Chinese | English

Search in the results

IMECH-IR

Browse/Search Results:  1-7 of 7 Help

Filters                    
Selected(0)Clear Items/Page:    Sort:
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)
View  |  Adobe PDF(671Kb)  |  Favorite  |  View/Download：293/118  |  Submit date：2016/08/25
Shock/boundary-layer Interaction  Nonequilibrium Chemical Reactions  Shock Tube Flow  Weno Scheme  
Key issues of ultraviolet radiation of OH at high altitudes 会议论文
the 29th International Symposium on Rarefied Gas Dynamics, Xi'an, China, July13-18, 2014
Authors:  Zhang YH(张羽淮);  Wan T(万田);  Jiang JZ(蒋建政);  Fan J(樊菁)
View  |  Adobe PDF(853Kb)  |  Favorite  |  View/Download：701/198  |  Submit date：2015/01/21
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)
Adobe PDF(972Kb)  |  Favorite  |  View/Download：934/291  |  Submit date：2013/03/01
Compressible Multifluids  Adaptive  Equation Of State  
Numerical Simulation of a Low-power Hydrazine Arcjet Thruster 会议论文
18TH INTERNATIONAL VACUUM CONGRESS (IVC-18), Beijing, PEOPLES R CHINA, AUG 23-27, 2010
Authors:  Wang HX;  Geng JY;  Chen Xi;  Pan WX(潘文霞);  Wang HX (reprint author), Beijing Univ Aeronaut & Astronaut, Sch Astronaut, Beijing 100191, Peoples R China.
Adobe PDF(212Kb)  |  Favorite  |  View/Download：1173/345  |  Submit date：2011/01/12
Low-power Arcjet  Plasma Flow And Heat Transfer  Numerical Modeling  Hydrazine  
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：733/188  |  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)
Adobe PDF(400Kb)  |  Favorite  |  View/Download：556/233  |  Submit date：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
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：848/194  |  Submit date：2013/02/26
Hypersonic  Blunt Leading Edge  Aerothermodynamic  Inverse Design  Homotopy