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Numerical Study of Shock/Boundary Layer Interaction of Chemically Reacting Flow in Shock Tube 期刊论文
Procedia Engineering, 2015, 卷号: 126, 页码: 617-621
作者:  Chen S(陈松);  Sun QH(孙泉华)
浏览  |  Adobe PDF(671Kb)  |  收藏  |  浏览/下载：246/94  |  提交时间：2016/08/25
Shock/boundary-layer Interaction  Nonequilibrium Chemical Reactions  Shock Tube Flow  Weno Scheme  
Molecular simulation of small Knudsen number flows 会议论文
28th International Symposium on Rarefied Gas Dynamics (RGD), Zaragoza, SPAIN, JUL 09-13, 2012
作者:  Fei F(费飞);  Fan J(樊菁);  Fei, F (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(476Kb)  |  收藏  |  浏览/下载：643/148  |  提交时间：2013/02/26
Dsmc  Ip  Molecular Diffusion  Time Step  Cell Size  Rarefied-gas Flows  Low-reynolds-number  Statistical Simulation  Monte-carlo  Flat-plate  Model  
Mode Transition and Symmetry-Breaking in the Wake of a Flapping Foil 会议论文
6th International Conference on Fluid Mechanics, Guangzhou, PEOPLES R CHINA, JUN 30-JUL 03, 2011
作者:  He, GY (He G Y;  Zhang X(张星);  Zhang SG;  Wang Q
Adobe PDF(5337Kb)  |  收藏  |  浏览/下载：565/196  |  提交时间：2014/01/14
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
作者:  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
Adobe PDF(966Kb)  |  收藏  |  浏览/下载：694/171  |  提交时间：2013/02/26
Turbulent-boundary-layer  Direct Numerical-simulation  
One-Step Direct Aeroacoustic Simulation Using Space-Time Conservation Element and Solution Element Method 会议论文
6th International Conference on Fluid Mechanics, Guangzhou, PEOPLES R CHINA, JUN 30-JUL 03, 2011
作者:  Ho CY;  Leung RCK;  Zhou K;  Lam GCY;  Jiang ZL(姜宗林)
Adobe PDF(400Kb)  |  收藏  |  浏览/下载：493/199  |  提交时间：2014/01/14
Aeroacoustics  Caa  Ce/se Method  Acoustic Wave  Supersonic Jet  
LES of Asymmetric Wave-induced Flow 会议论文
6th International Conference on Fluid Mechanics, Guangzhou, PEOPLES R CHINA, JUN 30-JUL 03, 2011
作者:  Chen JB(陈江波);  Zhou JF(周济福);  Zhang Q;  Chen, JB (reprint author), Chinese Acad Sci, Inst Mech, Key Lab Environm Mech, Beijing 100190, Peoples R China.
Adobe PDF(382Kb)  |  收藏  |  浏览/下载：955/246  |  提交时间：2013/02/26
Large-eddy Simulation  Asymmetric Wave  The Degree Of Asymmetry  Reynolds Number  Oscillatory Boundary-layers  Model  
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
作者:  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)  |  收藏  |  浏览/下载：784/188  |  提交时间：2013/02/26
Hypersonic  Blunt Leading Edge  Aerothermodynamic  Inverse Design  Homotopy  
Primary study of aerodynamic performance evaluation and optimization of the high-speed train 会议论文
6th International Conference on Fluid Mechanics, Guangzhou, PEOPLES R CHINA, JUN 30-JUL 03, 2011
作者:  Wang XP(王秀平);  Cui K(崔凯);  Hu SC(胡守超);  Gao TY(高太元);  Yang GW(杨国伟);  Wang, XP (reprint author), Chinese Acad Sci, Inst Mech, LHD, Beijing 100190, Peoples R China.
Adobe PDF(349Kb)  |  收藏  |  浏览/下载：606/142  |  提交时间：2013/02/26
China Railways High-speed (Crh)  Nose Shape  Computational Fluid Mechanics  Optimization