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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：243/92  |  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：660/175  |  提交时间：2015/01/21
Hypersonic Rarefied Gas Flow  Electron Density  Dsmc  Tss  Ram-c Ii Flight Test  
Oscillation-free adaptive simulation of compressible two-fluid flows with different types of equation of state 会议论文
8th Workshop on Synthetic Turbulence Models, Paris, FRANCE, JUN 28-29, 2012
作者:  Zheng HW(郑洪伟);  Shu C;  Chew YT;  Qin N;  Zheng HW(郑洪伟)
Adobe PDF(972Kb)  |  收藏  |  浏览/下载：891/277  |  提交时间：2013/03/01
Compressible Multifluids  Adaptive  Equation Of State  
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
作者:  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.
Adobe PDF(645Kb)  |  收藏  |  浏览/下载：879/219  |  提交时间：2013/02/26
Hypersonic Flow  Flat Plate  Bridging Formula  Dsmc Method  
Shock pressure induced by glass-confined laser shock peening: Experiments, modeling and simulation 会议论文
9th Workshop on Piezoresponse Force Microscopy (PFM)/10th International Symposium on Ferroic Domains, Prague, CZECH REPUBLIC, SEP 22-24, 2010
作者:  Wu XQ(吴先前);  Duan ZP(段祝平);  Song HW(宋宏伟);  Wei YP(魏延鹏);  Wang X(王曦);  Huang CG(黄晨光);  Wu, XQ (reprint author), Chinese Acad Sci, Inst Mech, Key Lab Hydrodynam & Ocean Engn, Beijing 100190, Peoples R China
Adobe PDF(814Kb)  |  收藏  |  浏览/下载：1026/256  |  提交时间：2013/02/26
Doppler Effect  Dynamic Response  Glass  Glass Lasers  Velocimeters  Velocity Control  Velocity Measurement  Analytical Model  Diagnostic Capabilities  Empirical Formulas  Exponential Decays  Free Surface Velocity  Free Surfaces  Laser Shock Peening  Ls-dyna  Particle Velocities  Photonic Doppler Velocimetry  Plasma Pressures  Shock Pressure  Short Time Scale  Stress Wave  Target Materials  Temporal Profile  Wave Experiments  Stress Waves  Plasma  Generation  Aluminum  Geometry  Alloys  Metals  
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：693/171  |  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：491/198  |  提交时间：2014/01/14
Aeroacoustics  Caa  Ce/se Method  Acoustic Wave  Supersonic Jet  
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：781/187  |  提交时间：2013/02/26
Hypersonic  Blunt Leading Edge  Aerothermodynamic  Inverse Design  Homotopy