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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  
Monte Carlo modeling of electron density in hypersonic rarefied gas flows 会议论文
the 29th International Symposium on Rarefied Gas Dynamics, Xi'an, China, July13-18, 2014
作者:  Fan J(樊菁);  Zhang YH(张羽淮);  Jiang JZ(蒋建政)
浏览  |  Adobe PDF(835Kb)  |  收藏  |  浏览/下载：661/175  |  提交时间：2015/01/21
Hypersonic Rarefied Gas Flow  Electron Density  Dsmc  Tss  Ram-c Ii Flight Test  
Study of the coupling between real gas effects and rarefied effects on hypersonic aerodynamics 会议论文
28th International Symposium on Rarefied Gas Dynamics (RGD), Zaragoza, SPAIN, JUL 09-13, 2012
作者:  Chen S(陈松);  Hu Y(胡远);  Sun QH(孙泉华);  Chen, S (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(465Kb)  |  收藏  |  浏览/下载：888/249  |  提交时间：2013/02/26
Hypersonic Flow  Real Gas Effects  Rarefied Gas Effects  Coupling Mechanism  Flow  
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  
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