Geodesic
Experience of validation and tuning of turbulence models as applied to the problem of boundary layer separation on a finite-width wedge
Žurnal vyčislitelʹnoj matematiki i matematičeskoj fiziki, Tome 56 (2016) no. 6, pp. 1034-1048 
A. A. Babulin; S. M. Bosnyakov; V. V. Vlasenko; M. F. Engulatova; S. V. Matyash; S. V. Mikhailov. Experience of validation and tuning of turbulence models as applied to the problem of boundary layer separation on a finite-width wedge. Žurnal vyčislitelʹnoj matematiki i matematičeskoj fiziki, Tome 56 (2016) no. 6, pp. 1034-1048. http://geodesic.mathdoc.fr/item/ZVMMF_2016_56_6_a9/
@article{ZVMMF_2016_56_6_a9,
     author = {A. A. Babulin and S. M. Bosnyakov and V. V. Vlasenko and M. F. Engulatova and S. V. Matyash and S. V. Mikhailov},
     title = {Experience of validation and tuning of turbulence models as applied to the problem of boundary layer separation on a finite-width wedge},
     journal = {\v{Z}urnal vy\v{c}islitelʹnoj matematiki i matemati\v{c}eskoj fiziki},
     pages = {1034--1048},
     year = {2016},
     volume = {56},
     number = {6},
     language = {ru},
     url = {http://geodesic.mathdoc.fr/item/ZVMMF_2016_56_6_a9/}
}
TY  - JOUR
AU  - A. A. Babulin
AU  - S. M. Bosnyakov
AU  - V. V. Vlasenko
AU  - M. F. Engulatova
AU  - S. V. Matyash
AU  - S. V. Mikhailov
TI  - Experience of validation and tuning of turbulence models as applied to the problem of boundary layer separation on a finite-width wedge
JO  - Žurnal vyčislitelʹnoj matematiki i matematičeskoj fiziki
PY  - 2016
SP  - 1034
EP  - 1048
VL  - 56
IS  - 6
UR  - http://geodesic.mathdoc.fr/item/ZVMMF_2016_56_6_a9/
LA  - ru
ID  - ZVMMF_2016_56_6_a9
ER  - 
%0 Journal Article
%A A. A. Babulin
%A S. M. Bosnyakov
%A V. V. Vlasenko
%A M. F. Engulatova
%A S. V. Matyash
%A S. V. Mikhailov
%T Experience of validation and tuning of turbulence models as applied to the problem of boundary layer separation on a finite-width wedge
%J Žurnal vyčislitelʹnoj matematiki i matematičeskoj fiziki
%D 2016
%P 1034-1048
%V 56
%N 6
%U http://geodesic.mathdoc.fr/item/ZVMMF_2016_56_6_a9/
%G ru
%F ZVMMF_2016_56_6_a9

Voir la notice de l'article provenant de la source Math-Net.Ru

Modern differential turbulence models are validated by computing a separation zone generated in the supersonic flow past a compression wedge lying on a plate of finite width. The results of three- and two-dimensional computations based on the $(q-\omega)$, SST, and Spalart–Allmaras turbulence models are compared with experimental data obtained for 8$^\circ$, 25$^\circ$, and 45$^\circ$ wedges by A. A. Zheltovodov at the Institute of Theoretical and Applied Mechanics of the Siberian Branch of the Russian Academy of Sciences. An original law-of-the-wall boundary condition and modifications of the SST model intended for improving the quality of the computed separation zone are described.

[1] ANSYS 14.5 Capabilities Brochure, ANSYS, Inc., 2013, 8 pp.

[2] CFD-FASTRAN User Manual, Version 2009.0, ESI CFD Inc., 2009, 345 pp.

[3] Brailko I. A., Makarov V. E., Fedorchenko Yu. P., Shorstov V. A., Programmnyi kompleks COBRA v2.5, Svidetelstvo o gos. registratsii No 2010613209, 2010

[4] Bosnyakov S. M., Vlasenko V. V., Engulatova M. F., Zlenko N. A., Matyash S. V., Mikhailov S. V., Programmnyi kompleks EWT, Svidetelstvo o gosudarstvennoi registratsii programmy dlya EVM No 2008610227, 2008

[5] Settles G. S., Dodson L. J., “Supersonic and hypersonic shock/boundary layer interaction database”, AIAA J., 32:7 (1994), 1377–1383 | DOI

[6] Zheltovodov A. A., Shock waves/turbulent boundary-layer interactions — fundamental studies and applications, AIAA Paper 96-1977, 1996

[7] Knight D. D., Zheltovodov A. A., “Ideal-gas shock wave — turbulent boundary-layer interactions (STBLIs) in supersonic flows and their modeling: two-dimensional interactions”, Shock Wave — Boundary-Layer Interactions, eds. H. Babinsky, J. Harvey, Cambridge University Press, New York, 2011, 137–201 | DOI | MR

[8] Liou W. W., Huang G., Shih T. H., “Turbulence model assessment for shock-wave/turbulent-boundary-layer interaction in transonic and supersonic flows”, Computers and Fluids, 29 (2000), 275–299 | DOI | Zbl

[9] Bedarev I. A., Fedorova N. N., “Issledovanie faktorov, vliyayuschikh na kachestvo predskazaniya turbulentnykh otryvnykh techenii”, Vychislitelnye tekhnologii, 4:1 (1999), 14–32

[10] Sinha K., Manesh K., Candler G. V., “Modeling the effect of shock unsteadiness in shock/turbulent boundary-layer interactions”, AIAA J., 43:3 (2005), 586–594 | DOI

[11] Zheltovodov A. A., “Analiz svoistv dvumernykh otryvnykh techenii pri sverkhzvukovykh skorostyakh”, Issledovaniya pristennykh techenii vyazkogo gaza, ed. N. N. Yanenko, Novosibirsk, 1979, 59–94

[12] Zheltovodov A. A., Shilein E. X., Yakovlev V. N., Razvitie turbulentnogo pogranichnogo sloya v usloviyakh smeshannogo vzaimodeistviya so skachkami uplotneniya i volnami razrezheniya, Prepr. ITPM SO RAN No 28-83, Novosibirsk, 1983

[13] Zheltovodov A. A., Yakovlev V. N., Etapy razvitiya, struktura i kharakteristiki turbulentnosti szhimaemykh otryvnykh techenii v okrestnosti dvumernykh prepyatstvii, Prepr. ITPM SO RAN No 27-86, Novosibirsk, 1986

[14] Bosnyakov S. M., Babulin A. A., Vlasenko V. V., Engulatova M. F., Matyash S. V., Mikhailov S. V., “O tochnosti chislennogo modelirovaniya otryva pogranichnogo sloya na kline ogranichennoi shiriny”, Matem. modelirovanie, 27:10 (2015), 32–46

[15] Wilcox D. C., Turbulence modeling for CFD, 3rd edition, DCW Industries, 2006

[16] Kazhan E. V., “Povyshenie ustoichivosti yavnoi skhemy GKR lokalnym vvedeniem neyavnogo sglazhivatelya”, Uchenye zapiski TsAGI, 2012, no. 6, 66–84

[17] Vlasenko V. V., “O matematicheskom podkhode i printsipakh postroeniya chislennykh metodologii dlya paketa prikladnykh programm EWT-TsAGI”, Trudy TsAGI, 2671, 2007

[18] Spalart P. R., Allmaras S. R., A one-equation turbulence model for aerodynamic flows, AIAA Paper 92-0439, 1992

[19] Coakley T. J., Turbulence modelling methods for the compressible Navier–Stokes equations, AIAA Paper 83-1693, 1983

[20] Coakley T., Hsieh T., Comparison between implicit and hybrid methods for the calculation of steady and unsteady inlet flows, AIAA Paper 85-1125, 1985

[21] Dash S., Weilersteen G., Vaglio-Laurin R., Compressibility effects in free turbulent shear flows, TR-75-1436, AFOSR, 1975

[22] Prakticheskie aspekty resheniya zadach vneshnei i vnutrennei aerodinamiki s primeneniem tekhnologii ZEUS v ramkakh paketa EWT-TsAGI, Sb. statei, Trudy TsAGI, 2735, 2015

[23] Vieser W., Esch T., Menter F., Heat transfer predictions using advanced two-equation turbulence models, CFX Validation Report 10/0602, AEA Technology, 2002, 69 pp.

[24] Vlasenko V. V., Shiryaeva A. A., “Numerical simulation of non stationary propagation of combustion along a duct with supersonic flow of a viscid gas”, Proc. Institution of Mechanical Engineers. Part G: Journal of Aerospace Engineering, 227:3 (2012), 480–492 | DOI | MR

[25] Demyanenko V. S., Zheltovodov A. A., “Ekcperimentalnye issledovaniya otryva turbulentnogo pogranichnogo sloya v okrestnosti stupenki”, Izv. AN SSSR. MZhG, 1977, no. 5, 73–80

[26] Loginov M. S., Adams N. F., Zheltovodov A. A., “Large-eddy simulation of shock-wave/turbulent-boundary-layer interaction”, J. Fluid Mech., 565 (2006), 135–169 | DOI | Zbl