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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
Authors:  Chen S(陈松);  Sun QH(孙泉华)
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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
Authors:  Fan J(樊菁);  Zhang YH(张羽淮);  Jiang JZ(蒋建政)
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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
Authors:  Zheng HW(郑洪伟);  Shu C;  Chew YT;  Qin N;  Zheng HW(郑洪伟)
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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
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
Adobe PDF(966Kb)  |  Favorite  |  View/Download：720/185  |  Submit date：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
Authors:  Ho CY;  Leung RCK;  Zhou K;  Lam GCY;  Jiang ZL(姜宗林)
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Aeroacoustics  Caa  Ce/se Method  Acoustic Wave  Supersonic Jet  
Optimization of the upper surface of hypersonic vehicle based on CFD analysis 会议论文
6th International Conference on Fluid Mechanics, Guangzhou, PEOPLES R CHINA, JUN 30-JUL 03, 2011
Authors:  Gao TY(高太元);  Cui K(崔凯);  Hu SC(胡守超);  Wang XP(王秀平);  Yang GW(杨国伟);  Gao, TY (reprint author), Chinese Acad Sci, Inst Mech, Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(305Kb)  |  Favorite  |  View/Download：736/199  |  Submit date：2013/02/26
Hypersonic  Shape Optimization  Sequential Quadratic Programming (Sqp)