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| Simulation on Three-Dimensional Shock Interactions and Aerodynamic Heating Between Body and Wing 期刊论文 AIAA JOURNAL, 2021, 页码: 12 Authors: Lin MY(林明月); Wang C(王春); Peng J(彭俊); Jiang ZL(姜宗林) Adobe PDF(4805Kb)  |  Favorite  |  View/Download:324/60  |  Submit date:2022/01/12 |
| 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) Adobe PDF(1333Kb)  |  Favorite  |  View/Download:555/146  |  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:315/75  |  Submit date:2018/10/30 Body And Wing Flow Field Hypersonic Flow Shock/shock Interaction Wave Configurations |
| 超声速三维进气道内激波干扰的研究 期刊论文 推进技术, 2017, 期号: 12, 页码: 6 Authors: 项高翔; 王春; 汪运鹏; 姜宗林 Adobe PDF(1393Kb)  |  Favorite  |  View/Download:485/102  |  Submit date:2017/12/22 高超声速流动 箱式进气道 侧壁压缩进气道 波系结构 流场区域 |
| 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) View  |  Adobe PDF(207Kb)  |  Favorite  |  View/Download:471/113  |  Submit date:2018/01/04 |
| 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:494/121  |  Submit date:2016/12/08 3d Asymmetrical Shock/shock Interaction Spatial-dimension Reduction Mach Reflection Flow Field Theoretical Analysis |
| On the numerical technique for the simulation of hypervelocity test flows 期刊论文 Computers & Fluids, 2015, 卷号: 106, 页码: 12-18 Authors: Hu ZM(胡宗民); Wang C(王春); Jiang ZL(姜宗林); Khoo BC; Hu ZM(胡宗民) View  |  Adobe PDF(1617Kb)  |  Favorite  |  View/Download:1583/921  |  Submit date:2014/11/27 Hypervelocity Test Flow Dcd Scheme Flux-splitting Spurious Oscillation |
| Self-organized generation of transverse waves in diverging cylindrical detonations 期刊论文 Combustion and Flame, 2009, 期号: 156, 页码: 1653–1661 Authors: Jiang ZL(姜宗林); Han GL(韩桂来); Wang C(王春); Zhang F(张凡) Adobe PDF(1273Kb)  |  Favorite  |  View/Download:1388/435  |  Submit date:2009/12/08 Cylindrical Detonation |
| 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:957/162  |  Submit date:2009/08/03 Supersonic Mixing Flame Holder "swallowtail" Cavity Combustion Ignition Numerical Simulation |
| 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 Authors: Hu ZM(胡宗民); Myong R S; Wang C(王春); Cho T H; Jiang ZL(姜宗林) View  |  Adobe PDF(954Kb)  |  Favorite  |  View/Download:211/84  |  Submit date:2020/08/26 Shock Shock Interaction Oscillation Hypersonic Double-wedge Numerical Study |