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Numerical study of the oscillations induced by shock/shock interaction in hypersonic double-wedge flows 期刊论文
SHOCK WAVES, 2008, 卷号: 18, 期号: 1, 页码: 41-51
作者:  Hu ZM(胡宗民);  Myong R S;  Wang C(王春);  Cho T H;  Jiang ZL(姜宗林)
浏览  |  Adobe PDF(954Kb)  |  收藏  |  浏览/下载：194/79  |  提交时间：2020/08/26
Shock  Shock Interaction  Oscillation  Hypersonic  Double-wedge  Numerical Study  
Research Progress On Thermal Protection Materials And Structures Of Hypersonic Vehicles 期刊论文
Applied Mathematics and Mechanics (English Edition), 2008, 页码: 51-60
作者:  Yang YZ(杨亚政);  Yang JL;  Fang DN;  Yang, YZ (reprint author), Beijing Univ Aeronaut & Astronaut, Sch Aeronaut Sci & Technol, Beijing 100083, Peoples R China.
Adobe PDF(601Kb)  |  收藏  |  浏览/下载：911/357  |  提交时间：2009/08/03
Hypersonic Vehicle  High-temperature  Thermal Protection  High-temperature Ceramics  Carbon/carbon Composites  Oxidation Behavior  Creep-behavior  Carbon  Microstructure  Diboride  Kinetics  
Research progress on high-enthalpy and hypersonic flows 会议论文
5th International Conference on Fluid Mechanics, Shanghai, PEOPLES R CHINA, AUG 15-19, 2007
作者:  Jiang ZL(姜宗林);  Yu HR(俞鸿儒);  Lin ZB(林贞彬);  Jiang Z
Adobe PDF(690Kb)  |  收藏  |  浏览/下载：875/238  |  提交时间：2009/07/23
Hypersonic Flows  Detonation Driver  Shock-reflected Tunnels  Shock-expanded Tube  Heat Transfer  
Waverider configurations derived from general conical flowfields 期刊论文
Acta Mechanica Sinica, 2007, 卷号: 23, 期号: 3, 页码: 247-255
作者:  Cui K(崔凯);  Zhao DX;  Yang GW(杨国伟);  Cui, K (reprint author), Dalian Univ Technol, State Key Lab Struct Anal Ind Equipment, Dalian 116023, Peoples R China.
Adobe PDF(649Kb)  |  收藏  |  浏览/下载：821/209  |  提交时间：2009/08/03
Waverider  Hypersonic  Computational Fluid Dynamics  Navier-stokes Solver  Design  Cone  
Three-dimensional sidewall-compression scramjet inlet CFD simulation and experimental comparison 会议论文
39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2003, Huntsville, AL, United states, July 20, 2003 - July 23, 2003
作者:  Chen F;  Chen LH(陈立红);  Chang XY(张新宇)
浏览  |  Adobe PDF(4312Kb)  |  收藏  |  浏览/下载：145/61  |  提交时间：2017/06/01
Compressible Navier-stokes  Computational Studies  Experimental Comparison  Experimental Investigations  Flow Charac-teristics  Hypersonic Propulsion Test Facility  Performance Parameters  Scramjet Inlets  
Development of the facility for model scramjet testing 会议论文
10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference 2001, Kyoto, Japan, April 24, 2001 - April 27, 2001
作者:  Chang XY(张新宇);  Chen LH(陈立红);  Yu G(俞刚);  Qian DX(钱大兴)
浏览  |  Adobe PDF(872Kb)  |  收藏  |  浏览/下载：212/80  |  提交时间：2017/06/01
Chinese Academy Of Sciences  Enthalpy Flow  Hypersonic Propulsion Test Facility  Performance Tests  Scramjet Testing  Supersonic Combustion  Total Pressure  Total Temperatures