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Advances in critical technologies for hypersonic and high-enthalpy wind tunnel 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3027-3038
Authors:  Jiang ZL(姜宗林);  Hu ZM(胡宗民);  Wang YP(汪运鹏);  Han GL(韩桂来)
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High-enthalpy flow  Hypersonic wind tunnel  Aerospace vehicle  Aerodynamic balance  Heat flux sensor  Optical measurement technique  
Parameter-correlation study on shock-shock interaction using a machine learning method 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 107, 页码: 106247
Authors:  Peng J(彭俊);  Luo ZT(罗长童);  Han ZJ(韩子健);  Hu ZM(胡宗民);  Han GL(韩桂来);  Jiang ZL(姜宗林)
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Shock-shock interaction  Machine learning  Hypersonic flow  Impinging jet  Genetic programming  Triple point  
On theory and methods for advanced detonation-driven hypervelocity shock tunnels 期刊论文
NATIONAL SCIENCE REVIEW, 2020, 卷号: 7, 期号: 7, 页码: 1198-1207
Authors:  Jiang ZL(姜宗林);  Li JP(李进平);  Hu ZM(胡宗民);  Liu YF(刘云峰);  Yu HR(俞鸿儒)
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hypervelocity  shock tunnel  detonation driver  flight condition  tailored condition  test facilities  
Numerical investigation of the effects of shock tube geometry on the propagation of an ideal blast wave profile 期刊论文
SHOCK WAVES, 2017, 卷号: 27, 期号: 5, 页码: 771-779
Authors:  Li, X. D.;  Hu ZM(胡宗民);  Jiang ZL(姜宗林);  Hu, ZM (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.;  Hu, ZM (reprint author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China.
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Blast Wave Profile  Biological Shock Tube  Blast Overpressure  Geometrical Configuration  
Starting Process in a Large-Scale Shock Tunnel 期刊论文
AIAA Journal, 2016, 卷号: 54, 期号: 5, 页码: 1240-1249
Authors:  Wang YP(汪运鹏);  Hu ZM(胡宗民);  Liu YF(刘云峰);  Jiang ZL(姜宗林)
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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.
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3d Asymmetrical Shock/shock Interaction  Spatial-dimension Reduction  Mach Reflection  Flow Field  Theoretical Analysis  
Development of the detonation-driven expansion tube for orbital speed experiments 期刊论文
Science China-Technological Sciences, 2015, 卷号: 58, 期号: 4, 页码: 695-700
Authors:  Jiang ZL(姜宗林);  Wu B(吴波);  Gao YL;  Zhao W(赵伟);  Hu ZM(胡宗民);  Jiang, ZL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Detonation Driver  Shock-expansion Tube  High-enthalpy Flow  Test Flow  
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)
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Hypervelocity Test Flow  Dcd Scheme  Flux-splitting  Spurious Oscillation  
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)
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Shock  Shock Interaction  Oscillation  Hypersonic  Double-wedge  Numerical Study  
Numerical Study on the Performance of Nozzle Flow for Supersonic Chemical Oxygen-Iodine Lasers 期刊论文
ACTA MECHANICA SINICA, 2008, 卷号: 24, 期号: 2, 页码: 133-142
Authors:  Hu ZM(胡宗民);  Lv JM(吕俊明);  Jiang ZL(姜宗林);  Myong RS;  Cho TH;  Jiang, ZL (reprint author), CAS, Inst Mech, LHD, Beijing 100080, Peoples R China.
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Chemical Oxygen-iodine Laser (Coil)  Numerical Simulation  Small Signal Gains  Unsteady Structures