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Hypersonic aerodynamics of a flat plate: bridging formula and wall temperature effects 会议论文
28th International Symposium on Rarefied Gas Dynamics (RGD), Zaragoza, SPAIN, JUL 09-13, 2012
Authors:  Hu Y(胡远);  Chen S(陈松);  Sun QH(孙泉华);  Hu, Y (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Hypersonic Flow  Flat Plate  Bridging Formula  Dsmc Method  
DNS of shock/boundary layer interaction flow in a supersonic compression ramp 会议论文
6th International Conference on Computational Fluid Dynamics, St Petersburg, RUSSIA, JUL 12-16, 2010
Authors:  Li XL(李新亮);  Fu DX(傅德薰);  Ma YW(马延文);  Liang X(梁贤);  Li, XL (reprint author), CAS, Inst Mech, LHD, Beijing 100190, Peoples R China
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Turbulent-boundary-layer  Direct Numerical-simulation  
Leading edge aerothermal inverse design of hyersonic vehicle based on homotopy optimization method 会议论文
6th International Conference on Fluid Mechanics, Guangzhou, PEOPLES R CHINA, JUN 30-JUL 03, 2011
Authors:  Cui K(崔凯);  Hu SC(胡守超);  Gao TY(高太元);  Wang XP(王秀平);  Yang GW(杨国伟);  Cui, K (reprint author), Chinese Acad Sci, Inst Mech, LHD, Beijing 100190, Peoples R China.
Adobe PDF(53Kb)  |  Favorite  |  View/Download：845/193  |  Submit date：2013/02/26
Hypersonic  Blunt Leading Edge  Aerothermodynamic  Inverse Design  Homotopy