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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.
Adobe PDF(5046Kb)  |  Favorite  |  View/Download：1418/509  |  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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Numerical Study on the Performance of Nozzle Flow for Supersonic Chemical Oxygen-Iodine Lasers 期刊论文
ACTA MECHANICA SINICA, 2008, 卷号: 24, 期号: 2, 页码: 133-142
Authors:  Hu ZM(胡宗民);  Lv JM(吕俊明);  Jiang ZL(姜宗林);  Myong RS;  Cho TH;  Jiang, ZL (reprint author), CAS, Inst Mech, LHD, Beijing 100080, Peoples R China.
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Chemical Oxygen-iodine Laser (Coil)  Numerical Simulation  Small Signal Gains  Unsteady Structures