IMECH-IR
(本次检索基于用户作品认领结果)

浏览/检索结果: 共9条,第1-9条 帮助

限定条件            
已选(0)清除 条数/页:   排序方式:
Numerical study on aerodynamic performance of waverider with a new bluntness method 期刊论文
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2021, 卷号: 235, 期号: 10, 页码: 1225-1233
作者:  Qu ZP;  Xiao HD;  Lv MY;  Li GL(李广利);  Cui K(崔凯)
Adobe PDF(1179Kb)  |  收藏  |  浏览/下载:227/97  |  提交时间:2021/06/11
bluntness method  computational fluid dynamics  hypersonic  volume  Waverider  
Experimental investigation of a hypersonic I-shaped configuration with a waverider compression surface 期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2020, 卷号: 63, 期号: 5, 页码: 3
作者:  Li GL(李广利);  Cui K(崔凯);  Xu YZ(徐应洲);  Wang HX(王浩祥);  Yang J(杨靖);  Xu XG(许先贵)
Adobe PDF(661Kb)  |  收藏  |  浏览/下载:382/92  |  提交时间:2020/05/18
Hypersonic I-shaped aerodynamic configurations 期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2018, 卷号: 61, 期号: 2, 页码: 24722
作者:  Cui K(崔凯);  Xiao Y(肖尧);  Xu YZ;  Li GL
浏览  |  Adobe PDF(665Kb)  |  收藏  |  浏览/下载:431/130  |  提交时间:2018/10/30
High-Pressure Capturing Wing Configurations 期刊论文
AIAA JOURNAL, 2017, 卷号: 55, 期号: 6, 页码: 1909-1919
作者:  Cui K(崔凯);  Li GL;  Xiao Y(肖尧);  Xu YZ;  Cui,K(reprint author), Chinese Acad Sci, Inst Mech
浏览  |  Adobe PDF(671Kb)  |  收藏  |  浏览/下载:636/177  |  提交时间:2017/07/24
Conceptual design and aerodynamic evaluation of hypersonic airplane with double flanking air inlets 期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2013, 卷号: 56, 期号: 8, 页码: 1980-1988
作者:  Cui K(崔凯);  Hu SC(胡守超);  Li GL(李广利);  Qu ZP(屈志朋);  Situ M;  Cui, K (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(1426Kb)  |  收藏  |  浏览/下载:880/296  |  提交时间:2013/09/27
Hypersonic  Flanking Air Inlet  Waverider  Computational Fluid Dynamics(Cfd)  
Aerodynamic optimization and evaluation for the three-dimensional afterbody/nozzle integrated configuration of hypersonic vehicles 期刊论文
Chinese Science Bulletin, 2012, 卷号: 57, 期号: 8, 页码: 849-857
作者:  Gao TY(高太元);  Cui K(崔凯);  Wang XP(王秀平);  Hu SC(胡守超);  Yang GW(杨国伟);  Ren L;  kcui@imech.ac.cn
Adobe PDF(985Kb)  |  收藏  |  浏览/下载:1138/312  |  提交时间:2012/09/26
Hypersonic Afterbody/Nozzle Integrated Configuration Single Expanding Ramp Nozzle Optimization Computational Fluid Dynamics  
Shape Optimization for Hypersonic Arc-Wing Missiles 期刊论文
Journal of Spacecraft and Rockets, 2010, 卷号: 47, 期号: 4, 页码: 694-700
作者:  Cui K(崔凯);  Yang GW(杨国伟)
Adobe PDF(4987Kb)  |  收藏  |  浏览/下载:1217/234  |  提交时间:2010/09/07
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:840/216  |  提交时间:2009/08/03
Waverider  Hypersonic  Computational Fluid Dynamics  Navier-stokes Solver  Design  Cone  
The Effect of Conical Flowfields on the Performance of Waveriders at Mach 6 期刊论文
Chinese Science Bulletin, 2007, 卷号: 52, 期号: 1, 页码: 57-64
作者:  Cui K(崔凯);  Yang GW(杨国伟);  Cui, K (reprint author), Chinese Acad Sci, Inst Mech, Key Lab High Temp Gas Dynam, Beijing 100080, Peoples R China.
Adobe PDF(655Kb)  |  收藏  |  浏览/下载:730/255  |  提交时间:2007/06/15