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A numerical study of oblique detonation re-stabilization by expansion waves 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 卷号: 122, 页码: 8
Authors:  Yao KP(姚克鹏);  Wang C(王春);  Jiang ZL(姜宗林)
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Oblique detonation  Stationary  Thermal choking  Expansion waves  
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  
Numerical investigation of a Mach 9 oblique detonation engine with fuel pre-injection 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 105, 页码: 9
Authors:  Zhang ZJ(张子健);  Ma KF(马凯夫);  Zhang WS(张文硕);  Han X(韩鑫);  Liu YF(刘云峰);  Jiang ZL(姜宗林)
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Oblique detonation engine  Pre-injection  Detonative combustion  Mixing  Hydrogen  
Aerodynamic principles of shock-induced combustion ramjet engines 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 103, 页码: 8
Authors:  Ma KF(马凯夫);  Zhang ZJ(张子健);  Liu YF(刘云峰);  Jiang ZL(姜宗林)
Adobe PDF(1657Kb)  |  Favorite  |  View/Download:275/97  |  Submit date:2020/08/26
Scramjet engines  Shock-induced combustion ramjet engines  Supersonic combustion  Chapman-Jouguet detonation  
A theoretical and computational study of the vibration excitation on the transition criteria of shock wave reflections 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 89, 页码: 299-306
Authors:  Peng J(彭俊);  Zhang ZJ(张子健);  Hu ZM(胡宗民);  Jiang ZL(姜宗林)
View  |  Adobe PDF(2165Kb)  |  Favorite  |  View/Download:410/94  |  Submit date:2019/09/09
Shock reflection  Vibration excitation  Mach reflection  Transition criterion  Hypersonic flow  
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)
View  |  Adobe PDF(1937Kb)  |  Favorite  |  View/Download:266/86  |  Submit date:2018/10/30
Hypersonic  Shock tunnel  Start-up process  Impulse force  Vibration  
Numerical study of inflow equivalence ratio inhomogeneity on oblique detonation formation in hydrogen-air mixtures 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 卷号: 71, 页码: 256-263
Authors:  Fang YS(方宜申);  Hu ZM(胡宗民);  Teng HH(滕宏辉);  Jiang ZL(姜宗林);  Ng HD
View  |  Adobe PDF(2663Kb)  |  Favorite  |  View/Download:382/95  |  Submit date:2018/02/08
Oblique Detonation  Equivalence Ratio  Mixture Inhomogeneity  Detailed Chemistry