="hlt">shock</span> wave is presented, that can directly measure the shear modulus of material. This method relies on the correlation between the shear modulus of <span class="hlt">shock</span> <span class="hlt">compressed</span> state and amplitude damping and oscillation of an initial sinusoidal disturbance on <span class="hlt">shock</span> front in concerned substance. Two important steps are required to determine the shear modulus of material. The first is to measure the damping and oscillation feature of disturbance by the flyer impacted method. The second is to find the quantitative relationship between the disturbed amplitude damping and shear modulus by the finite difference method which is applied to obtain the numerical solutions for disturbance amplitude damping behavior of sinusoidal <span class="hlt">shock</span> front in flyer impacted flow field. When aluminum <span class="hlt">shocked</span> to 80 GPa is taken as an example, the shape of perturbed <span class="hlt">shock</span> front and its disturbed amplitude development with propagation distance, are approximately mapped out. The figure shows an oscillatory damping characteristic. At the early stage the perturbation amplitude on the <span class="hlt">shock</span> front experiences a decaying process until to zero point, then it rises to a maximum but in reverse phase, and then it decays again. Comparing these data with those simulated using the SCG constitutive model, the effective shear modulus for aluminum <span class="hlt">shocked</span> to 80 GPa is determined to be about 90 GPa, which is higher than the result given by Yu.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017APS..SHK.G1001D','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017APS..SHK.G1001D"><span>In situ insights into <span class="hlt">shock</span>-driven reactive flow</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Dattelbaum, Dana</p> <p>2017-06-01</p> <p><span class="hlt">Shock</span>-driven reactions are commonplace. Examples include the detonation of high explosives, <span class="hlt">shock</span>-driven dissociation of polymers, and transformation of carbon from graphite to diamond phases. The study of <span class="hlt">shock</span>-driven chemical reactions is important for understanding reaction thresholds, their mechanisms and rates, and associated state sensitivities under the extreme conditions generated by <span class="hlt">shock</span> <span class="hlt">compression</span>. Reactions are distinguished by their thermicity - e.g. the volume and enthalpy changes along the reaction coordinate. A survey of the hallmarks of <span class="hlt">shock</span>-driven reactivity for a variety of simple molecules and polymers will be presented, including benzene, acetylenes and nitriles, and formic acid. Many of the examples will illustrate the nature of the reactive flow through particle velocity wave profiles measured by in situ electromagnetic gauging in gas gun-driven plate impact experiments. General trends will be presented linking molecular moieties, <span class="hlt">shock</span> temperatures, and reaction state sensitivities. Progress in applying bond-specific diagnostics will also be presented, including time-resolved Raman spectroscopy, and recent results of in situ x-ray diffraction of carbon at the Linac Coherent Light Souce (LCLS) free electron laser.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017APS..SHK.K6001H','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017APS..SHK.K6001H"><span>Measurements of the <span class="hlt">Shock</span> Release Of Quartz and Paralyene-N</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Hawreliak, James; Karasik, Max; Oh, Jaechul; Aglitskiy, Yefim</p> <p>2017-06-01</p> <p>The <span class="hlt">shock</span> and release properties of Quartz and hydrocarbons are important to high energy density (HED) research and inertial confinement fusion (ICF) science. The bulk of HED material research studies single <span class="hlt">shock</span> or multiple <span class="hlt">shock</span> conditions. The challenge with measuring release properties is unlike <span class="hlt">shocks</span> which have a single interface from which to measure the properties, the release establishes gradients in the sample. The streaked x-ray imaging capability of the NIKE laser allow the interface between quartz and CH to be measured during the release, giving measurements of the interface velocity and CH density. Here, we present experimental results from the NIKE laser where quartz and parylene-N are <span class="hlt">shock</span> <span class="hlt">compressed</span> to high pressure and temperature and the release state is measured through x-ray imaging. The <span class="hlt">shock</span> state is characterized by <span class="hlt">shock</span> front velocity measurements using VISAR and the release state is characterized by using side-on streaked x-ray radiography Work supported by DOE/NNSA.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1235267-ethane-xenon-mixtures-under-shock-conditions','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1235267-ethane-xenon-mixtures-under-shock-conditions"><span>Ethane-xenon mixtures under <span class="hlt">shock</span> conditions</span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>Magyar, Rudolph J.; Root, Seth; Mattsson, Thomas; ...</p> <p>2015-04-22</p> <p>Mixtures of light elements with heavy elements are important in inertial confinement fusion. We explore the physics of molecular scale mixing through a validation study of equation of state (EOS) properties. Density functional theory molecular dynamics (DFT-MD) at elevated temperature and pressure is used to obtain the thermodynamic state properties of pure xenon, ethane, and various <span class="hlt">compressed</span> mixture compositions along their principal Hugoniots. In order to validate these simulations, we have performed <span class="hlt">shock</span> <span class="hlt">compression</span> experiments using the Sandia Z-Machine. A bond tracking analysis correlates the sharp rise in the Hugoniot curve with the completion of dissociation in ethane. Furthermore, themore » DFT-based simulation results compare well with the experimental data along the principal Hugoniots and are used to provide insight into the dissociation and temperature along the Hugoniots as a function of mixture composition. Interestingly, we find that the <span class="hlt">compression</span> ratio for complete dissociation is similar for several compositions suggesting a limiting <span class="hlt">compression</span> for C-C bonded systems.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19720038719&hterms=shock+elastic&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D40%26Ntt%3Dshock%2Belastic','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19720038719&hterms=shock+elastic&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D40%26Ntt%3Dshock%2Belastic"><span>Factors affecting the thermal <span class="hlt">shock</span> behavior of yttria stabilized hafnia based graphite and tungsten composites.</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Lineback, L. D.; Manning, C. R.</p> <p>1971-01-01</p> <p>Hafnia-based composites containing either graphite or tungsten were investigated as rocket nozzle throat inserts in solid propellant rocket engines. The thermal <span class="hlt">shock</span> resistance of these materials is considered in terms of macroscopic thermal conductivity, thermal expansion, modulus of elasticity, and <span class="hlt">compressive</span> fracture stress. The effect of degree of hafnia stabilization, density, and graphite or tungsten content upon these parameters is discussed. The variation of the ratio of elastic modulus to <span class="hlt">compressive</span> fracture stress with density and its effect upon thermal <span class="hlt">shock</span> resistance of these materials are discussed in detail.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2010PhPl...17e2704L','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2010PhPl...17e2704L"><span>Gain curves and hydrodynamic modeling for <span class="hlt">shock</span> ignition</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Lafon, M.; Ribeyre, X.; Schurtz, G.</p> <p>2010-05-01</p> <p>Ignition of a precompressed thermonuclear fuel by means of a converging <span class="hlt">shock</span> is now considered as a credible scheme to obtain high gains for inertial fusion energy. This work aims at modeling the successive stages of the fuel time history, from <span class="hlt">compression</span> to final thermonuclear combustion, in order to provide the gain curves of <span class="hlt">shock</span> ignition (SI). The leading physical mechanism at work in SI is pressure amplification, at first by spherical convergence, and by collision with the <span class="hlt">shock</span> reflected at center during the stagnation process. These two effects are analyzed, and ignition conditions are provided as functions of the <span class="hlt">shock</span> pressure and implosion velocity. Ignition conditions are obtained from a non-isobaric fuel assembly, for which we present a gain model. The corresponding gain curves exhibit a significantly lower ignition threshold and higher target gains than conventional central ignition.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016APS..DFD.D5002K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016APS..DFD.D5002K"><span>Sensitivity of <span class="hlt">shock</span> boundary-layer interactions to weak geometric perturbations</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Kim, Ji Hoon; Eaton, John K.</p> <p>2016-11-01</p> <p><span class="hlt">Shock</span>-boundary layer interactions can be sensitive to small changes in the inlet flow and boundary conditions. Robust computational models must capture this sensitivity, and validation of such models requires a suitable experimental database with well-defined inlet and boundary conditions. To that end, the purpose of this experiment is to systematically document the effects of small geometric perturbations on a SBLI flow to investigate the flow physics and establish an experimental dataset tailored for CFD validation. The facility used is a Mach 2.1, continuous operation wind tunnel. The SBLI is generated using a <span class="hlt">compression</span> wedge; the region of interest is the resulting reflected <span class="hlt">shock</span> SBLI. The geometric perturbations, which are small spanwise rectangular prisms, are introduced ahead of the <span class="hlt">compression</span> ramp on the opposite wall. PIV is used to study the SBLI for 40 different perturbation geometries. Results show that the dominant effect of the perturbations is a global shift of the SBLI itself. In addition, the bumps introduce weaker <span class="hlt">shocks</span> of varying strength and angles, depending on the bump height and location. Various scalar validation metrics, including a measure of <span class="hlt">shock</span> unsteadiness, and their uncertainties are also computed to better facilitate CFD validation. Ji Hoon Kim is supported by an OTR Stanford Graduate Fellowship.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19980235999&hterms=acm&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D50%26Ntt%3Dacm','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19980235999&hterms=acm&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D50%26Ntt%3Dacm"><span>Low Dissipative High Order <span class="hlt">Shock</span>-Capturing Methods Using Characteristic-Based Filters</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Yee, H. C.; Sandham, N. D.; Djomehri, M. J.</p> <p>1998-01-01</p> <p>An approach which closely maintains the non-dissipative nature of classical fourth or higher- order spatial differencing away from <span class="hlt">shock</span> waves and steep gradient regions while being capable of accurately capturing discontinuities, steep gradient and fine scale turbulent structures in a stable and efficient manner is described. The approach is a generalization of the method of Gustafsson and Oisson and the artificial <span class="hlt">compression</span> method (ACM) of Harten. Spatially non-dissipative fourth or higher-order compact and non-compact spatial differencings are used as the base schemes. Instead of applying a scalar filter as in Gustafsson and Olsson, an ACM like term is used to signal the appropriate amount of second or third-order TVD or ENO types of characteristic based numerical dissipation. This term acts as a characteristic filter to minimize numerical dissipation for the overall scheme. For time-accurate computations, time discretizations with low dissipation are used. Numerical experiments on 2-D vortical flows, vortex-<span class="hlt">shock</span> interactions and <span class="hlt">compressible</span> spatially and temporally evolving mixing layers showed that the proposed schemes have the desired property with only a 10% increase in operations count over standard second-order TVD schemes. Aside from the ability to accurately capture <span class="hlt">shock</span>-turbulence interaction flows, this approach is also capable of accurately preserving vortex convection. Higher accuracy is achieved with fewer grid points when compared to that of standard second-order TVD or ENO schemes. To demonstrate the applicability of these schemes in sustaining turbulence where <span class="hlt">shock</span> waves are absent, a simulation of 3-D <span class="hlt">compressible</span> turbulent channel flow in a small domain is conducted.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19980201047','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19980201047"><span>Low Dissipative High Order <span class="hlt">Shock</span>-Capturing Methods using Characteristic-Based Filters</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Yee, H. C.; Sandham, N. D.; Djomehri, M. J.</p> <p>1998-01-01</p> <p>An approach which closely maintains the non-dissipative nature of classical fourth or higher- order spatial differencing away from <span class="hlt">shock</span> waves and steep gradient regions while being capable of accurately capturing discontinuities, steep gradient and fine scale turbulent structures in a stable and efficient manner is described. The approach is a generalization of the method of Gustafsson and Olsson and the artificial <span class="hlt">compression</span> method (ACM) of Harten. Spatially non-dissipative fourth or higher-order compact and non-compact spatial differencings are used as the base schemes. Instead of applying a scalar filter as in Gustafsson and Olsson, an ACM like term is used to signal the appropriate amount of second or third-order TVD or ENO types of characteristic based numerical dissipation. This term acts as a characteristic filter to minimize numerical dissipation for the overall scheme. For time-accurate computations, time discretizations with low dissipation are used. Numerical experiments on 2-D vortical flows, vortex-<span class="hlt">shock</span> interactions and <span class="hlt">compressible</span> spatially and temporally evolving mixing layers showed that the proposed schemes have the desired property with only a 10% increase in operations count over standard second-order TVD schemes. Aside from the ability to accurately capture <span class="hlt">shock</span>-turbulence interaction flows, this approach is also capable of accurately preserving vortex convection. Higher accuracy is achieved with fewer grid points when compared to that of standard second-order TVD or ENO schemes. To demonstrate the applicability of these schemes in sustaining turbulence where <span class="hlt">shock</span> waves are absent, a simulation of 3-D <span class="hlt">compressible</span> turbulent channel flow in a small domain is conducted.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_20");'>20</a></li> <li><a href="#" onclick='return showDiv("page_21");'>21</a></li> <li class="active"><span>22</span></li> <li><a href="#" onclick='return showDiv("page_23");'>23</a></li> <li><a href="#" onclick='return showDiv("page_24");'>24</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_22 --> <div id="page_23" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_21");'>21</a></li> <li><a href="#" onclick='return showDiv("page_22");'>22</a></li> <li class="active"><span>23</span></li> <li><a href="#" onclick='return showDiv("page_24");'>24</a></li> <li><a href="#" onclick='return showDiv("page_25");'>25</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="441"> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.loc.gov/pictures/collection/hh/item/al1087.photos.046808p/','SCIGOV-HHH'); return false;" href="https://www.loc.gov/pictures/collection/hh/item/al1087.photos.046808p/"><span>33. BENCH CORE STATION, GREY <span class="hlt">IRON</span> FOUNDRY CORE ROOM WHERE ...</span></a></p> <p><a target="_blank" href="http://www.loc.gov/pictures/collection/hh/">Library of Congress Historic Buildings Survey, Historic Engineering Record, Historic Landscapes Survey</a></p> <p></p> <p></p> <p>33. BENCH CORE STATION, GREY <span class="hlt">IRON</span> FOUNDRY CORE ROOM WHERE CORE MOLDS WERE HAND FILLED AND OFTEN PNEUMATICALLY <span class="hlt">COMPRESSED</span> WITH A HAND-HELD RAMMER BEFORE THEY WERE BAKED. - Stockham Pipe & Fittings Company, Grey <span class="hlt">Iron</span> Foundry, 4000 Tenth Avenue North, Birmingham, Jefferson County, AL</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19830025957','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19830025957"><span>Iterative spectral methods and spectral solutions to <span class="hlt">compressible</span> flows</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Hussaini, M. Y.; Zang, T. A.</p> <p>1982-01-01</p> <p>A spectral multigrid scheme is described which can solve pseudospectral discretizations of self-adjoint elliptic problems in O(N log N) operations. An iterative technique for efficiently implementing semi-implicit time-stepping for pseudospectral discretizations of Navier-Stokes equations is discussed. This approach can handle variable coefficient terms in an effective manner. Pseudospectral solutions of <span class="hlt">compressible</span> flow problems are presented. These include one dimensional problems and two dimensional Euler solutions. Results are given both for <span class="hlt">shock</span>-capturing approaches and for <span class="hlt">shock</span>-fitting ones.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017PhRvL.118l5101G','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017PhRvL.118l5101G"><span>Role of Magnetosonic Solitons in Perpendicular Collisionless <span class="hlt">Shock</span> Reformation</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Gueroult, Renaud; Ohsawa, Yukiharu; Fisch, Nathaniel J.</p> <p>2017-03-01</p> <p>The nature of the magnetic structure arising from ion specular reflection in <span class="hlt">shock</span> <span class="hlt">compression</span> studies is examined by means of 1D particle-in-cell simulations. Propagation speed, field profiles, and supporting currents for this magnetic structure are shown to be consistent with a magnetosonic soliton. Coincidentally, this structure and its evolution are typical of foot structures observed in perpendicular <span class="hlt">shock</span> reformation. To reconcile these two observations, we propose, for the first time, that <span class="hlt">shock</span> reformation can be explained as the result of the formation, growth, and subsequent transition to a supercritical <span class="hlt">shock</span> of a magnetosonic soliton. This argument is further supported by the remarkable agreement found between the period of the soliton evolution cycle and classical reformation results. This new result suggests that the unique properties of solitons can be used to shed new light on the long-standing issue of <span class="hlt">shock</span> nonstationarity and its role on particle acceleration.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2014AGUFMMR31A4318T','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2014AGUFMMR31A4318T"><span><span class="hlt">Compression</span> of Fe-Si-H alloys</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Tagawa, S.; Ohta, K.; Hirose, K.</p> <p>2014-12-01</p> <p>The light elements in the Earth's core have not been fully identified yet, but hydrogen is now collecting more attention in part because recent planet formation theory suggests that large amount of water should have been brought to the Earth during its formation (giant-impact stage). Nevertheless, the effect of hydrogen on the property of <span class="hlt">iron</span> alloys is little known so far. The earlier experimental study by Hirao et al. [2004 GRL] examined the <span class="hlt">compression</span> behavior of dhcp FeHx (x ≈ 1) and found that it becomes much stiffer than pure <span class="hlt">iron</span> above 50 GPa, where magnetization disappears. Here we examined the solubility of hydrogen into <span class="hlt">iron</span>-rich Fe-Si alloys and the <span class="hlt">compression</span> behavior of dhcp Fe-Si-H alloy at room temperature. Fe+6.5wt.%Si or Fe+9wt.%Si foil was loaded into a diamond-anvil cell (DAC), and then liquid hydrogen was introduced at temperatures below 20 K. X-ray diffraction measurements at SPring-8 revealed the formation of a dhcp phase with or without thermal annealing by laser above 8.4 GPa. The concentration of hydrogen in such dhcp lattice was calculated following the formula reported by Fukai [1992]; y = 0.5 and 0.2 for Fe-6.5wt.%Si-H or Fe-9wt.%Si-H alloys, respectively when y is defined as Fe(1-x)SixHy. Unlike Fe-H alloy, hydrogen didn't fully occupy the octahedral sites even under hydrogen-saturated conditions in the case of Fe-Si-H system. Anomaly was observed in obtained pressure-volume curve around 44 Å3 of unit-cell volume for both Fe-6.5wt.%Si-H and Fe-9wt.%Si-H alloys, which may be related to the spin transition in the dhcp phase. They became slightly stiffer at higher pressures, but their <span class="hlt">compressibility</span> was still similar to that of pure <span class="hlt">iron</span>.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/26382524','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/26382524"><span>Passage of a <span class="hlt">shock</span> wave through inhomogeneous media and its impact on gas-bubble deformation.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Nowakowski, A F; Ballil, A; Nicolleau, F C G A</p> <p>2015-08-01</p> <p>The paper investigates <span class="hlt">shock</span>-induced vortical flows within inhomogeneous media of nonuniform thermodynamic properties. Numerical simulations are performed using a Eulerian type mathematical model for <span class="hlt">compressible</span> multicomponent flow problems. The model, which accounts for pressure nonequilibrium and applies different equations of state for individual flow components, shows excellent capabilities for the resolution of interfaces separating <span class="hlt">compressible</span> fluids as well as for capturing the baroclinic source of vorticity generation. The developed finite volume Godunov type computational approach is equipped with an approximate Riemann solver for calculating fluxes and handles numerically diffused zones at flow component interfaces. The computations are performed for various initial conditions and are compared with available experimental data. The initial conditions promoting a <span class="hlt">shock</span>-bubble interaction process include weak to high planar <span class="hlt">shock</span> waves with a Mach number ranging from 1.2 to 3 and isolated cylindrical bubble inhomogeneities of helium, argon, nitrogen, krypton, and sulphur hexafluoride. The numerical results reveal the characteristic features of the evolving flow topology. The impulsively generated flow perturbations are dominated by the reflection and refraction of the <span class="hlt">shock</span>, the <span class="hlt">compression</span>, and acceleration as well as the vorticity generation within the medium. The study is further extended to investigate the influence of the ratio of the heat capacities on the interface deformation.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2000SPIE.3989..266G','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2000SPIE.3989..266G"><span>Magneto-rheological fluid <span class="hlt">shock</span> absorbers for HMMWV</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Gordaninejad, Faramarz; Kelso, Shawn P.</p> <p>2000-04-01</p> <p>This paper presents the development and evaluation of a controllable, semi-active magneto-rheological fluid (MRF) <span class="hlt">shock</span> absorber for a High Mobility Multi-purpose Wheeled Vehicle (HMMWV). The University of Nevada, Reno (UNR) MRF damper is tailored for structures and ground vehicles that undergo a wide range of dynamic loading. It also has the capability for unique rebound and <span class="hlt">compression</span> characteristics. The new MRF <span class="hlt">shock</span> absorber emulates the original equipment manufacturer (OEM) <span class="hlt">shock</span> absorber behavior in passive mode, and provides a wide controllable damping force range. A theoretical study is performed to evaluate the UNR MRF <span class="hlt">shock</span> absorber. The Bingham plastic theory is employed to model the nonlinear behavior of the MR fluid. A fluid-mechanics-based theoretical model along with a three-dimensional finite element electromagnetic analysis is utilized to predict the MRF damper performance. The theoretical results are compared with experimental data and are demonstrated to be in excellent agreement.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2013JAP...114l3509X','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2013JAP...114l3509X"><span>Molecular dynamics studies of thermal dissipation during <span class="hlt">shock</span> induced spalling</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Xiang, Meizhen; Hu, Haibo; Chen, Jun; Liao, Yi</p> <p>2013-09-01</p> <p>Under <span class="hlt">shock</span> loadings, the temperature of materials may vary dramatically during deformation and fracture processes. Thus, thermal effect is important for constructing dynamical failure models. Existing works on thermal dissipation effects are mostly from meso- to macro-scale levels based on phenomenological assumptions. The main purpose of the present work is to provide several atomistic scale perspectives about thermal dissipation during spall fracture by nonequilibrium molecular dynamics simulations on single-crystalline and nanocrystalline Pb. The simulations show that temperature arising starts from the vicinity of voids during spalling. The thermal dissipation rate in void nucleation stage is much higher than that in the later growth and coalescence stages. Both classical spallation and micro-spallation are taken into account. Classical spallation is corresponding to spallation phenomenon where materials keep in solid state during <span class="hlt">shock</span> <span class="hlt">compression</span> and release stages, while micro-spallation is corresponding to spallation phenomenon where melting occurs during <span class="hlt">shock</span> <span class="hlt">compression</span> and release stages. In classical spallation, whether residuary dislocations are produced in pre-spall stages has significant influences on thermal dissipation rate during void growth and coalescence. The thermal dissipation rates decrease as <span class="hlt">shock</span> intensity increases. When the <span class="hlt">shock</span> intensity exceeds the threshold of micro-spallation, the thermal dissipation rate in void nucleation stage drops precipitously. It is found that grain boundaries mainly influence the thermal dissipation rate in void nucleation stage in classical spallation. In micro-spallation, the grain boundary effects are insignificant.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017APS..DPPPO5006D','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017APS..DPPPO5006D"><span>First-Principles Equation of State and <span class="hlt">Shock</span> <span class="hlt">Compression</span> of Warm Dense Aluminum and Hydrocarbons</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Driver, Kevin; Soubiran, Francois; Zhang, Shuai; Militzer, Burkhard</p> <p>2017-10-01</p> <p>Theoretical studies of warm dense plasmas are a key component of progress in fusion science, defense science, and astrophysics programs. Path integral Monte Carlo (PIMC) and density functional theory molecular dynamics (DFT-MD), two state-of-the-art, first-principles, electronic-structure simulation methods, provide a consistent description of plasmas over a wide range of density and temperature conditions. Here, we combine high-temperature PIMC data with lower-temperature DFT-MD data to compute coherent equations of state (EOS) for aluminum and hydrocarbon plasmas. Subsequently, we derive <span class="hlt">shock</span> Hugoniot curves from these EOSs and extract the temperature-density evolution of plasma structure and ionization behavior from pair-correlation function analyses. Since PIMC and DFT-MD accurately treat effects of atomic shell structure, we find <span class="hlt">compression</span> maxima along Hugoniot curves attributed to K-shell and L-shell ionization, which provide a benchmark for widely-used EOS tables, such as SESAME and LEOS, and more efficient models. LLNL-ABS-734424. Funding provided by the DOE (DE-SC0010517) and in part under the auspices of the U.S. Department of Energy by Lawrence Livermore National Laboratory under Contract DE-AC52-07NA27344. Computational resources provided by Blue Waters (NSF ACI1640776) and NERSC. K. Driver's and S. Zhang's current address is Lawrence Livermore Natl. Lab, Livermore, CA, 94550, USA.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1417591-nanometer-scale-characterization-laser-driven-compression-shocks-phase-transitions-ray-scattering-using-free-electron-lasers','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1417591-nanometer-scale-characterization-laser-driven-compression-shocks-phase-transitions-ray-scattering-using-free-electron-lasers"><span>Nanometer-scale characterization of laser-driven <span class="hlt">compression</span>, <span class="hlt">shocks</span>, and phase transitions, by x-ray scattering using free electron lasers</span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>Kluge, T.; Rödel, C.; Rödel, M.; ...</p> <p>2017-10-23</p> <p>In this paper, we study the feasibility of using small angle X-ray scattering (SAXS) as a new experimental diagnostic for intense laser-solid interactions. By using X-ray pulses from a hard X-ray free electron laser, we can simultaneously achieve nanometer and femtosecond resolution of laser-driven samples. This is an important new capability for the Helmholtz international beamline for extreme fields at the high energy density endstation currently built at the European X-ray free electron laser. We review the relevant SAXS theory and its application to transient processes in solid density plasmas and report on first experimental results that confirm the feasibilitymore » of the method. Finally, we present results of two test experiments where the first experiment employs ultra-short laser pulses for studying relativistic laser plasma interactions, and the second one focuses on <span class="hlt">shock</span> <span class="hlt">compression</span> studies with a nanosecond laser system.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/1417591-nanometer-scale-characterization-laser-driven-compression-shocks-phase-transitions-ray-scattering-using-free-electron-lasers','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/1417591-nanometer-scale-characterization-laser-driven-compression-shocks-phase-transitions-ray-scattering-using-free-electron-lasers"><span>Nanometer-scale characterization of laser-driven <span class="hlt">compression</span>, <span class="hlt">shocks</span>, and phase transitions, by x-ray scattering using free electron lasers</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Kluge, T.; Rödel, C.; Rödel, M.</p> <p></p> <p>In this paper, we study the feasibility of using small angle X-ray scattering (SAXS) as a new experimental diagnostic for intense laser-solid interactions. By using X-ray pulses from a hard X-ray free electron laser, we can simultaneously achieve nanometer and femtosecond resolution of laser-driven samples. This is an important new capability for the Helmholtz international beamline for extreme fields at the high energy density endstation currently built at the European X-ray free electron laser. We review the relevant SAXS theory and its application to transient processes in solid density plasmas and report on first experimental results that confirm the feasibilitymore » of the method. Finally, we present results of two test experiments where the first experiment employs ultra-short laser pulses for studying relativistic laser plasma interactions, and the second one focuses on <span class="hlt">shock</span> <span class="hlt">compression</span> studies with a nanosecond laser system.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2016APS..DFDG12002R','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2016APS..DFDG12002R"><span>A <span class="hlt">compressible</span> multiphase framework for simulating supersonic atomization</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Regele, Jonathan D.; Garrick, Daniel P.; Hosseinzadeh-Nik, Zahra; Aslani, Mohamad; Owkes, Mark</p> <p>2016-11-01</p> <p>The study of atomization in supersonic combustors is critical in designing efficient and high performance scramjets. Numerical methods incorporating surface tension effects have largely focused on the incompressible regime as most atomization applications occur at low Mach numbers. Simulating surface tension effects in high speed <span class="hlt">compressible</span> flow requires robust numerical methods that can handle discontinuities caused by both material interfaces and <span class="hlt">shocks</span>. A <span class="hlt">shock</span> capturing/diffused interface method is developed to simulate high-speed <span class="hlt">compressible</span> gas-liquid flows with surface tension effects using the five-equation model. This includes developments that account for the interfacial pressure jump that occurs in the presence of surface tension. A simple and efficient method for computing local interface curvature is developed and an acoustic non-dimensional scaling for the surface tension force is proposed. The method successfully captures a variety of droplet breakup modes over a range of Weber numbers and demonstrates the impact of surface tension in countering droplet deformation in both subsonic and supersonic cross flows.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/940747-effect-laser-shock-peening-life-failure-mode-cold-pilger-die','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/940747-effect-laser-shock-peening-life-failure-mode-cold-pilger-die"><span>THE EFFECT OF LASER <span class="hlt">SHOCK</span> PEENING ON THE LIFE AND FAILURE MODE OF A COLD PILGER DIE</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Lavender, Curt A.; Hong, Sung-tae; Smith, Mark T.</p> <p>2008-08-11</p> <p>The laser <span class="hlt">shock</span> peening process was used to increase fatigue life of pilger dies made of A2 tool steel by imparting <span class="hlt">compressive</span> residual stresses to fatigue prone areas of the dies. The result of X-Ray diffraction analysis indicated that deep, high- magnitude <span class="hlt">compressive</span> residual stresses were generated by the laser <span class="hlt">shock</span> peening process, and the peened dies exhibited a significant increase of in-service life. Fractography of the failed dies indicates that the fracture mechanism was altered by the peening process.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018PhRvB..97n0101T','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018PhRvB..97n0101T"><span>Multiple <span class="hlt">shock</span> reverberation <span class="hlt">compression</span> of dense Ne up to the warm dense regime: Evaluating the theoretical models</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Tang, J.; Gu, Y. J.; Chen, Q. F.; Li, Z. G.; Zheng, J.; Li, C. J.; Li, J. T.</p> <p>2018-04-01</p> <p>Multiple <span class="hlt">shock</span> reverberation <span class="hlt">compression</span> experiments are designed and performed to determine the equation of state of neon ranging from the initial dense gas up to the warm dense regime where the pressure is from about 40 MPa to 120 GPa and the temperature is from about 297 K up to above 20 000 K. The wide region experimental data are used to evaluate the available theoretical models. It is found that, for neon below 1.1 g/cm 3 , within the framework of density functional theory molecular dynamics, a van der Waals correction is meaningful. Under high pressure and temperature, results from the self-consistent fluid variational theory model are sensitive to the potential parameter and could give successful predictions in the whole experimental regime if a set of proper parameters is employed. The new observations on neon under megabar (1 Mbar =1011Pa ) pressure and eV temperature (1 eV ≈104K ) enrich the understanding on properties of warm dense matter and have potential applications in revealing the formation and evolution of gaseous giants or mega-Earths.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2013APS..DPPY10003A','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2013APS..DPPY10003A"><span><span class="hlt">Shock</span>-induced perturbation evolution in planar laser targets</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Aglitskiy, Y.; Karasik, M.; Velikovich, A. L.; Serlin, V.; Weaver, J. L.; Kessler, T. J.; Schmitt, A. J.; Obenschain, S. P.; Metzler, N.; Oh, J.</p> <p>2013-10-01</p> <p>Experimental studies of hydrodynamic perturbation evolution triggered by a laser-driven <span class="hlt">shock</span> wave in a planar target done on the KrF Nike laser facility are reported. The targets were made of solid plastic and/or plastic foam with single mode sinusoidal perturbation on the front or back surface or plastic/foam interface. Two specific cases are discussed. When a planar solid plastic target rippled at the front side is irradiated with a 350 ps long laser pulse, ablative Richtmyer-Meshkov (RM) oscillation of its areal mass modulation amplitude is detected while the laser is on, followed by observed strong oscillations of the areal mass in the unsupported <span class="hlt">shock</span> flow after the laser pulse ends. When the target is rippled at the rear side, the nature of the perturbation evolution after the <span class="hlt">shock</span> breakout is determined by the strength of the laser-driven <span class="hlt">shock</span> wave. At pressure below 1 Mbar <span class="hlt">shock</span> interaction with rear-surface ripples produces planar collimated jets manifesting the development of a classical RM instability in a weakly <span class="hlt">compressible</span> <span class="hlt">shocked</span> fluid. At <span class="hlt">shock</span> pressure ~ 8 Mbar sufficient for vaporizing the <span class="hlt">shocked</span> target material we observed instead the strong areal mass oscillations characteristic of a rippled centered rarefaction wave. Work supported by US DOE, Defense Programs.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19970023722','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19970023722"><span>FE Line Diagnostics of Multiply <span class="hlt">Shocked</span> Stellar Atmospheres: The Mira S. Carinae</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Bookbinder, Jay</p> <p>1997-01-01</p> <p>Extensive LWP-HI spectra were obtained of the Mira S Car at a rapid time cadence as compared with the <span class="hlt">shock</span> cycle time of S Car. These spectra were obtained in an attempt to understand the velocity structures in the <span class="hlt">shocked</span> wind using the fluoresced <span class="hlt">iron</span> lines. Data analysis of the IUE observations, which included the primary calibration of all of the IUE spectra obtained of S Car, was carried out. In addition, line identifications, flux calculations, background subtractions, and line profile analysis as a function of S Car's pulsational phase were performed. The database incorporated all line identifications as a function of pulsation phase for all IUE LWP-HI observations to date of S Car. At least 45 separate <span class="hlt">iron</span> line features are identified in the S Car spectrum at one or more phases of the <span class="hlt">shock</span> cycle, including those due to Fe II (UV 161) which is pumped by three different <span class="hlt">iron</span> lines; Fe I(UV 44) which is pumped by the Mg II k line. Other strong multiplets that have been identified include UV(1), UV(2), UV(5), UV(32), UV(60), UV(63), UV(161), UV(207), and UV(399). Over 300 weaker lines have also been tentatively identified with Fe line transitions.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1348971-behaviour-rippled-shocks-from-ablatively-driven-richtmyer-meshkov-metals-accounting-strength','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1348971-behaviour-rippled-shocks-from-ablatively-driven-richtmyer-meshkov-metals-accounting-strength"><span>Behaviour of rippled <span class="hlt">shocks</span> from ablatively-driven Richtmyer-Meshkov in metals accounting for strength</span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>Opie, S.; Gautam, S.; Fortin, E.; ...</p> <p>2016-05-26</p> <p>While numerous continuum material strength and phase transformation models have been proposed to capture their complex dependences on intensive properties and deformation history, few experimental methods are available to validate these models particularly in the large pressure and strain rate regime typical of strong <span class="hlt">shock</span> and ramp dynamic loading. In the experiments and simulations we present, a rippled <span class="hlt">shock</span> is created by laser-ablation of a periodic surface perturbation on a metal target. The strength of the <span class="hlt">shock</span> can be tuned to access phase transitions in metals such as <span class="hlt">iron</span> or simply to study high-pressure strength in isomorphic materials such asmore » copper. Simulations, with models calibrated and validated to the experiments, show that the evolution of the amplitude of imprinted perturbations on the back surface by the rippled <span class="hlt">shock</span> is strongly affected by strength and phase transformation kinetics. Increased strength has a smoothing effect on the perturbed <span class="hlt">shock</span> front profile resulting in smaller perturbations on the free surface. Lastly, in <span class="hlt">iron</span>, faster phase transformations kinetics had a similar effect as increased strength, leading to smoother pressure contours inside the samples and smaller amplitudes of free surface perturbations in our simulations.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1208837-imaging-shock-waves-diamond-both-high-temporal-spatial-resolution-xfel','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1208837-imaging-shock-waves-diamond-both-high-temporal-spatial-resolution-xfel"><span>Imaging <span class="hlt">shock</span> waves in diamond with both high temporal and spatial resolution at an XFEL</span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>Schropp, Andreas; Hoppe, Robert; Meier, Vivienne; ...</p> <p>2015-06-18</p> <p>The advent of hard x-ray free-electron lasers (XFELs) has opened up a variety of scientific opportunities in areas as diverse as atomic physics, plasma physics, nonlinear optics in the x-ray range, and protein crystallography. In this article, we access a new field of science by measuring quantitatively the local bulk properties and dynamics of matter under extreme conditions, in this case by using the short XFEL pulse to image an elastic <span class="hlt">compression</span> wave in diamond. The elastic wave was initiated by an intense optical laser pulse and was imaged at different delay times after the optical pump pulse using magnifiedmore » x-ray phase-contrast imaging. The temporal evolution of the <span class="hlt">shock</span> wave can be monitored, yielding detailed information on <span class="hlt">shock</span> dynamics, such as the <span class="hlt">shock</span> velocity, the <span class="hlt">shock</span> front width, and the local <span class="hlt">compression</span> of the material. The method provides a quantitative perspective on the state of matter in extreme conditions.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/26086176','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/26086176"><span>Imaging <span class="hlt">Shock</span> Waves in Diamond with Both High Temporal and Spatial Resolution at an XFEL.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Schropp, Andreas; Hoppe, Robert; Meier, Vivienne; Patommel, Jens; Seiboth, Frank; Ping, Yuan; Hicks, Damien G; Beckwith, Martha A; Collins, Gilbert W; Higginbotham, Andrew; Wark, Justin S; Lee, Hae Ja; Nagler, Bob; Galtier, Eric C; Arnold, Brice; Zastrau, Ulf; Hastings, Jerome B; Schroer, Christian G</p> <p>2015-06-18</p> <p>The advent of hard x-ray free-electron lasers (XFELs) has opened up a variety of scientific opportunities in areas as diverse as atomic physics, plasma physics, nonlinear optics in the x-ray range, and protein crystallography. In this article, we access a new field of science by measuring quantitatively the local bulk properties and dynamics of matter under extreme conditions, in this case by using the short XFEL pulse to image an elastic <span class="hlt">compression</span> wave in diamond. The elastic wave was initiated by an intense optical laser pulse and was imaged at different delay times after the optical pump pulse using magnified x-ray phase-contrast imaging. The temporal evolution of the <span class="hlt">shock</span> wave can be monitored, yielding detailed information on <span class="hlt">shock</span> dynamics, such as the <span class="hlt">shock</span> velocity, the <span class="hlt">shock</span> front width, and the local <span class="hlt">compression</span> of the material. The method provides a quantitative perspective on the state of matter in extreme conditions.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19870015001','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19870015001"><span>Calculation of external-internal flow fields for mixed-<span class="hlt">compression</span> inlets</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Chyu, W. J.; Kawamura, T.; Bencze, D. P.</p> <p>1986-01-01</p> <p>Supersonic inlet flows with mixed external-internal <span class="hlt">compressions</span> were computed using a combined implicit-explicit (Beam-Warming-Steger/MacCormack) method for solving the three-dimensional unsteady, <span class="hlt">compressible</span> Navier-Stokes equations in conservation form. Numerical calculations were made of various flows related to such inlet operations as the <span class="hlt">shock</span>-wave intersections, subsonic spillage around the cowl lip, and inlet started versus unstarted conditions. Some of the computed results were compared with wind tunnel data.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19880050126&hterms=Internal+External&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D40%26Ntt%3DInternal%2BExternal','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19880050126&hterms=Internal+External&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D40%26Ntt%3DInternal%2BExternal"><span>Calculation of external-internal flow fields for mixed-<span class="hlt">compression</span> inlets</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Chyu, W. J.; Kawamura, T.; Bencze, D. P.</p> <p>1987-01-01</p> <p>Supersonic inlet flows with mixed external-internal <span class="hlt">compressions</span> were computed using a combined implicit-explicit (Beam-Warming-Steger/MacCormack) method for solving the three-dimensional unsteady, <span class="hlt">compressible</span> Navier-Stokes equations in conservation form. Numerical calculations were made of various flows related to such inlet operations as the <span class="hlt">shock</span>-wave intersections, subsonic spillage around the cowl lip, and inlet started versus unstarted conditions. Some of the computed results were compared with wind tunnel data.</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_21");'>21</a></li> <li><a href="#" onclick='return showDiv("page_22");'>22</a></li> <li class="active"><span>23</span></li> <li><a href="#" onclick='return showDiv("page_24");'>24</a></li> <li><a href="#" onclick='return showDiv("page_25");'>25</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_23 --> <div id="page_24" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_21");'>21</a></li> <li><a href="#" onclick='return showDiv("page_22");'>22</a></li> <li><a href="#" onclick='return showDiv("page_23");'>23</a></li> <li class="active"><span>24</span></li> <li><a href="#" onclick='return showDiv("page_25");'>25</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="461"> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/26764625','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/26764625"><span>Entropic lattice Boltzmann model for <span class="hlt">compressible</span> flows.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Frapolli, N; Chikatamarla, S S; Karlin, I V</p> <p>2015-12-01</p> <p>We present a lattice Boltzmann model (LBM) that covers the entire range of fluid flows, from low Mach weakly <span class="hlt">compressible</span> to transonic and supersonic flows. One of the most restrictive limitations of the lattice Boltzmann method, the low Mach number limit, is overcome here by three fundamental changes to the LBM scheme: use of an appropriately chosen multispeed lattice, accurate evaluation of the equilibrium, and the entropic relaxation for the collision. The range of applications is demonstrated through the simulation of a bow <span class="hlt">shock</span> in front of an airfoil and the simulation of decaying <span class="hlt">compressible</span> turbulence with shocklets.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/17928216','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/17928216"><span>Reuse of waste <span class="hlt">iron</span> as a partial replacement of sand in concrete.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Ismail, Zainab Z; Al-Hashmi, Enas A</p> <p>2008-11-01</p> <p>One of the major environmental issues in Iraq is the large quantity of waste <span class="hlt">iron</span> resulting from the industrial sector which is deposited in domestic waste and in landfills. A series of 109 experiments and 586 tests were carried out in this study to examine the feasibility of reusing this waste <span class="hlt">iron</span> in concrete. Overall, 130 kg of waste <span class="hlt">iron</span> were reused to partially replace sand at 10%, 15%, and 20% in a total of 1703 kg concrete mixtures. The tests performed to evaluate waste-<span class="hlt">iron</span> concrete quality included slump, fresh density, dry density, <span class="hlt">compressive</span> strength, and flexural strength tests: 115 cubes of concrete were molded for the <span class="hlt">compressive</span> strength and dry density tests, and 87 prisms were cast for the flexural strength tests. This work applied 3, 7, 14, and 28 days curing ages for the concrete mixes. The results confirm that reuse of solid waste material offers an approach to solving the pollution problems that arise from an accumulation of waste in a production site; in the meantime modified properties are added to the concrete. The results show that the concrete mixes made with waste <span class="hlt">iron</span> had higher <span class="hlt">compressive</span> strengths and flexural strengths than the plain concrete mixes.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1352360-verification-assessment-piston-boundary-conditions-lagrangian-simulation-compressible-flow-similarity-solutions','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1352360-verification-assessment-piston-boundary-conditions-lagrangian-simulation-compressible-flow-similarity-solutions"><span>Verification assessment of piston boundary conditions for Lagrangian simulation of <span class="hlt">compressible</span> flow similarity solutions</span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>Ramsey, Scott D.; Ivancic, Philip R.; Lilieholm, Jennifer F.</p> <p>2015-12-10</p> <p>This work is concerned with the use of similarity solutions of the <span class="hlt">compressible</span> flow equations as benchmarks or verification test problems for finite-volume <span class="hlt">compressible</span> flow simulation software. In practice, this effort can be complicated by the infinite spatial/temporal extent of many candidate solutions or “test problems.” Methods can be devised with the intention of ameliorating this inconsistency with the finite nature of computational simulation; the exact strategy will depend on the code and problem archetypes under investigation. For example, self-similar <span class="hlt">shock</span> wave propagation can be represented in Lagrangian <span class="hlt">compressible</span> flow simulations as rigid boundary-driven flow, even if no such “piston”more » is present in the counterpart mathematical similarity solution. The purpose of this work is to investigate in detail the methodology of representing self-similar <span class="hlt">shock</span> wave propagation as a piston-driven flow in the context of various test problems featuring simple closed-form solutions of infinite spatial/temporal extent. The closed-form solutions allow for the derivation of similarly closed-form piston boundary conditions (BCs) for use in Lagrangian <span class="hlt">compressible</span> flow solvers. Finally, the consequences of utilizing these BCs (as opposed to directly initializing the self-similar solution in a computational spatial grid) are investigated in terms of common code verification analysis metrics (e.g., <span class="hlt">shock</span> strength/position errors and global convergence rates).« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/1352360','SCIGOV-STC'); return false;" href="https://www.osti.gov/servlets/purl/1352360"><span>Verification assessment of piston boundary conditions for Lagrangian simulation of <span class="hlt">compressible</span> flow similarity solutions</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Ramsey, Scott D.; Ivancic, Philip R.; Lilieholm, Jennifer F.</p> <p></p> <p>This work is concerned with the use of similarity solutions of the <span class="hlt">compressible</span> flow equations as benchmarks or verification test problems for finite-volume <span class="hlt">compressible</span> flow simulation software. In practice, this effort can be complicated by the infinite spatial/temporal extent of many candidate solutions or “test problems.” Methods can be devised with the intention of ameliorating this inconsistency with the finite nature of computational simulation; the exact strategy will depend on the code and problem archetypes under investigation. For example, self-similar <span class="hlt">shock</span> wave propagation can be represented in Lagrangian <span class="hlt">compressible</span> flow simulations as rigid boundary-driven flow, even if no such “piston”more » is present in the counterpart mathematical similarity solution. The purpose of this work is to investigate in detail the methodology of representing self-similar <span class="hlt">shock</span> wave propagation as a piston-driven flow in the context of various test problems featuring simple closed-form solutions of infinite spatial/temporal extent. The closed-form solutions allow for the derivation of similarly closed-form piston boundary conditions (BCs) for use in Lagrangian <span class="hlt">compressible</span> flow solvers. Finally, the consequences of utilizing these BCs (as opposed to directly initializing the self-similar solution in a computational spatial grid) are investigated in terms of common code verification analysis metrics (e.g., <span class="hlt">shock</span> strength/position errors and global convergence rates).« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018ApJ...858...95G','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018ApJ...858...95G"><span>Electron Heating in Low Mach Number Perpendicular <span class="hlt">Shocks</span>. II. Dependence on the Pre-<span class="hlt">shock</span> Conditions</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Guo, Xinyi; Sironi, Lorenzo; Narayan, Ramesh</p> <p>2018-05-01</p> <p>Recent X-ray observations of merger <span class="hlt">shocks</span> in galaxy clusters have shown that the post-<span class="hlt">shock</span> plasma is two-temperature, with the protons being hotter than the electrons. In this work, the second of a series, we investigate the efficiency of irreversible electron heating in perpendicular low Mach number <span class="hlt">shocks</span>, by means of two-dimensional particle-in-cell simulations. We consider values of plasma beta (the ratio of thermal and magnetic pressures) in the range 4 ≲ β p0 ≲ 32, and sonic Mach number (the ratio of <span class="hlt">shock</span> speed to pre-<span class="hlt">shock</span> sound speed) in the range 2 ≲ M s ≲ 5, as appropriate for galaxy cluster <span class="hlt">shocks</span>. As shown in Paper I, magnetic field amplification—induced by <span class="hlt">shock</span> <span class="hlt">compression</span> of the pre-<span class="hlt">shock</span> field, or by strong proton cyclotron and mirror modes accompanying the relaxation of proton temperature anisotropy—can drive the electron temperature anisotropy beyond the threshold of the electron whistler instability. The growth of whistler waves breaks the electron adiabatic invariance, and allows for efficient entropy production. We find that the post-<span class="hlt">shock</span> electron temperature T e2 exceeds the adiabatic expectation {T}e2,{ad} by an amount ({T}e2-{T}e2,{ad})/{T}e0≃ 0.044 {M}s({M}s-1) (here, T e0 is the pre-<span class="hlt">shock</span> temperature), which depends only weakly on the plasma beta over the range 4 ≲ β p0 ≲ 32 that we have explored, as well as on the proton-to-electron mass ratio (the coefficient of ≃0.044 is measured for our fiducial {m}i/{m}e=49, and we estimate that it will decrease to ≃0.03 for the realistic mass ratio). Our results have important implications for current and future observations of galaxy cluster <span class="hlt">shocks</span> in the radio band (synchrotron emission and Sunyaev–Zel’dovich effect) and at X-ray frequencies.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2009JAP...105i3523G','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2009JAP...105i3523G"><span>Picosecond time scale dynamics of short pulse laser-driven <span class="hlt">shocks</span> in tin</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Grigsby, W.; Bowes, B. T.; Dalton, D. A.; Bernstein, A. C.; Bless, S.; Downer, M. C.; Taleff, E.; Colvin, J.; Ditmire, T.</p> <p>2009-05-01</p> <p>The dynamics of high strain rate <span class="hlt">shock</span> waves driven by a subnanosecond laser pulse in thin tin slabs have been investigated. These <span class="hlt">shocks</span>, with pressure up to 1 Mbar, have been diagnosed with an 800 nm wavelength ultrafast laser pulse in a pump-probe configuration, which measured reflectivity and two-dimensional interferometry of the expanding rear surface. Time-resolved rear surface expansion data suggest that we reached pressures necessary to <span class="hlt">shock</span> melt tin upon <span class="hlt">compression</span>. Reflectivity measurements, however, show an anomalously high drop in the tin reflectivity for free standing foils, which can be attributed to microparticle formation at the back surface when the laser-driven <span class="hlt">shock</span> releases.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://www.dtic.mil/docs/citations/AD1054563','DTIC-ST'); return false;" href="http://www.dtic.mil/docs/citations/AD1054563"><span>Test Operations Procedure (TOP) 10-2-400 Open End <span class="hlt">Compressed</span> Gas Driven <span class="hlt">Shock</span> Tube</span></a></p> <p><a target="_blank" href="http://www.dtic.mil/">DTIC Science & Technology</a></p> <p></p> <p></p> <p>gas-driven <span class="hlt">shock</span> tube. Procedures are provided for instrumentation, test item positioning, estimation of key test parameters, operation of the <span class="hlt">shock</span>...tube, data collection, and reporting. The procedures in this document are based on the use of helium gas and Mylar film diaphragms.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20080022442','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20080022442"><span>Nonstandard Analysis and Jump Conditions for Converging <span class="hlt">Shock</span> Waves</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Baty, Roy S.; Farassat, Fereidoun; Tucker, Don H.</p> <p>2008-01-01</p> <p>Nonstandard analysis is an area of modern mathematics which studies abstract number systems containing both infinitesimal and infinite numbers. This article applies nonstandard analysis to derive jump conditions for one-dimensional, converging <span class="hlt">shock</span> waves in a <span class="hlt">compressible</span>, inviscid, perfect gas. It is assumed that the <span class="hlt">shock</span> thickness occurs on an infinitesimal interval and the jump functions in the thermodynamic and fluid dynamic parameters occur smoothly across this interval. Predistributions of the Heaviside function and the Dirac delta measure are introduced to model the flow parameters across a <span class="hlt">shock</span> wave. The equations of motion expressed in nonconservative form are then applied to derive unambiguous relationships between the jump functions for the flow parameters.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1232687-resistance-fly-ash-portland-cement-blends-thermal-shock','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1232687-resistance-fly-ash-portland-cement-blends-thermal-shock"><span>Resistance of fly ash-Portland cement blends to thermal <span class="hlt">shock</span></span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>Pyatina, Tatiana; Sugama, Toshifumi</p> <p>2015-09-11</p> <p>Thermal-<span class="hlt">shock</span> resistance of high-content fly ash-Portland cement blends was tested in the following ways. Activated and non-activated blends with 80-90 % fly ash F (FAF) were left to set at room temperature, then hydrated for 24 hours at 85°C and 24-more hours at 300°C and tested in five thermal-<span class="hlt">shock</span> cycles (600°C heat - 25°C water quenching). XRD, and thermal gravimetric analyses, along with calorimetric measurements and SEM-EDX tests demonstrated that the activated blends form more hydrates after 24 hours at 300°C, and achieve a higher short-term <span class="hlt">compressive</span> strength than do non-activated ones. Sodium meta-silicate and sodaash engendered the concomitant hydrationmore » of OPC and FAF, with the formation of mixed crystalline FAF-OPC hydrates and FAF hydrates, such as garranite, analcime, and wairakite, along with the amorphous FAF hydration products. In SS-activated and non-activated blends separate OPC (tobermorite) and FAF (amorphous gel) hydrates with no mixed crystalline products formed. The <span class="hlt">compressive</span> strength of all tested blends decreased by nearly 50% after 5 thermal-<span class="hlt">shock</span> test cycles. These changes in the <span class="hlt">compressive</span> strength were accompanied by a marked decrease in the intensities of XRD patterns of the crystalline hydrates after the thermalshock. As a result, there was no significant difference in the performance of the blends with different activators« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/1409985-situ-ray-diffraction-measurement-shock-wave-driven-twinning-lattice-dynamics','SCIGOV-STC'); return false;" href="https://www.osti.gov/biblio/1409985-situ-ray-diffraction-measurement-shock-wave-driven-twinning-lattice-dynamics"><span>In situ X-ray diffraction measurement of <span class="hlt">shock</span>-wave-driven twinning and lattice dynamics</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Wehrenberg, C. E.; McGonegle, D.; Bolme, C.</p> <p></p> <p>We report that pressure-driven <span class="hlt">shock</span> waves in solid materials can cause extreme damage and deformation. Understanding this deformation and the associated defects that are created in the material is crucial in the study of a wide range of phenomena, including planetary formation and asteroid impact sites, the formation of interstellar dust clouds, ballistic penetrators, spacecraft shielding and ductility in high-performance ceramics. At the lattice level, the basic mechanisms of plastic deformation are twinning (whereby crystallites with a mirror-image lattice form) and slip (whereby lattice dislocations are generated and move), but determining which of these mechanisms is active during deformation ismore » challenging. Experiments that characterized lattice defects have typically examined the microstructure of samples after deformation, and so are complicated by post-<span class="hlt">shock</span> annealing and reverberations. In addition, measurements have been limited to relatively modest pressures (less than 100 gigapascals). In situ X-ray diffraction experiments can provide insights into the dynamic behaviour of materials, but have only recently been applied to plasticity during <span class="hlt">shock</span> <span class="hlt">compression</span> and have yet to provide detailed insight into competing deformation mechanisms. Here we present X-ray diffraction experiments with femtosecond resolution that capture in situ, lattice-level information on the microstructural processes that drive <span class="hlt">shock</span>-wave-driven deformation. To demonstrate this method we <span class="hlt">shock-compress</span> the body-centred-cubic material tantalum—an important material for high-energy-density physics owing to its high <span class="hlt">shock</span> impedance and high X-ray opacity. Tantalum is also a material for which previous <span class="hlt">shock</span> <span class="hlt">compression</span> simulations and experiments have provided conflicting information about the dominant deformation mechanism. Our experiments reveal twinning and related lattice rotation occurring on the timescale of tens of picoseconds. In addition, despite the common</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1409985-situ-ray-diffraction-measurement-shock-wave-driven-twinning-lattice-dynamics','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1409985-situ-ray-diffraction-measurement-shock-wave-driven-twinning-lattice-dynamics"><span>In situ X-ray diffraction measurement of <span class="hlt">shock</span>-wave-driven twinning and lattice dynamics</span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>Wehrenberg, C. E.; McGonegle, D.; Bolme, C.; ...</p> <p>2017-10-25</p> <p>We report that pressure-driven <span class="hlt">shock</span> waves in solid materials can cause extreme damage and deformation. Understanding this deformation and the associated defects that are created in the material is crucial in the study of a wide range of phenomena, including planetary formation and asteroid impact sites, the formation of interstellar dust clouds, ballistic penetrators, spacecraft shielding and ductility in high-performance ceramics. At the lattice level, the basic mechanisms of plastic deformation are twinning (whereby crystallites with a mirror-image lattice form) and slip (whereby lattice dislocations are generated and move), but determining which of these mechanisms is active during deformation ismore » challenging. Experiments that characterized lattice defects have typically examined the microstructure of samples after deformation, and so are complicated by post-<span class="hlt">shock</span> annealing and reverberations. In addition, measurements have been limited to relatively modest pressures (less than 100 gigapascals). In situ X-ray diffraction experiments can provide insights into the dynamic behaviour of materials, but have only recently been applied to plasticity during <span class="hlt">shock</span> <span class="hlt">compression</span> and have yet to provide detailed insight into competing deformation mechanisms. Here we present X-ray diffraction experiments with femtosecond resolution that capture in situ, lattice-level information on the microstructural processes that drive <span class="hlt">shock</span>-wave-driven deformation. To demonstrate this method we <span class="hlt">shock-compress</span> the body-centred-cubic material tantalum—an important material for high-energy-density physics owing to its high <span class="hlt">shock</span> impedance and high X-ray opacity. Tantalum is also a material for which previous <span class="hlt">shock</span> <span class="hlt">compression</span> simulations and experiments have provided conflicting information about the dominant deformation mechanism. Our experiments reveal twinning and related lattice rotation occurring on the timescale of tens of picoseconds. In addition, despite the common</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/22809840','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/22809840"><span>External cardiac <span class="hlt">compression</span> may be harmful in some scenarios of pulseless electrical activity.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Hogan, T S</p> <p>2012-10-01</p> <p>Pulseless electrical activity occurs when organised or semi-organised electrical activity of the heart persists but the product of systemic vascular resistance and the increase in systemic arterial flow generated by the ejection of the left venticular stroke volume is not sufficient to produce a clinically detectable pulse. Pulseless electrical activity encompasses a very heterogeneous variety of severe circulatory <span class="hlt">shock</span> states ranging in severity from pseudo-cardiac arrest to effective cardiac arrest. Outcomes of cardiopulmonary resuscitation for pulseless electrical activity are generally poor. Impairment of cardiac filling is the limiting factor to cardiac output in many scenarios of pulseless electrical activity, including extreme vasodilatory <span class="hlt">shock</span> states. There is no evidence that external cardiac <span class="hlt">compression</span> can increase cardiac output when impaired cardiac filling is the limiting factor to cardiac output. If impaired cardiac filling is the limiting factor to cardiac output and the heart is effectively ejecting all the blood returning to it, then external cardiac <span class="hlt">compression</span> can only increase cardiac output if it increases venous return and cardiac filling. Repeated cardiac <span class="hlt">compression</span> asynchronous with the patient's cardiac cycle and raised mean intrathoracic pressure due to chest <span class="hlt">compression</span> can be expected to reduce rather than to increase cardiac filling and therefore to reduce rather than to increase cardiac output in such circumstances. The hypothesis is proposed that the performance of external cardiac <span class="hlt">compression</span> will have zero or negative effect on cardiac output in pulseless electrical activity when impaired cardiac filling is the limiting factor to cardiac output. External cardiac <span class="hlt">compression</span> may be both directly and indirectly harmful to significant sub-groups of patients with pulseless electrical activity. We have neither evidence nor theory to provide comfort that external cardiac <span class="hlt">compression</span> is not harmful in many scenarios of pulseless</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/6941929','DOE-PATENT-XML'); return false;" href="https://www.osti.gov/biblio/6941929"><span><span class="hlt">Shock</span> wave absorber having apertured plate</span></a></p> <p><a target="_blank" href="http://www.osti.gov/doepatents">DOEpatents</a></p> <p>Shin, Y.W.; Wiedermann, A.H.; Ockert, C.E.</p> <p>1983-08-26</p> <p>The <span class="hlt">shock</span> or energy absorber disclosed herein utilizes an apertured plate maintained under the normal level of liquid flowing in a piping system and disposed between the normal liquid flow path and a cavity pressurized with a <span class="hlt">compressible</span> gas. The degree of openness (or porosity) of the plate is between 0.01 and 0.60. The energy level of a <span class="hlt">shock</span> wave travelling down the piping system thus is dissipated by some of the liquid being jetted through the apertured plate toward the cavity. The cavity is large compared to the quantity of liquid jetted through the apertured plate, so there is little change in its volume. The porosity of the apertured plate influences the percentage of energy absorbed.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/865724','DOE-PATENT-XML'); return false;" href="https://www.osti.gov/servlets/purl/865724"><span><span class="hlt">Shock</span> wave absorber having apertured plate</span></a></p> <p><a target="_blank" href="http://www.osti.gov/doepatents">DOEpatents</a></p> <p>Shin, Yong W.; Wiedermann, Arne H.; Ockert, Carl E.</p> <p>1985-01-01</p> <p>The <span class="hlt">shock</span> or energy absorber disclosed herein utilizes an apertured plate maintained under the normal level of liquid flowing in a piping system and disposed between the normal liquid flow path and a cavity pressurized with a <span class="hlt">compressible</span> gas. The degree of openness (or porosity) of the plate is between 0.01 and 0.60. The energy level of a <span class="hlt">shock</span> wave travelling down the piping system thus is dissipated by some of the liquid being jetted through the apertured plate toward the cavity. The cavity is large compared to the quantity of liquid jetted through the apertured plate, so there is little change in its volume. The porosity of the apertured plate influences the percentage of energy absorbed.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2009PhDT.........1V','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2009PhDT.........1V"><span>Modeling magnetic field amplification in nonlinear diffusive <span class="hlt">shock</span> acceleration</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Vladimirov, Andrey</p> <p>2009-02-01</p> <p>This research was motivated by the recent observations indicating very strong magnetic fields at some supernova remnant <span class="hlt">shocks</span>, which suggests in-situ generation of magnetic turbulence. The dissertation presents a numerical model of collisionless <span class="hlt">shocks</span> with strong amplification of stochastic magnetic fields, self-consistently coupled to efficient <span class="hlt">shock</span> acceleration of charged particles. Based on a Monte Carlo simulation of particle transport and acceleration in nonlinear <span class="hlt">shocks</span>, the model describes magnetic field amplification using the state-of-the-art analytic models of instabilities in magnetized plasmas in the presence of non-thermal particle streaming. The results help one understand the complex nonlinear connections between the thermal plasma, the accelerated particles and the stochastic magnetic fields in strong collisionless <span class="hlt">shocks</span>. Also, predictions regarding the efficiency of particle acceleration and magnetic field amplification, the impact of magnetic field amplification on the maximum energy of accelerated particles, and the <span class="hlt">compression</span> and heating of the thermal plasma by the <span class="hlt">shocks</span> are presented. Particle distribution functions and turbulence spectra derived with this model can be used to calculate the emission of observable nonthermal radiation.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/12935242','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/12935242"><span>Three-dimensional lattice Boltzmann model for <span class="hlt">compressible</span> flows.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Sun, Chenghai; Hsu, Andrew T</p> <p>2003-07-01</p> <p>A three-dimensional <span class="hlt">compressible</span> lattice Boltzmann model is formulated on a cubic lattice. A very large particle-velocity set is incorporated in order to enable a greater variation in the mean velocity. Meanwhile, the support set of the equilibrium distribution has only six directions. Therefore, this model can efficiently handle flows over a wide range of Mach numbers and capture <span class="hlt">shock</span> waves. Due to the simple form of the equilibrium distribution, the fourth-order velocity tensors are not involved in the formulation. Unlike the standard lattice Boltzmann model, no special treatment is required for the homogeneity of fourth-order velocity tensors on square lattices. The Navier-Stokes equations were recovered, using the Chapman-Enskog method from the Bhatnagar-Gross-Krook (BGK) lattice Boltzmann equation. The second-order discretization error of the fluctuation velocity in the macroscopic conservation equation was eliminated by means of a modified collision invariant. The model is suitable for both viscous and inviscid <span class="hlt">compressible</span> flows with or without <span class="hlt">shocks</span>. Since the present scheme deals only with the equilibrium distribution that depends only on fluid density, velocity, and internal energy, boundary conditions on curved wall are easily implemented by an extrapolation of macroscopic variables. To verify the scheme for inviscid flows, we have successfully simulated a three-dimensional <span class="hlt">shock</span>-wave propagation in a box and a normal <span class="hlt">shock</span> of Mach number 10 over a wedge. As an application to viscous flows, we have simulated a flat plate boundary layer flow, flow over a cylinder, and a transonic flow over a NACA0012 airfoil cascade.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017APS..SHK.B3001S','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017APS..SHK.B3001S"><span>Multi-<span class="hlt">shock</span> experiments on a TATB-based composition</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Sorin, Remy</p> <p>2017-06-01</p> <p>Temperature based models for condensed explosive need an unreacted equation of state (EOS) that allows a realistic estimation of the temperature for a <span class="hlt">shock</span> <span class="hlt">compression</span> driven at detonation velocity. To feed the detonation models, we aim at exploring the high pressure <span class="hlt">shock</span> Hugoniot of unreacted TATB composition up to 30 GPa with both hydrodynamic and temperature measurements. We performed on the gas gun facility ARES, multi-<span class="hlt">shock</span> experiments where the first <span class="hlt">shock</span> is designed to desensitize the explosive and inhibit the reactivity of the composition. The hydrodynamic behavior was measured via the velocity of a TATB/LiF interface with PDV probes. We attempted to measure the temperature of the <span class="hlt">shocked</span> material via surface emissivity with a pyrometer calibrated to the expected low temperature range. Based on single <span class="hlt">shock</span> experiments and on ab-initio calculation, we built a complete EOS for the unreacted phase of the TATB explosive. The hydrodynamic data are in good agreement with our unreacted EOS. Despite the record of multi-stage emissivity signals, the temperature measurements were difficult to interpret dur to high-luminisity phenomena pertubation. In collaboration with: Nicolas Desbiens, Vincent Dubois and Fabrice Gillot, CEA DAM DIF.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/19940009447','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/19940009447"><span>Thermal <span class="hlt">shock</span> resistance of ceramic matrix composites</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Carper, D. M.; Nied, H. F.</p> <p>1993-01-01</p> <p>The experimental and analytical investigation of the thermal <span class="hlt">shock</span> phenomena in ceramic matrix composites is detailed. The composite systems examined were oxide-based, consisting of an aluminosilicate matrix with either polycrystalline aluminosilicate or single crystal alumina fiber reinforcement. The program was divided into three technical tasks; baseline mechanical properties, thermal <span class="hlt">shock</span> modeling, and thermal <span class="hlt">shock</span> testing. The analytical investigation focused on the development of simple expressions for transient thermal stresses induced during thermal <span class="hlt">shock</span>. The effect of various material parameters, including thermal conductivity, elastic modulus, and thermal expansion, were examined analytically for their effect on thermal <span class="hlt">shock</span> performance. Using a simple maximum stress criteria for each constituent, it was observed that fiber fracture would occur only at the most extreme thermal <span class="hlt">shock</span> conditions and that matrix fracture, splitting parallel to the reinforcing fiber, was to be expected for most practical cases. Thermal <span class="hlt">shock</span> resistance for the two material systems was determined experimentally by subjecting plates to sudden changes in temperature on one surface while maintaining the opposite surface at a constant temperature. This temperature change was varied in severity (magnitude) and in number of <span class="hlt">shocks</span> applied to a given sample. The results showed that for the most severe conditions examined that only surface matrix fracture was present with no observable fiber fracture. The impact of this damage on material performance was limited to the matrix dominated properties only. Specifically, <span class="hlt">compression</span> strength was observed to decrease by as much as 50 percent from the measured baseline.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018AIPC.1959g0015K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018AIPC.1959g0015K"><span>Stability of an arch type <span class="hlt">shock</span> absorber made of a rubber-like material</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Kabrits, Sergey A.; Kolpak, Eugeny P.</p> <p>2018-05-01</p> <p>The paper considers the stability problem of an arch <span class="hlt">shock</span> absorber made of a rubber-like material. As a model, the nonlinear theory of thin shells from elastomers K.F. Chernykh is used. The case of symmetrical and asymmetrical deformation of an arch <span class="hlt">shock</span> absorber under symmetrical <span class="hlt">compression</span> is investigated. The possibility of asymmetric bifurcation is evaluated depending on the boundary conditions.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2003PhDT........17J','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2003PhDT........17J"><span><span class="hlt">Shock</span>-activated reaction synthesis and high pressure response of titanium-based ternary carbide and nitride ceramics</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Jordan, Jennifer Lynn</p> <p></p> <p>The objectives of this study were to (a) investigate the effect of <span class="hlt">shock</span> activation of precursor powders for solid-state reaction synthesis of Ti-based ternary ceramics and (b) to determine the high pressure phase stability and Hugoniot properties of Ti3SiC2. Dynamically densified compacts of Ti, SiC, and graphite precursor powders and Ti and AlN precursor powders were used to study the <span class="hlt">shock</span>-activated formation of Ti 3SiC2 and Ti2AlN ternary compounds, respectively, which are considered to be novel ceramics having high stiffness but low hardness. Gas gun and explosive loading techniques were used to obtain a range of loading conditions resulting in densification and activation. Measurements of fraction reacted as a function of time and temperature and activation energies obtained from DTA experiments were used to determine the degree of activation caused by <span class="hlt">shock</span> <span class="hlt">compression</span> and its subsequent effect on the reaction mechanisms and kinetics. In both systems, <span class="hlt">shock</span> activation led to an accelerated rate of reaction at temperatures less than 1600°C and, above that temperature, it promoted the formation of almost 100% of the ternary compound. A kinetics-based mathematical model based on mass and thermal transport was developed to predict the effect of <span class="hlt">shock</span> activation and reaction synthesis conditions that ensure formation of the ternary compounds. Model predictions revealed a transition temperature above which the reaction is taken over by the "run-away" combustion-type mode. The high pressure phase stability of pre-alloyed Ti 3SiC2 compound was investigated by performing Hugoniot <span class="hlt">shock</span> and particle velocity measurements using the facilities at the National Institute for Materials Science (Tsukuba, Japan). Experiments performed at pressures of 95--120 GPa showed that the <span class="hlt">compressibility</span> of Ti3SiC 2 at these pressures deviates from the previously reported <span class="hlt">compressibility</span> of the material under static high pressure loading. The deviation in <span class="hlt">compressibility</span> behavior is</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_21");'>21</a></li> <li><a href="#" onclick='return showDiv("page_22");'>22</a></li> <li><a href="#" onclick='return showDiv("page_23");'>23</a></li> <li class="active"><span>24</span></li> <li><a href="#" onclick='return showDiv("page_25");'>25</a></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_24 --> <div id="page_25" class="hiddenDiv"> <div class="row"> <div class="col-sm-12"> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_21");'>21</a></li> <li><a href="#" onclick='return showDiv("page_22");'>22</a></li> <li><a href="#" onclick='return showDiv("page_23");'>23</a></li> <li><a href="#" onclick='return showDiv("page_24");'>24</a></li> <li class="active"><span>25</span></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div> </div> <div class="row"> <div class="col-sm-12"> <ol class="result-class" start="481"> <li> <p><a target="_blank" onclick="trackOutboundLink('https://ntrs.nasa.gov/search.jsp?R=19900038236&hterms=guns&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D50%26Ntt%3Dguns','NASA-TRS'); return false;" href="https://ntrs.nasa.gov/search.jsp?R=19900038236&hterms=guns&qs=Ntx%3Dmode%2Bmatchall%26Ntk%3DAll%26N%3D0%26No%3D50%26Ntt%3Dguns"><span>Improvement of pump tubes for gas guns and <span class="hlt">shock</span> tube drivers</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Bogdanoff, D. W.</p> <p>1990-01-01</p> <p>In a pump tube, a gas is mechanically <span class="hlt">compressed</span>, producing very high pressures and sound speeds. The intensely heated gas produced in such a tube can be used to drive light gas guns and <span class="hlt">shock</span> tubes. Three concepts are presented that have the potential to allow substantial reductions in the size and mass of the pump tube to be achieved. The first concept involves the use of one or more diaphragms in the pump tube, thus replacing a single <span class="hlt">compression</span> process by multiple, successive <span class="hlt">compressions</span>. The second concept involves a radical reduction in the length-to-diameter ratio of the pump tube and the pump tube piston. The third concept involves <span class="hlt">shock</span> heating of the working gas by high explosives in a cyclindrical geometry reusable device. Preliminary design analyses are performed on all three concepts and they appear to be quite feasible. Reductions in the length and mass of the pump tube by factors up to about 11 and about 7, respectively, are predicted, relative to a benchmark conventional pump tube.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/9330454','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/9330454"><span>In vitro study of the mechanical effects of <span class="hlt">shock</span>-wave lithotripsy.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Howard, D; Sturtevant, B</p> <p>1997-01-01</p> <p>Impulsive stress in repeated <span class="hlt">shock</span> waves administered during extracorporeal <span class="hlt">shock</span>-wave lithotripsy (ESWL) causes injury to kidney tissue. In a study of the mechanical input of ESWL, the effects of focused <span class="hlt">shock</span> waves on thin planar polymeric membranes immersed in a variety of tissue-mimicking fluids have been examined. A direct mechanism of failure by <span class="hlt">shock</span> <span class="hlt">compression</span> and an indirect mechanism by bubble collapse have been observed. Thin membranes are easily damaged by bubble collapse. After propagating through cavitation-free acoustically heterogeneous media (liquids mixed with hollow glass spheres, and tissue) <span class="hlt">shock</span> waves cause membranes to fail in fatigue by a shearing mechanism. As is characteristic of dynamic fatigue, the failure stress increases with strain rate, determined by the amplitude and rise time of the attenuated <span class="hlt">shock</span> wave. <span class="hlt">Shocks</span> with large amplitude and short rise time (i.e., in uniform media) cause no damage. Thus the inhomogeneity of tissue is likely to contribute to injury in ESWL. A definition of dose is proposed which yields a criterion for damage based on measurable <span class="hlt">shock</span> wave properties.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2013APS..DPPGP8124H','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2013APS..DPPGP8124H"><span>Magnetic Diagnostics on the Magnetized <span class="hlt">Shock</span> Experiment (MSX)</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Hutchinson, T. M.; Weber, T. E.; Boguski, J. C.; Intrator, T. P.; Smith, R. J.; Dunn, J. P.</p> <p>2013-10-01</p> <p>The Magnetized <span class="hlt">Shock</span> Experiment (MSX) at Los Alamos National Laboratory was built to investigate the physics of high-Alfvénic, supercritical, magnetized <span class="hlt">shocks</span> through the acceleration and subsequent stagnation of a Field Reversed Configuration (FRC) plasmoid against a magnetic mirror and/or plasma target. An array of high-bandwidth, multi-axis, robust, internal magnetic probes has been constructed to characterize flux <span class="hlt">compression</span> ratios, instability formation, and turbulent macro-scale features of the post-<span class="hlt">shock</span> plasma. The mirror magnet is mounted on a linear translation stage, providing a capability to axially move the <span class="hlt">shock</span> layer through the probe field of view. An independent, external probe array also provides conventional information on the FRC shape, velocity, and total pressure during the formation and acceleration phases. Probe design, characterization, configuration, and initial results are presented. This work is supported by the DOE OFES and NNSA under LANS contract DE-AC52-06NA25369. LA-UR-13-25189.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/24827366','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/24827366"><span>Modeling multiscale evolution of numerous voids in <span class="hlt">shocked</span> brittle material.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Yu, Yin; Wang, Wenqiang; He, Hongliang; Lu, Tiecheng</p> <p>2014-04-01</p> <p>The influence of the evolution of numerous voids on macroscopic properties of materials is a multiscale problem that challenges computational research. A <span class="hlt">shock</span>-wave <span class="hlt">compression</span> model for brittle material, which can obtain both microscopic evolution and macroscopic <span class="hlt">shock</span> properties, was developed using discrete element methods (lattice model). Using a model interaction-parameter-mapping procedure, qualitative features, as well as trends in the calculated <span class="hlt">shock</span>-wave profiles, are shown to agree with experimental results. The <span class="hlt">shock</span> wave splits into an elastic wave and a deformation wave in porous brittle materials, indicating significant <span class="hlt">shock</span> plasticity. Void collapses in the deformation wave were the natural reason for volume shrinkage and deformation. However, media slippage and rotation deformations indicated by complex vortex patterns composed of relative velocity vectors were also confirmed as an important source of <span class="hlt">shock</span> plasticity. With increasing pressure, the contribution from slippage deformation to the final plastic strain increased. Porosity was found to determine the amplitude of the elastic wave; porosity and <span class="hlt">shock</span> stress together determine propagation speed of the deformation wave, as well as stress and strain on the final equilibrium state. Thus, <span class="hlt">shock</span> behaviors of porous brittle material can be systematically designed for specific applications.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/1995ApOpt..34.6465C','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/1995ApOpt..34.6465C"><span>Optical distortion in the field of a lithotripter <span class="hlt">shock</span> wave</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Carnell, M. T.; Emmony, D. C.</p> <p>1995-10-01</p> <p>The schlieren observation of cavitation phenomena produced in the tail of a lithotripter <span class="hlt">shock</span> wave has indicated the presence of some interesting features. The images produced appear to indicate that cavitation transients in the field of a <span class="hlt">shock</span> wave propagate nonsymmetrically; this is not the case. The apparent lack of symmetry exhibited by the primary cavitation transients is due to a complex optical lensing effect, which is brought about by the change in refractive index associated with the pressure profile of the <span class="hlt">shock</span> wave. Objects seen through or immersed in the <span class="hlt">shock</span>-wave field of an electromagnetic acoustic transducer, such as cavitation, appear highly distorted because of the strong positive and negative lensing effects of the <span class="hlt">compression</span> and rarefaction cycles of the <span class="hlt">shock</span> wave. A modification of the schlieren technique called the scale method has been used to model the distortion introduced by the <span class="hlt">shock</span> wave and consequently explain the cavitation distortion. The technique has also been used to quantitatively analyze and partially reconstruct the lithotripter <span class="hlt">shock</span> wave. The combination of schlieren and scale imaging gives more information about the refractive index field and therefore the <span class="hlt">shock</span>-wave structure itself.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017APS..MAR.H2003K','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017APS..MAR.H2003K"><span>Electronic Structure of Energetic Molecules and Crystals Under <span class="hlt">Compression</span></span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Kay, Jeffrey</p> <p></p> <p>Understanding how the electronic structure of energetic materials change under <span class="hlt">compression</span> is important to elucidating mechanisms of <span class="hlt">shock</span>-induced reactions and detonation. In this presentation, the electronic structure of prototypical energetic crystals are examined under high degrees of <span class="hlt">compression</span> using ab initio quantum chemical calculations. The effects of <span class="hlt">compression</span> on and interactions between the constituent molecules are examined in particular. The insights these results provide into previous experimental observations and theoretical predictions of energetic materials under high pressure are discussed. Sandia National Laboratories is a multi-program laboratory managed and operated by Sandia Corporation, a wholly owned subsidiary of Lockheed Martin Corporation, for the U.S. DOE's National Nuclear Security Administration under contract DE-AC04-94AL85000.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2005shwa.book.1235A','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2005shwa.book.1235A"><span>A new <span class="hlt">shock</span> wave assisted sandalwood oil extraction technique</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Arunkumar, A. N.; Srinivasa, Y. B.; Ravikumar, G.; Shankaranarayana, K. H.; Rao, K. S.; Jagadeesh, G.</p> <p></p> <p>A new <span class="hlt">shock</span> wave assisted oil extraction technique from sandalwood has been developed in the <span class="hlt">Shock</span> Waves Lab, IISc, Bangalore. The fragrant oil extracted from sandalwood finds variety of applications in medicine and perfumery industries. In the present method sandal wood specimens (2.5mm diameter and 25mm in length)are subjected to <span class="hlt">shock</span> wave loading (over pressure 15 bar)in a constant area <span class="hlt">shock</span> tube, before extracting the sandal oil using non-destructive oil extraction technique. The results from the study indicates that both the rate of extraction as well as the quantity of oil obtained from sandal wood samples exposed to <span class="hlt">shock</span> waves are higher (15-40 percent) compared to non-destructive oil extraction technique. The <span class="hlt">compressive</span> squeezing of the interior oil pockets in the sandalwood specimen due to <span class="hlt">shock</span> wave loading appears to be the main reason for enhancement in the oil extraction rate. This is confirmed by the presence of warty structures in the cross-section and micro-fissures in the radial direction of the wood samples exposed to <span class="hlt">shock</span> waves in the scanning electron microscopic investigation. In addition the gas chromatographic studies do not show any change in the q uality of sandal oil extracted from samples exposed to <span class="hlt">shock</span> waves.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/biblio/6775425','DOE-PATENT-XML'); return false;" href="https://www.osti.gov/biblio/6775425"><span><span class="hlt">Shock</span>-induced synthesis of high temperature superconducting materials</span></a></p> <p><a target="_blank" href="http://www.osti.gov/doepatents">DOEpatents</a></p> <p>Ginley, D.S.; Graham, R.A.; Morosin, B.; Venturini, E.L.</p> <p>1987-06-18</p> <p>It has now been determined that the unique features of the high pressure <span class="hlt">shock</span> method, especially the <span class="hlt">shock</span>-induced chemical synthesis technique, are fully applicable to high temperature superconducting materials. Extraordinarily high yields are achievable in accordance with this invention, e.g., generally in the range from about 20% to about 99%, often in the range from about 50% to about 90%, lower and higher yields, of course, also being possible. The method of this invention involves the application of a controlled high pressure <span class="hlt">shock</span> <span class="hlt">compression</span> pulse which can be produced in any conventional manner, e.g., by detonation of a high explosive material, the impact of a high speed projectile or the effect of intense pulsed radiation sources such as lasers or electron beams. Examples and a discussion are presented.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2017APS..SHK.J6004D','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2017APS..SHK.J6004D"><span>Dynamic <span class="hlt">Compression</span> Experiments on Hydrogen and Deuterium in the Warm Dense Liquid.</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Desjarlais, Michael; McCoy, Chad; Cochrane, Kyle; Mattsson, Thomas; Knudson, Marcus; Redmer, Ronald</p> <p>2017-06-01</p> <p>Recently a <span class="hlt">shock</span>-ramp platform has been developed on the Z Accelerator to access off-Hugoniot states in liquids. The accelerator delivers a two-step current pulse; the first accelerates the electrode to a constant velocity, which upon impact with the sample cell creates a well-defined <span class="hlt">shock</span>, the subsequent current rise produces ramp <span class="hlt">compression</span> from the initially <span class="hlt">shocked</span> state producing relatively cool (1-2 kK), high pressure (>300 GPa), high <span class="hlt">compression</span> (10 to 15-fold <span class="hlt">compression</span>) states. This technique allows experimental access to the region of phase space where hydrogen is predicted to undergo a first-order phase transition from an insulating molecular-like to a conducting atomic-like liquid. Here we discuss the experimental platform, survey various theoretical predictions for the liquid-liquid, insulator-to-metal transition in hydrogen, and present results of experiments on both deuterium and hydrogen that clearly show an abrupt transition to a metallic state. We also present results from recent experiments at higher temperatures (3-4 kK) and compare the observations to both first-principles theory and previous step-wise loading experiments that exhibited a minimum metallic conductivity. Sandia National Laboratories is a multi-program laboratory managed and operated by Sandia Corporation, a wholly owned subsidiary of Lockheed Martin Corporation, for the U.S. Department of Energy's National Nuclear Security Administration under contract DE-AC04-94AL85000.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2001APS..SHK.M1004W','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2001APS..SHK.M1004W"><span>Characteristics of <span class="hlt">shock</span> propagation in high-strength cement mortar</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Wang, Zhanjiang; Li, Xiaolan; Zhang, Ruoqi</p> <p>2001-06-01</p> <p>Planar impact experiments have been performed on high-strength cement mortar to determine characteristics of <span class="hlt">shock</span> propagation.The experiments were conducted on a light-gas gun,and permanent-magnet particle velocity gages were used to obtain the sand of 0.5 3.5mm size.A bulk density of 2.31g/cm^3,and a <span class="hlt">compressive</span> and tensile strength of 82MPa and 7.8MPa,respectively,were determined.Three kinds of experimental techniques were used,including the reverse ballistic configuration.These techniques effectively averaged the measured dynamic <span class="hlt">compression</span> state over a sensibly large volume of the test sample.The impact velocities were controlled over a range of approximately 80m/s to 0.83km/s.Hugoniot equation of state data were obtained for the material over a pressure range of approximately 0.2 2.0GPa,and its nonlinear constitutive relation were analyzed.The experiment results show that,in higher pressure range provided in the experiment,the <span class="hlt">shock</span> wave in the material splits into two components of an elastic and a plastic,with the Hugoniot elastic limit 0.4 0.5GPa and the precursor velocity about 4.7km/s,and the material presents a very strong nonlinear dynamic response,and its <span class="hlt">shock</span> amplitude will greatly decrease in propagation.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/15071397','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/15071397"><span>Assessment of inflammatory response and sequestration of blood <span class="hlt">iron</span> transferrin complexes in a rat model of lung injury resulting from exposure to low-frequency <span class="hlt">shock</span> waves.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Gorbunov, Nikolai V; McFaul, Steve J; Van Albert, Stephen; Morrissette, Craig; Zaucha, Gary M; Nath, Jayasree</p> <p>2004-04-01</p> <p>Impact of air blast overpressure waves (OPW), or <span class="hlt">shock</span> wave, with the body wall or body armor produces two types of energy waves: high-frequency low-amplitude stress waves and long-duration low-frequency share waves. These types of energy waves are characterized by different mechanisms of primary tissue injury that mostly affect lung. Systemic inflammation and resultant acute respiratory distress syndrome are known major secondary causative agents of delayed multiple organ failure and subsequent death after OPW exposure. However, association of each pattern of the blast OPW-produced energy waves with postexposure inflammatory events has not yet been delineated. The objectives of the present research were a) establishment of a rat model for assessment of the inflammatory response following lung injury produced by exposure to medium-amplitude (approximately 120 kPa) low-frequency (260+/-5 Hz) OPWs; and b) assessment of the dynamics of alteration in polymorphonuclear leukocyte counts and expression of CD11b adhesion molecules on the surface of polymorphonuclear leukocytes and status of <span class="hlt">iron</span>-transferrin complexes in peripheral blood after OPW exposure. This study focused on the OPW effects at different time periods, using a sequential approach to postexposure events. Lung injury in rat was induced by OPW generated in a laboratory <span class="hlt">shock</span> tube. Animals were exposed to OPW (at peak overpressure of 118+/-7 kPa) that produced "moderate" lung injury. Military research institute. Twenty-seven CVF Sprague-Dawley rats were subjected to OPW exposures, and 17 sham-treated animals were used as control. Lung tissue and blood samples were collected at 1, 3, 6, 12, and 24 hrs following OPW exposures and compared with samples collected from nonexposed animals. OPW-induced lung injury caused a 2.7-fold increase in the number of circulatory polymorphonuclear leukocytes as early as 1 hr postexposure, which is indicative of mobilization of the pool of marginated polymorphonuclear</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://hdl.handle.net/2060/20110008062','NASA-TRS'); return false;" href="http://hdl.handle.net/2060/20110008062"><span>Experimental Plans for Subsystems of a <span class="hlt">Shock</span> Wave Driven Gas Core Reactor</span></a></p> <p><a target="_blank" href="http://ntrs.nasa.gov/search.jsp">NASA Technical Reports Server (NTRS)</a></p> <p>Kazeminezhad, F.; Anghai, S.</p> <p>2008-01-01</p> <p>This Contractor Report proposes a number of plans for experiments on subsystems of a <span class="hlt">shock</span> wave driven pulsed magnetic induction gas core reactor (PMI-GCR, or PMD-GCR pulsed magnet driven gas core reactor). Computer models of <span class="hlt">shock</span> generation and collision in a large-scale PMI-GCR <span class="hlt">shock</span> tube have been performed. Based upon the simulation results a number of issues arose that can only be addressed adequately by capturing experimental data on high pressure (approx.1 atmosphere or greater) partial plasma <span class="hlt">shock</span> wave effects in large bore <span class="hlt">shock</span> tubes ( 10 cm radius). There are three main subsystems that are of immediate interest (for appraisal of the concept viability). These are (1) the <span class="hlt">shock</span> generation in a high pressure gas using either a plasma thruster or pulsed high magnetic field, (2) collision of MHD or gas dynamic <span class="hlt">shocks</span>, their interaction time, and collision pile-up region thickness, and (3) magnetic flux <span class="hlt">compression</span> power generation (not included here).</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1331272-fully-compressible-solutions-early-stage-richtmyermeshkov-instability','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1331272-fully-compressible-solutions-early-stage-richtmyermeshkov-instability"><span>Fully <span class="hlt">compressible</span> solutions for early stage Richtmyer–Meshkov instability</span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>Margolin, Len G.; Reisner, Jon Michael</p> <p>2016-10-27</p> <p>Here, we will consider the effects of <span class="hlt">compressibility</span> and viscosity on the early dynamics of the Richtmyer–Meshkov instability (RMI). In particular, we will combine theory, scaling, and high resolution simulation of RMI to probe the details of the initial <span class="hlt">compression</span> and the subsequent viscous damping as a <span class="hlt">shock</span> interacts with a density discontinuity. We will propose a refinement of the classic 1D model for the linear regime of RMI that, for small initial perturbation wavelengths, more accurately reproduces the 2D dynamics of a fully resolved numerical simulation.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('http://adsabs.harvard.edu/abs/2018PASJ...70S..53I','NASAADS'); return false;" href="http://adsabs.harvard.edu/abs/2018PASJ...70S..53I"><span>The formation of massive molecular filaments and massive stars triggered by a magnetohydrodynamic <span class="hlt">shock</span> wave</span></a></p> <p><a target="_blank" href="http://adsabs.harvard.edu/abstract_service.html">NASA Astrophysics Data System (ADS)</a></p> <p>Inoue, Tsuyoshi; Hennebelle, Patrick; Fukui, Yasuo; Matsumoto, Tomoaki; Iwasaki, Kazunari; Inutsuka, Shu-ichiro</p> <p>2018-05-01</p> <p>Recent observations suggest an that intensive molecular cloud collision can trigger massive star/cluster formation. The most important physical process caused by the collision is a <span class="hlt">shock</span> <span class="hlt">compression</span>. In this paper, the influence of a <span class="hlt">shock</span> wave on the evolution of a molecular cloud is studied numerically by using isothermal magnetohydrodynamics simulations with the effect of self-gravity. Adaptive mesh refinement and sink particle techniques are used to follow the long-time evolution of the <span class="hlt">shocked</span> cloud. We find that the <span class="hlt">shock</span> <span class="hlt">compression</span> of a turbulent inhomogeneous molecular cloud creates massive filaments, which lie perpendicularly to the background magnetic field, as we have pointed out in a previous paper. The massive filament shows global collapse along the filament, which feeds a sink particle located at the collapse center. We observe a high accretion rate \\dot{M}_acc> 10^{-4} M_{⊙}yr-1 that is high enough to allow the formation of even O-type stars. The most massive sink particle achieves M > 50 M_{⊙} in a few times 105 yr after the onset of the filament collapse.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/1087699','SCIGOV-STC'); return false;" href="https://www.osti.gov/servlets/purl/1087699"><span>Flash Lamp Integrating Sphere Technique for Measuring the Dynamic Reflectance of <span class="hlt">Shocked</span> Materials</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Stevens, Gerald; La Lone, Brandon; Veeser, Lynn</p> <p>2013-07-08</p> <p>Accurate reflectance (R) measurements of metals undergoing <span class="hlt">shock</span> wave <span class="hlt">compression</span> can benefit high pressure research in several ways. For example, pressure dependent reflectance measurements can be used to deduce electronic band structure, and discrete changes with pressure or temperature may indicate the occurrence of a phase boundary. Additionally, knowledge of the wavelength dependent emissivity (1 -R, for opaque samples) of the metal surface is essential for accurate pyrometric temperature measurement because the radiance is a function of both the temperature and emissivity. We have developed a method for measuring dynamic reflectance in the visible and near IR spectral regions withmore » nanosecond response time and less than 1.5% uncertainty. The method utilizes an integrating sphere fitted with a xenon flash-lamp illumination source. Because of the integrating sphere, the measurements are insensitive to changes in surface curvature or tilt. The in-situ high brightness of the flash-lamp exceeds the sample’s thermal radiance and also enables the use of solid state detectors for recording the reflectance signals with minimal noise. Using the method, we have examined the dynamic reflectance of gallium and tin subjected to <span class="hlt">shock</span> <span class="hlt">compression</span> from high explosives. The results suggest significant reflectance changes across phase boundaries for both metals. We have also used the method to determine the spectral emissivity of <span class="hlt">shock</span> <span class="hlt">compressed</span> tin at the interface between tin and a LiF window. The results were used to perform emissivity corrections to previous pyrometry data and obtain <span class="hlt">shock</span> temperatures of the tin/LiF interface with uncertainties of less than 2%.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/1334528','SCIGOV-STC'); return false;" href="https://www.osti.gov/servlets/purl/1334528"><span>Sound velocities in highly oriented pyrolytic graphite <span class="hlt">shocked</span> to 18 GPa: Orientational order dependence and elastic instability</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Lucas, Marcel; Winey, J. M.; Gupta, Y. M.</p> <p></p> <p>Previous reports of rapid phase transformation above 18 GPa [Erskine and Nellis, Nature 349, 317 (1991)] and large elastic waves below 18 GPa [Lucas et al., J. Appl. Phys. 114, 093515 (2013)] for <span class="hlt">shock-compressed</span> ZYB-grade highly-oriented pyrolytic graphite (HOPG), but not for less oriented ZYH-grade HOPG, indicated a link between the orientational order dependence of the HOPG response above and below the phase transformation stress. To gain insight into this link and into the mechanical response of HOPG <span class="hlt">shocked</span> to peak stresses approaching the phase transformation onset, the <span class="hlt">compressibility</span> of ZYB- and ZYH-grade HOPG in the <span class="hlt">shocked</span> state was examinedmore » using front surface impact experiments. Particle velocity histories and sound velocities were measured for peak stresses reaching 18 GPa. Although the locus of the measured peak stress-particle velocity states is indistinguishable for the two grades of HOPG, the measured sound velocities in the peak state reveal significant differences between the two grades. Specifically, 1) The measured sound velocities are somewhat higher for ZYH-grade HOPG, compared to ZYB-grade HOPG. 2) The measured sound velocities for ZYH-grade HOPG increase smoothly with <span class="hlt">compression</span>, whereas those for ZYB-2 grade HOPG exhibit a significant reduction in the <span class="hlt">compression</span> dependence from 12 GPa to 17 GPa and an abrupt increase from 17 GPa to 18 GPa. 3) The longitudinal moduli, determined from the measured sound velocities, are smaller than the calculated bulk moduli for ZYB-grade HOPG <span class="hlt">shocked</span> to peak stresses above 15 GPa, indicating the onset of an elastic instability. The present findings demonstrate that the softening of the longitudinal modulus (or elastic instability) presented here is linked to the large elastic waves and the rapid phase transformation reported previously – all observed only for <span class="hlt">shocked</span> ZYB-grade HOPG. The elastic instability in <span class="hlt">shocked</span> ZYB-grade HOPG is likely a precursor to the rapid phase transformation observed</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1334528-sound-velocities-highly-oriented-pyrolytic-graphite-shocked-gpa-orientational-order-dependence-elastic-instability','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1334528-sound-velocities-highly-oriented-pyrolytic-graphite-shocked-gpa-orientational-order-dependence-elastic-instability"><span>Sound velocities in highly oriented pyrolytic graphite <span class="hlt">shocked</span> to 18 GPa: Orientational order dependence and elastic instability</span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>Lucas, Marcel; Winey, J. M.; Gupta, Y. M.</p> <p>2015-12-28</p> <p>Previous reports of rapid phase transformation above 18 GPa [Erskine and Nellis, Nature 349, 317 (1991)] and large elastic waves below 18 GPa [Lucas et al., J. Appl. Phys. 114, 093515 (2013)] for <span class="hlt">shock-compressed</span> ZYB-grade highly-oriented pyrolytic graphite (HOPG), but not for less oriented ZYH-grade HOPG, indicated a link between the orientational order dependence of the HOPG response above and below the phase transformation stress. To gain insight into this link and into the mechanical response of HOPG <span class="hlt">shocked</span> to peak stresses approaching the phase transformation onset, the <span class="hlt">compressibility</span> of ZYB- and ZYH-grade HOPG in the <span class="hlt">shocked</span> state was examinedmore » using front surface impact experiments. Particle velocity histories and sound velocities were measured for peak stresses reaching 18 GPa. Although the locus of the measured peak stress-particle velocity states is indistinguishable for the two grades of HOPG, the measured sound velocities in the peak state reveal significant differences between the two grades. Specifically, 1) The measured sound velocities are somewhat higher for ZYH-grade HOPG, compared to ZYB-grade HOPG. 2) The measured sound velocities for ZYH-grade HOPG increase smoothly with <span class="hlt">compression</span>, whereas those for ZYB-2 grade HOPG exhibit a significant reduction in the <span class="hlt">compression</span> dependence from 12 GPa to 17 GPa and an abrupt increase from 17 GPa to 18 GPa. 3) The longitudinal moduli, determined from the measured sound velocities, are smaller than the calculated bulk moduli for ZYB-grade HOPG <span class="hlt">shocked</span> to peak stresses above 15 GPa, indicating the onset of an elastic instability. The present findings demonstrate that the softening of the longitudinal modulus (or elastic instability) presented here is linked to the large elastic waves and the rapid phase transformation reported previously – all observed only for <span class="hlt">shocked</span> ZYB-grade HOPG. The elastic instability in <span class="hlt">shocked</span> ZYB-grade HOPG is likely a precursor to the rapid phase transformation observed</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.ncbi.nlm.nih.gov/pubmed/23214575','PUBMED'); return false;" href="https://www.ncbi.nlm.nih.gov/pubmed/23214575"><span>Uniform <span class="hlt">shock</span> waves in disordered granular matter.</span></a></p> <p><a target="_blank" href="https://www.ncbi.nlm.nih.gov/entrez/query.fcgi?DB=pubmed">PubMed</a></p> <p>Gómez, Leopoldo R; Turner, Ari M; Vitelli, Vincenzo</p> <p>2012-10-01</p> <p>The confining pressure P is perhaps the most important parameter controlling the properties of granular matter. Strongly <span class="hlt">compressed</span> granular media are, in many respects, simple solids in which elastic perturbations travel as ordinary phonons. However, the speed of sound in granular aggregates continuously decreases as the confining pressure decreases, completely vanishing at the jamming-unjamming transition. This anomalous behavior suggests that the transport of energy at low pressures should not be dominated by phonons. In this work we use simulations and theory to show how the response of granular systems becomes increasingly nonlinear as pressure decreases. In the low-pressure regime the elastic energy is found to be mainly transported through nonlinear waves and <span class="hlt">shocks</span>. We numerically characterize the propagation speed, shape, and stability of these <span class="hlt">shocks</span> and model the dependence of the <span class="hlt">shock</span> speed on pressure and impact intensity by a simple analytical approach.</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/pages/biblio/1410511-time-resolved-diffraction-shock-released-sio2-diaplectic-glass-formation','SCIGOV-DOEP'); return false;" href="https://www.osti.gov/pages/biblio/1410511-time-resolved-diffraction-shock-released-sio2-diaplectic-glass-formation"><span>Time-resolved diffraction of <span class="hlt">shock</span>-released SiO 2 and diaplectic glass formation</span></a></p> <p><a target="_blank" href="http://www.osti.gov/pages">DOE PAGES</a></p> <p>Gleason, A. E.; Bolme, C. A.; Lee, H. J.; ...</p> <p>2017-11-14</p> <p>Understanding how rock-forming minerals transform under <span class="hlt">shock</span> loading is critical for modeling collisions between planetary bodies, interpreting the significance of <span class="hlt">shock</span> features in minerals and for using them as diagnostic indicators of impact conditions, such as <span class="hlt">shock</span> pressure. To date, our understanding of the formation processes experienced by <span class="hlt">shocked</span> materials is based exclusively on ex situ analyses of recovered samples. Formation mechanisms and origins of commonly observed mesoscale material features, such as diaplectic (i.e., <span class="hlt">shocked</span>) glass, remain therefore controversial and unresolvable. Here in this paper we show in situ pump-probe X-ray diffraction measurements on fused silica crystallizing to stishovite onmore » <span class="hlt">shock</span> <span class="hlt">compression</span> and then converting to an amorphous phase on <span class="hlt">shock</span> release in only 2.4 ns from 33.6 GPa. Recovered glass fragments suggest permanent densification. These observations of real-time diaplectic glass formation attest that it is a back-transformation product of stishovite with implications for revising traditional <span class="hlt">shock</span> metamorphism stages.« less</p> </li> <li> <p><a target="_blank" onclick="trackOutboundLink('https://www.osti.gov/servlets/purl/1410511','SCIGOV-STC'); return false;" href="https://www.osti.gov/servlets/purl/1410511"><span>Time-resolved diffraction of <span class="hlt">shock</span>-released SiO 2 and diaplectic glass formation</span></a></p> <p><a target="_blank" href="http://www.osti.gov/search">DOE Office of Scientific and Technical Information (OSTI.GOV)</a></p> <p>Gleason, A. E.; Bolme, C. A.; Lee, H. J.</p> <p></p> <p>Understanding how rock-forming minerals transform under <span class="hlt">shock</span> loading is critical for modeling collisions between planetary bodies, interpreting the significance of <span class="hlt">shock</span> features in minerals and for using them as diagnostic indicators of impact conditions, such as <span class="hlt">shock</span> pressure. To date, our understanding of the formation processes experienced by <span class="hlt">shocked</span> materials is based exclusively on ex situ analyses of recovered samples. Formation mechanisms and origins of commonly observed mesoscale material features, such as diaplectic (i.e., <span class="hlt">shocked</span>) glass, remain therefore controversial and unresolvable. Here in this paper we show in situ pump-probe X-ray diffraction measurements on fused silica crystallizing to stishovite onmore » <span class="hlt">shock</span> <span class="hlt">compression</span> and then converting to an amorphous phase on <span class="hlt">shock</span> release in only 2.4 ns from 33.6 GPa. Recovered glass fragments suggest permanent densification. These observations of real-time diaplectic glass formation attest that it is a back-transformation product of stishovite with implications for revising traditional <span class="hlt">shock</span> metamorphism stages.« less</p> </li> </ol> <div class="pull-right"> <ul class="pagination"> <li><a href="#" onclick='return showDiv("page_1");'>«</a></li> <li><a href="#" onclick='return showDiv("page_21");'>21</a></li> <li><a href="#" onclick='return showDiv("page_22");'>22</a></li> <li><a href="#" onclick='return showDiv("page_23");'>23</a></li> <li><a href="#" onclick='return showDiv("page_24");'>24</a></li> <li class="active"><span>25</span></li> <li><a href="#" onclick='return showDiv("page_25");'>»</a></li> </ul> </div> </div><!-- col-sm-12 --> </div><!-- row --> </div><!-- page_25 --> <div class="footer-extlink text-muted" style="margin-bottom:1rem; text-align:center;">Some links on this page may take you to non-federal websites. Their policies may differ from this site.</div> </div><!-- container --> <footer><a id="backToTop" href="#top"> </a><nav><a id="backToTop" href="#top"> </a><ul class="links"><a id="backToTop" href="#top"> </a><li><a id="backToTop" href="#top"></a><a href="/sitemap.html">Site Map</a></li> <li><a href="/members/index.html">Members Only</a></li> <li><a href="/website-policies.html">Website Policies</a></li> <li><a href="https://doe.responsibledisclosure.com/hc/en-us" target="_blank">Vulnerability Disclosure Program</a></li> <li><a href="/contact.html">Contact Us</a></li> </ul> <div class="small">Science.gov is maintained by the U.S. Department of Energy's <a href="https://www.osti.gov/" target="_blank">Office of Scientific and Technical Information</a>, in partnership with <a href="https://www.cendi.gov/" target="_blank">CENDI</a>.</div> </nav> </footer> <script type="text/javascript"><!-- // var lastDiv = ""; function showDiv(divName) { // hide last div if (lastDiv) { document.getElementById(lastDiv).className = "hiddenDiv"; } //if value of the box is not nothing and an object with that name exists, then change the class if (divName && document.getElementById(divName)) { document.getElementById(divName).className = "visibleDiv"; lastDiv = divName; } } //--> </script> <script> /** * Function that tracks a click on an outbound link in Google Analytics. * This function takes a valid URL string as an argument, and uses that URL string * as the event label. */ var trackOutboundLink = function(url,collectionCode) { try { h = window.open(url); setTimeout(function() { ga('send', 'event', 'topic-page-click-through', collectionCode, url); }, 1000); } catch(err){} }; </script> <!-- Google Analytics --> <script> (function(i,s,o,g,r,a,m){i['GoogleAnalyticsObject']=r;i[r]=i[r]||function(){ (i[r].q=i[r].q||[]).push(arguments)},i[r].l=1*new Date();a=s.createElement(o), m=s.getElementsByTagName(o)[0];a.async=1;a.src=g;m.parentNode.insertBefore(a,m) })(window,document,'script','//www.google-analytics.com/analytics.js','ga'); ga('create', 'UA-1122789-34', 'auto'); ga('send', 'pageview'); </script> <!-- End Google Analytics --> <script> showDiv('page_1') </script> </body> </html>