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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  
New trends in fluid mechanics research : proceeding of the fifth international conference on fluid mechanics (Shanghai, 2007) 专著
Beijing : New York:Tsinghua Univ. Press, Springer, 2008
作者:  editors, 庄逢甘;  Li JC(李家春)
Adobe PDF(117163Kb)  |  收藏  |  浏览/下载：1200/29  |  提交时间：2009/07/06
Research on three-dimensional scramjet inlet 会议论文
14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference, 2006, Beijing, China, 20-23 April 2006
作者:  Yue LJ(岳连捷);  Xiao YB(肖雅彬);  Chen LH(陈立红);  Xiang AY(向安宇);  Zhang XY(张新宇)
浏览  |  Adobe PDF(1265Kb)  |  收藏  |  浏览/下载：239/71  |  提交时间：2015/09/21
Research on three-dimensional scramiet inlet 会议论文
14th AIAA/AHI International Space Planes and Hypersonics Systems Technologies Conference, Canberra, Australia, November 6, 2006 - November 9, 2006
作者:  Yue LJ(岳连捷);  Chen LH(陈立红);  Xiao YB;  Gong P;  Chang XY(张新宇)
浏览  |  Adobe PDF(1267Kb)  |  收藏  |  浏览/下载：132/43  |  提交时间：2017/06/01
Capture Ratio  Mass Flow  Surface Oil Dot Visualization  Three-dimensional Scramjet Inlet  
A numerical analysis of vortex dislocation in wake-type flow with different spanwise nonuniformity 图书章节
2005
作者:  Ling GC(凌国灿)
Adobe PDF(311Kb)  |  收藏  |  浏览/下载：127/28  |  提交时间：2020/11/19
Direct numerical simulation  Transition behavior  Two distinct types of vortex dislocation  Wake-type flow  
3D Finite Volume Scheme for Czochralski Single Crystal Growth 会议论文
Sixth World Congress on Computational Mechanics in Conjunction with the Second Asian-Pacific Congress on Computational Mechanics,Sept. 5-10, 2004, Beijing,China, Beijing,China, Sept. 5-10, 2004
作者:  Lu J;  Zhang ZB(张自兵);  Chen QS(陈启生);  Chen QS(陈启生)
Adobe PDF(73Kb)  |  收藏  |  浏览/下载：658/111  |  提交时间：2007/12/18
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  
Wave dynamic processes induced by a supersonic projectile dischargingfrom a shock tube 期刊论文
Physics of Fluids, 2003, 卷号: 15, 期号: 6, 页码: 1665-1675
作者:  Jiang ZL(姜宗林)
浏览  |  Adobe PDF(1120Kb)  |  收藏  |  浏览/下载：823/281  |  提交时间：2007/06/15
高超声速乘波飞行器气动实验研究 期刊论文
宇航学报, 2002, 卷号: 23, 期号: 6, 页码: 82-85,90
作者:  姚文秀;  雷麦芳;  杨耀栋;  王发民
Adobe PDF(364Kb)  |  收藏  |  浏览/下载：536/170  |  提交时间：2010/05/03
乘波飞行器  气动构形  气动实验  预压缩性能  
可压缩轴对称射流空间发展的直接数值模拟 学位论文
博士后论文，北京: 中国科学院力学研究所, 2002
作者:  刘明宇
Adobe PDF(10746Kb)  |  收藏  |  浏览/下载：367/3  |  提交时间：2009/04/13