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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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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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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.
Adobe PDF(1027Kb)  |  Favorite  |  View/Download：802/291  |  Submit date：2007/06/15