| Citation: | SHI Lei, YAN Ming, YANG Yun-jun, ZHOU Wei-jiang. Applicability investigation about several common schemes and turbulence models in high speed flow[J]. Journal of Aerospace Power, 2014, (8): 1904-1910. doi: 10.13224/j.cnki.jasp.2014.08.019 |
| [1] |
Armstrong J G.Flight planning and conduct of the X-15A-2 envelope expansion program[R].[S.l.]:Air Force Flight Test Center,AFFTC-TD-69-4,1969.
|
| [2] |
Rasky D J,Pittman R B,Newfield M E.The reusable launch vehicle challenge[R].AIAA-2006-7208,2006.
|
| [3] |
Leonard C P,Amundsen R M,Bruce W E.Hyper-X hot structures design and comparison with flight data[R].AIAA-2005-3438,2005.
|
| [4] |
Levy D W,Vassberg J.Summary of data from the first AIAA CFD drag prediction workshop[R].AIAA-2002-0841,2002.
|
| [5] |
Vassberg J C.Drag prediction for the DLR-F4 wing/body using OVERFLOW and CFL3D on the overset mesh[R].AIAA-2002-0840,2002.
|
| [6] |
Alliance N.CFD verification and validation web site[EB/OL].[2011-01-01].http://www.grc.nacs.gov/www/wind/valid.htm.
|
| [7] |
Steger J L,Warming R F.Flux vector splitting of the inviscid gas-dynamic equations with application to finite-difference method[J].Journal of Computational Physics,1981,40(2):263-293.
|
| [8] |
Roe P L.Approximate riemann solvers,parameter vector and difference scheme[J].Journal of Computational Physics,1981,43(2):357-372.
|
| [9] |
Hanel D.On the accuracy of upwind scheme in the solution of Navier-Stokes equation[R].AIAA 87-1105,1987.
|
| [10] |
Liou M S.A sequel to AUSM:AUSM+[J].Journal of Computational Physics,1996,129(2):364-382.
|
| [11] |
Chima R V,Liou M S.Comparison of the AUSM+ and H-CUSP schemes for turbomachinery applications[R].AIAA-2003-4120,2003.
|
| [12] |
WANG Baoyuan,ZHA Gecheng.Comparison of a low diffusion E-CUSP and the Roe scheme for RANS calculation[R].AIAA-2008-0569,2008.
|
| [13] |
Lyubimov A N,Rusanov V V.Gas flows past blunt bodies .NASA TT F-715,1970.
|
| [14] |
Chaupt E,Dubois F.FLU3PNS:a three-dimensional thin layer and parabolized Navier-Strokes solver using the MUSCL upwind scheme[R].AIAA 91-0728,1991.
|
| [15] |
Coles D.Measurements in the boundary layer on a smooth flat plate in supersonic flow:Ⅰ the problem of the turbulent boundary layer[R].[S.l.]:Jet Propulsion Laboratory Report No.20-69,1953.
|
| [16] |
Settles G S,Williams D R,Baca B K,et al.Reattachment of a compressible turbulent free sheer layer[J].AIAA Journal,1982,20(1):60-67.
|
| [17] |
赵慧勇,雷波,乐嘉陵.非线性EASM在激波与湍流边界层相互作用中的数值应用[J].航空动力学报,2011,26(4):861-866. ZHAO Huiyong,LEI Bo,LE Jialing.Numerical application of nonlinear EASM model to the interaction between shock waves/turbulent boundary layer[J].Journal of Aerospace Power,2011,26(4):861-866.(in Chinese)
|
| [18] |
赵慧勇,雷波,乐嘉陵.非对称交叉激波和湍流边界层相互作用的数值研究[J].航空动力学报,2009,24(10):2184-2188. ZHAO Huiyong,LEI Bo,LE Jialing.Numerical investigation of interaction between asymmetric crossing shock waves/turbulent boundary layer[J].Journal of Aerospace Power,2009,24(10):2184-2188.(in Chinese)
|