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姜宗林 [2]
张子健 [2]
刘云峰 [1]
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Source Publication：AEROSPACE SCIENCE AND TECHNOLOGY
Creator：姜宗林
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Funding Project：National Natural Science Foundation of China[11532014]
Community：高温气体动力学国家重点实验室
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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)
Adobe PDF(2608Kb)
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View/Download：270/113
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Submit date：2020/11/30
Oblique detonation engine
Pre-injection
Detonative combustion
Mixing
Hydrogen
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)
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Adobe PDF(2165Kb)
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View/Download：410/94
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Submit date：2019/09/09
Shock reflection
Vibration excitation
Mach reflection
Transition criterion
Hypersonic flow
