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中国科学院力学研究所机构知识库
Knowledge Management System of Institue of Mechanics, CAS
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State Key ... [9]
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刘云峰 [9]
姜宗林 [9]
张子健 [4]
马凯夫 [3]
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Creator:刘云峰
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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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Submit date:2021/03/03
Oblique detonation wave
Combustor
Oblique detonation engine
Normal detonation wave
Boundary layer separation
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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Submit date:2020/11/30
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)
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Submit date:2020/08/26
Scramjet engines
Shock-induced combustion ramjet engines
Supersonic combustion
Chapman-Jouguet detonation
斜爆轰发动机流动机理分析
期刊论文
气体物理, 2019, 卷号: 4, 期号: 03, 页码: 1-10
Authors:
马凯夫
;
张子健
;
刘云峰
;
姜宗林
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Submit date:2019/09/12
斜爆轰发动机
超燃冲压发动机
超声速燃烧
爆轰波
激波诱导燃烧
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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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
Concept of non-ablative thermal protection system for hypersonic vehicles
会议论文
17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, San Francisco, CA, APR 11-14, 2011
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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Submit date:2013/12/12
气相爆轰物理的若干研究进展
期刊论文
力学进展, 2012, 卷号: 42, 期号: 2, 页码: 129-140
Authors:
姜宗林
;
滕宏辉
;
刘云峰
Adobe PDF(2609Kb)
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Submit date:2013/01/16
气相爆轰波
爆轰波形成
爆轰波传播
热点起爆
胞格结构
稳定性
Study on the Mechanism of Detonation to Quasi-detonation Transition
会议论文
2nd International Symposium on Computational Mechanics, Hong Kong, PEOPLES R CHINA, NOV 30-DEC 03, 2009
Authors:
Liu YF(刘云峰)
;
Jiang ZL(姜宗林)
;
Liu YF
Adobe PDF(288Kb)
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Submit date:2009/07/23
Detonation
Quasi-detonation
Thermal Choking