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刘云峰 [4]
姜宗林 [4]
张子健 [2]
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Creator:刘云峰
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Creator:姜宗林
Document Type:期刊论文
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Formation of stabilized oblique detonation waves in a combustor
期刊论文
COMBUSTION AND FLAME, 2021, 卷号: 223, 页码: 423-436
Authors:
Zhang ZJ(张子健)
;
Wen, Chihyung
;
Zhang WS(张文硕)
;
Liu YF(刘云峰)
;
Jiang ZL(姜宗林)
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View/Download:363/92
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Submit date:2021/03/03
Oblique detonation wave
Combustor
Oblique detonation engine
Normal detonation wave
Boundary layer separation
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)
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Submit date:2020/08/26
Scramjet engines
Shock-induced combustion ramjet engines
Supersonic combustion
Chapman-Jouguet detonation
Theoretical analysis on deflagration-to-detonation transition
期刊论文
CHINESE PHYSICS B, 2018, 卷号: 27, 期号: 8, 页码: 84703
Authors:
Liu YF(刘云峰)
;
Shen H(沈还)
;
Zhang DL(张德良)
;
Jiang ZL(姜宗林)
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Submit date:2018/10/30
deflagration
detonation
deflagration-to-detonation transition
Concept of non-ablative thermal protection system for hypersonic vehicles
期刊论文
AIAA Journal, 2013, 卷号: 51, 期号: 3, 页码: 584-590
Authors:
Liu YF(刘云峰)
;
Jiang ZL(姜宗林)
;
Jiang, ZL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temperature Gas Dynam, Beijing 100190, Peoples R China.
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View/Download:1403/503
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Submit date:2013/04/07
Flow Fields
Flow Visualization
Hypersonic Aerodynamics
Hypersonic Vehicles
Mach Number
Shock Waves
Thermal Insulating Materials
Engineering Applications
Experimental Datum
Hypersonic Wind Tunnels
Numerical Results
Stagnation Points
Thermal Protection
Thermal Protection System
Working Pressures