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Three-dimensional shock wave configurations induced by two asymmetrical intersecting wedges in supersonic flow 期刊论文
SHOCK WAVES, 2018, 卷号: 28, 期号: 2, 页码: 311-319
作者:  Xiang GX(项高翔);  Wang C(王春);  Teng HH(腾宏辉);  Jiang ZL(姜宗林)
浏览  |  Adobe PDF(1333Kb)  |  收藏  |  浏览/下载:529/136  |  提交时间:2018/10/30
Supersonic Flow  3d Shock/shock Interaction  3d Asymmetrical Wave Configurations  Spatial Dimension Reduction  
Shock/shock interactions between bodies and wings 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2018, 卷号: 31, 期号: 2, 页码: 255-261
作者:  Xiang GX(项高翔);  Wang C(王春);  Teng HH(腾宏辉);  Jiang ZL(姜宗林)
浏览  |  Adobe PDF(1161Kb)  |  收藏  |  浏览/下载:303/74  |  提交时间:2018/10/30
Body And Wing  Flow Field  Hypersonic Flow  Shock/shock Interaction  Wave Configurations  
Theoretical solutions to three-dimensional asymmetrical shock/shock interaction 期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2016, 卷号: 59, 期号: 8, 页码: 1208-1216
作者:  Xiang GX(项高翔);  Wang C(王春);  Hu ZM(胡宗民);  Li XD;  Jiang ZL(姜宗林);  Wang, C (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam LHD, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(995Kb)  |  收藏  |  浏览/下载:480/116  |  提交时间:2016/12/08
3d Asymmetrical Shock/shock Interaction  Spatial-dimension Reduction  Mach Reflection  Flow Field  Theoretical Analysis  
Analytical and numerical investigations of the reflection of asymmetric nonstationary shock waves 期刊论文
SHOCK WAVES, 2012, 卷号: 22, 期号: 5, 页码: 435-449
作者:  Yang Y(杨旸);  Wang C(王春);  Jiang ZL(姜宗林);  Yang, Y;  Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
Adobe PDF(1485Kb)  |  收藏  |  浏览/下载:855/195  |  提交时间:2013/01/18
Asymmetric Shock Waves  Mach Reflection  Detachment Criterion  Mach Reflection  Transition  Boundaries  Domains  Gas  
Computational Confirmation of AN Abnormal Mach Reflection Wave Configuration 期刊论文
PHYSICS OF FLUIDS, 2009, 卷号: 21, 期号: 1, 页码: 011702
作者:  Hu ZM(胡宗民);  Wang C(王春);  Zhang Y;  Myong RS;  Myong, RS (reprint author), Gyeongsang Natl Univ, ReCAPT, Jinju 660701, South Korea.
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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:198/81  |  提交时间:2020/08/26
Shock  Shock Interaction  Oscillation  Hypersonic  Double-wedge  Numerical Study