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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]
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Creator:刘云峰
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Criteria for hypersonic airbreathing propulsion and its experimental verification
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 3, 页码: 94-104
Authors:
Jiang ZL(姜宗林)
;
Zhang ZJ(张子健)
;
Liu YF(刘云峰)
;
Wang C(王春)
;
Luo ZT(罗长童)
Adobe PDF(1806Kb)
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Submit date:2021/05/17
Concept demonstration
Hypersonic propulsion
Oblique detonation engine
Scramjet
Shock wave
Supersonic combustion
Wind tunnel test
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)
Adobe PDF(3599Kb)
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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
Application of CE/SE method to gas-particle two-phase detonations under an Eulerian-Lagrangian framework
期刊论文
JOURNAL OF COMPUTATIONAL PHYSICS, 2019, 卷号: 394, 页码: 18-40
Authors:
Zhang ZJ(张子健)
;
Wen CY
;
Liu YF(刘云峰)
;
Zhang DL(张德良)
;
Jiang ZL(姜宗林)
Adobe PDF(4374Kb)
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Submit date:2019/09/09
Two-phase detonation
CE/SE
Eulerian-Lagrangian
MPI
Aluminum-air 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)
Adobe PDF(699Kb)
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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
Conceptual Study on Non-ablative TPS for Hypersonic Vehicles
会议论文
17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, San Francisco, CA, United states, APR 11-14, 2011
Authors:
Jiang ZL(姜宗林)
;
Liu YF(刘云峰)
;
Han GL(韩桂来)
;
Jiang ZL(姜宗林)
Adobe PDF(1058Kb)
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Submit date:2014/02/24
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