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Numerical Investigation on Longitudinal Stage Separation of Spiked Two-Stage-to-Orbit Vehicle 期刊论文
Journal of Spacecraft and Rockets, 2023, 卷号: 60, 期号: 1, 页码: 215-229
Authors:  Wang Y(王粤);  Wang YP(汪运鹏);  Wang C(王春);  Jiang ZL(姜宗林)
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Multistage Launch Vehicle  Aerodynamic Characteristics  Shock Wave Interaction  Angle of Attack  Waverider  Boundary Layer Flow  Total Variation Diminishing  Adverse Pressure Gradient  Hypersonic Flows  Hypersonic Wind Tunnels  
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
Authors:  Xiang GX(项高翔);  Wang C(王春);  Teng HH(腾宏辉);  Jiang ZL(姜宗林)
View  |  Adobe PDF(1333Kb)  |  Favorite  |  View/Download：569/151  |  Submit date：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
Authors:  Xiang GX(项高翔);  Wang C(王春);  Teng HH(腾宏辉);  Jiang ZL(姜宗林)
Adobe PDF(1161Kb)  |  Favorite  |  View/Download：322/76  |  Submit date：2018/10/30
Body And Wing  Flow Field  Hypersonic Flow  Shock/shock Interaction  Wave Configurations  
Experimental and Numerical Study on Hypersonic Flow over Double-Wedge Configuration 期刊论文
AIAA Journal, 2017, 卷号: 55, 期号: 9, 页码: 3227-3230
Authors:  Meng BQ(孟宝清);  Han GL(韩桂来);  Yuan CK(苑朝凯);  Wang C(王春);  Jiang ZL(姜宗林)
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Investigations of Three-Dimensional Shock/Shock Interactions over Symmetrical Intersecting Wedges 期刊论文
AIAA JOURNAL, 2016, 卷号: 54, 期号: 5, 页码: 1472-1481
Authors:  Xiang GX(项高翔);  Wang C(王春);  Teng HH(滕宏辉);  Jiang ZL(姜宗林);  Wang, C (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(578Kb)  |  Favorite  |  View/Download：495/170  |  Submit date：2016/09/14
Ceramics  Thermal Shock  Size Effect  
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
Authors:  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.
View  |  Adobe PDF(995Kb)  |  Favorite  |  View/Download：508/124  |  Submit date：2016/12/08
3d Asymmetrical Shock/shock Interaction  Spatial-dimension Reduction  Mach Reflection  Flow Field  Theoretical Analysis  
Study on Mach stems induced by interaction of planar shock waves on two intersecting wedges 期刊论文
ACTA MECHANICA SINICA, 2016, 卷号: 32, 期号: 3, 页码: 362-368
Authors:  Xiang GX(项高翔);  Wang C(王春);  Teng HH(滕宏辉);  Yang Y;  Jiang ZL(姜宗林);  Wang, C (reprint author), Chinese Acad Sci, Inst Mech, 15 Beisihuan Xi Rd, Beijing 100190, Peoples R China.
View  |  Adobe PDF(1122Kb)  |  Favorite  |  View/Download：382/103  |  Submit date：2016/09/14
3d Shock/shock Interaction  Mach Interaction  Spatial Dimension Reduction  
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
Authors:  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)  |  Favorite  |  View/Download：908/201  |  Submit date：2013/01/18
Asymmetric Shock Waves  Mach Reflection  Detachment Criterion  Mach Reflection  Transition  Boundaries  Domains  Gas  
Numerical Investigation On The Flowfield Of "Swallowtail" Cavity For Supersonic Mixing Enhancement 期刊论文
Acta Mechanica Sinica, 2009, 页码: 37-44
Authors:  Wang C(王春);  Jiang ZL(姜宗林);  Hu Z;  Lu J;  Wang C
Adobe PDF(620Kb)  |  Favorite  |  View/Download：965/165  |  Submit date：2009/08/03
Supersonic Mixing  Flame Holder  "swallowtail" Cavity  Combustion Ignition  Numerical Simulation