Sample records for zelmeu zles skbbarb

  1. Numerical flow simulation and efficiency prediction for axial turbines by advanced turbulence models

    NASA Astrophysics Data System (ADS)

    Jošt, D.; Škerlavaj, A.; Lipej, A.

    2012-11-01

    Numerical prediction of an efficiency of a 6-blade Kaplan turbine is presented. At first, the results of steady state analysis performed by different turbulence models for different operating regimes are compared to the measurements. For small and optimal angles of runner blades the efficiency was quite accurately predicted, but for maximal blade angle the discrepancy between calculated and measured values was quite large. By transient analysis, especially when the Scale Adaptive Simulation Shear Stress Transport (SAS SST) model with zonal Large Eddy Simulation (ZLES) in the draft tube was used, the efficiency was significantly improved. The improvement was at all operating points, but it was the largest for maximal discharge. The reason was better flow simulation in the draft tube. Details about turbulent structure in the draft tube obtained by SST, SAS SST and SAS SST with ZLES are illustrated in order to explain the reasons for differences in flow energy losses obtained by different turbulence models.

  2. Numerical investigation of the flow in axial water turbines and marine propellers with scale-resolving simulations

    NASA Astrophysics Data System (ADS)

    Morgut, Mitja; Jošt, Dragica; Nobile, Enrico; Škerlavaj, Aljaž

    2015-11-01

    The accurate prediction of the performances of axial water turbines and naval propellers is a challenging task, of great practical relevance. In this paper a numerical prediction strategy, based on the combination of a trusted CFD solver and a calibrated mass transfer model, is applied to the turbulent flow in axial turbines and around a model scale naval propeller, under non-cavitating and cavitating conditions. Some selected results for axial water turbines and a marine propeller, and in particular the advantages, in terms of accuracy and fidelity, of ScaleResolving Simulations (SRS), like SAS (Scale Adaptive Simulation) and Zonal-LES (ZLES) compared to standard RANS approaches, are presented. Efficiency prediction for a Kaplan and a bulb turbine was significantly improved by use of the SAS SST model in combination with the ZLES in the draft tube. Size of cavitation cavity and sigma break curve for Kaplan turbine were successfully predicted with SAS model in combination with robust high resolution scheme, while for mass transfer the Zwart model with calibrated constants were used. The results obtained for a marine propeller in non-uniform inflow, under cavitating conditions, compare well with available experimental measurements, and proved that a mass transfer model, previously calibrated for RANS (Reynolds Averaged Navier Stokes), can be successfully applied also within the SRS approaches.

  3. East Europe Report

    DTIC Science & Technology

    1986-01-23

    Mezögazdasäg, erdögazdäl- kodäs, vizgazdälkodäs 2,5% LfKözlekedes, tävközles 0,9% Lakossag 8,1% LEgyeb 9,6% -Ipar78,9% (2)VILLAM0S- ENERGIA ...1970’s centered around renovation of the completely used up infrastructure and the obsolete, dangerous buildings. It turned out, however, that the... renovation . [Question] But reconstruction began in 1976.... [Answer] Right. But this did not prove successful. The reason partly was that it began

  4. Operation HARDTACK. Volume 2. Radiological Safety. Extracted Version

    DTIC Science & Technology

    1979-10-01

    slowly to the southwest. This cell van reported 60 z.les southwest. at nightfnll with an intensity of 350 mr/hr measured by the sampler aircraft. This...POJOA , C J~~’/𔄃(Vera)L (Levoy)e ((Oscar) * / (Re RIBAI(Tom)______ (I( Van ) (Fred)R iliS~~ ~ ~ OF S;3 IE/1 NYA Avn (I(Henry) DEEP ENTRANC Radiologica...P2V was dispatched on a track of 260 degrees from Alice and read 300 mr 35 miles out. It van then sent due north of Pearl and found unscectedly an

  5. Numerical simulation of flow in a high head Francis turbine with prediction of efficiency, rotor stator interaction and vortex structures in the draft tube

    NASA Astrophysics Data System (ADS)

    Jošt, D.; Škerlavaj, A.; Morgut, M.; Mežnar, P.; Nobile, E.

    2015-01-01

    The paper presents numerical simulations of flow in a model of a high head Francis turbine and comparison of results to the measurements. Numerical simulations were done by two CFD (Computational Fluid Dynamics) codes, Ansys CFX and OpenFOAM. Steady-state simulations were performed by k-epsilon and SST model, while for transient simulations the SAS SST ZLES model was used. With proper grid refinement in distributor and runner and with taking into account losses in labyrinth seals very accurate prediction of torque on the shaft, head and efficiency was obtained. Calculated axial and circumferential velocity components on two planes in the draft tube matched well with experimental results.