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Effects of inflow Mach number on oblique detonation initiation with a two-step induction-reaction kinetic model 期刊论文
COMBUSTION AND FLAME, 2018, 卷号: 193, 页码: 246-256
Authors:  Yang PF;  Teng HH(滕宏辉);  Jiang ZL(姜宗林);  Ng HD
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Oblique detonation  Induction-reaction kinetics  Initiation length  Initiation structure  
高超声速条件下溢流液膜厚度测量方法 期刊论文
中国科学. 技术科学, 2018, 卷号: 48, 期号: 6, 页码: 629-638
Authors:  苑朝凯;  李进平;  陈宏;  姜宗林;  俞鸿儒
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高超声速热防护  主动冷却  液膜厚度  电导法  
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)
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Body And Wing  Flow Field  Hypersonic Flow  Shock/shock Interaction  Wave Configurations  
Numerical investigation of the axial impulse load during the startup in the shock tunnel 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 卷号: 73, 页码: 332-342
Authors:  Meng BQ(孟宝清);  Han GL(韩桂来);  Luo ZT(罗长童);  Jiang ZL(姜宗林)
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Hypersonic  Shock tunnel  Start-up process  Impulse force  Vibration  
高超声速溢流冷却实验研究 期刊论文
力学学报, 2018, 卷号: 50, 期号: 1, 页码: 1-8
Authors:  苑朝凯;  李进平;  陈宏;  姜宗林;  俞鸿儒
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高超声速热防护  主动冷却  溢流冷却  液膜  
A numerical study on the instability of oblique detonation waves with a two-step induction–reaction kinetic model 期刊论文
Proceedings of the Combustion Institute, 2018
Authors:  Yang PF(杨鹏飞);  Teng HH(滕红辉);  Ng HD;  Jiang ZL(姜宗林)
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AERODYNAMIC DRAG MEASUREMENT IN A HIGH-ENTHALPY SHOCK TUNNEL 会议论文
ASME Fluids Engineering Division Summer Meeting (FEDSM2018), Montreal, CANADA, JUL 15-20, 2018
Authors:  Wang YP(汪运鹏);  Jiang ZL(姜宗林);  Teng HH(滕宏辉)
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THE MECHANISM OF THREE-DIMENSION STEADY SHOCK WAVE INTERACTION 会议论文
ASME Fluids Engineering Division Summer Meeting (FEDSM2018), Montreal, CANADA, JUL 15-20, 2018
Authors:  Wang C(王春);  Yang RX(杨瑞欣);  Jiang ZL(姜宗林)
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