Citation: | Zhao Rui, Yan Chao, Yu Jianet al. New kind Baldwin-Lomax turbulence model under the limit of entropy[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, (2): 175-179,190. (in Chinese) |
[1] |
Baldwin B S, Lomax H. Thin layer approximation and algebraic model for seperated turbulent flows[R]. AIAA-78-257, 1978
|
[2] |
Degani D, Schiff L B. Computation of supersonic viscous flows around pointed bodies at large incidence[R]. AIAA-83-0034, 1983
|
[3] |
Panaras A G, Steger J L. A thin-layer solution of the flow about a prolate spheroid [J]. Z Flugwiss, 1988(12):173-180
|
[4] |
Panaras A G. Algebraic turbulence modeling for swept shock-wave/turbulent boundary-layer interactions [J]. AIAA Journal, 1997,35(2):456-463
|
[5] |
Shang J S, Hankey W L, Jr. Numerical solution for supersonic turbulent flow over a compression ramp[J]. AIAA Journal, 1975,13(10):1368-1374
|
[6] |
Wilcox D C. Reassessment of the scale determining equation for advanced turbulence models[J]. AIAA Journal, 1988, 26(11): 1299-1310
|
[7] |
Gao H, Fu D X, Ma Y W, et al. Direct numerical simulation of supersonic turbulent boundary layer flow[J]. Chinese Physics Letters, 2005, 22(7): 1709-1712
|
[8] |
Settles G S, Dodson L J. Hypersonic shock/boundary-layer interaction database[R]. NASA-CR-177577, 1991
|
[9] |
Visbal M, Knight D. The Baldwin-Lomax turbulence model for two-dimensional shock-wave/boundary-layer Interactions[J]. AIAA Journal, 1984,22(7):921-928
|
[10] |
Forsythe R, Hoffmann A, Damevin M. An assessment of several turbulence models for supersonic compression ramp flow[R]. AIAA 98-2648, 1998
|
[11] |
Knight D. RTO WG 10: test cases for CFD validation of hypersonic flight[R]. AIAA 2002-0433, 2002
|
[12] |
Knight D, ran H, Panaras A, et al. RTO WG 10: CFD validation for shock wave turbulent boundary layer interactions[R]. AIAA 2002-0437, 2002
|