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Starting Process in a Large-Scale Shock Tunnel 会议论文
22nd AIAA Computational Fluid Dynamics Conference, Dallas, TX, JUN 22-26, 2015
Authors:  Wang YP;  Hu ZM(胡宗民);  Liu YF(刘云峰);  Jiang ZL(姜宗林);  Wang, YP (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
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Numerical investigation of the starting process in a long-test-duration hypersonic shock tunnel 会议论文
22nd AIAA Computational Fluid Dynamics Conference, 2015, Dallas, TX, United states, June 22, 2015 - June 26, 2015
Authors:  Wang YP(汪运鹏);  Hu ZM(胡宗民);  Liu YF(刘云峰);  Jiang ZL(姜宗林)
View  |  Adobe PDF(5104Kb)  |  Favorite  |  View/Download：272/54  |  Submit date：2017/05/05
Inviscid Flows  Numerical Investigations  Outlet Diameters  Reflected Shock Waves  Simulated Results  Starting Process  Transmitted Shock  Unsteady Nozzle Flow  
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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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)
View  |  Adobe PDF(1058Kb)  |  Favorite  |  View/Download：546/138  |  Submit date：2014/02/24
Ignition of hydrogen suddenly leaked from a high pressure tank 会议论文
45th AIAA Aerospace Sciences Meeting 2007, Reno, NV, United states, January 8, 2007 - January 11, 2007
Authors:  Aizawa K;  Pinto D;  Liu YF(刘云峰);  Sato H;  Hayashi AK
View  |  Adobe PDF(202Kb)  |  Favorite  |  View/Download：159/83  |  Submit date：2017/06/01
Geometrical Conditions  Pressure Tank  Spouting  Tube Length