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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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力学所知识产出(19... [2]
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reprint au... [3]
姜宗林 [3]
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Indexed By:EI
Source Publication:AIAA Journal
Creator:reprint author
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Creator:姜宗林
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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:1412/507
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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
Forward-Running Detonation Drivers for High-Enthalpy Shock Tunnels
期刊论文
AIAA Journal, 2002, 卷号: 40, 期号: 10, 页码: 2009-2016
Authors:
Jiang ZL(姜宗林)
;
Zhao W(赵伟)
;
Wang C(王超)
;
Takayama K
;
Jiang, ZL (reprint author), Chinese Acad Sci, Inst Mech, Key Lab High Temp Gasdynam, Beijing 100080, Peoples R China.
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Submit date:2007/06/15
Micro-shock waves generated inside a fluid jet impinging on plane wall
期刊论文
AIAA Journal, 2001, 卷号: 39, 期号: 3, 页码: 424-430
Authors:
Jagadeesh G
;
Onodera O
;
Ogawa T
;
Takayama K
;
Jiang ZL(姜宗林)
;
Jagadeesh, G (reprint author), Tohoku Univ, Shock Wave Res Ctr, Inst Fluid Sci, Sendai, Miyagi 9808577, Japan.
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Submit date:2007/06/15