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A Data-Correlation Model of Aerodynamic Heating Based on Globally Optimal Learning Method 会议论文
16th International Conference on Natural Computation, Fuzzy Systems and Knowledge Discovery (ICNC-FSKD 2020), 西安，中国, 19-21 December 2020
Authors:  Chen Z(陈阵);  Li S(李森);  Luo ZT(罗长童);  Jiang ZL(姜宗林)
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Comparative Heat Flux Measurement of a Sharp Cone Between Three Hypersonic Test Facilities at LHD 会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
Authors:  Wang Q(汪球);  Lu P(卢盼);  Li JW(栗继伟);  Wu S(吴松);  Li JP(李进平);  Zhao W(赵伟);  Jiang ZL(姜宗林)
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Pressure and Heat Flux Calibration of the Long-test-duration Hypervelocity Detonation-driven Shock Tunnel 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:  Wang Q(汪球);  Li JW;  Lu P;  Li JP(李进平);  Zhao W(赵伟);  Jiang ZL(姜宗林)
View  |  Adobe PDF(679Kb)  |  Favorite  |  View/Download：414/78  |  Submit date：2018/01/16
Calibration  Detonation  Heat Transfer  Nozzles  Spacecraft  Supersonic Aerodynamics  Thermodynamics  Uncertainty Analysis  
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.
View  |  Adobe PDF(764Kb)  |  Favorite  |  View/Download：380/108  |  Submit date：2016/06/28
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：263/51  |  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)
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Heat Transfer Problems Induced By Multi-shocks Interaction 会议论文
2nd International Symposium on Computational Mechanics, Hong Kong, PEOPLES R CHINA, NOV 30-DEC 03, 2009
Authors:  Jiang ZL(姜宗林);  Li JP(李进平);  Jiang ZL
Adobe PDF(257Kb)  |  Favorite  |  View/Download：821/247  |  Submit date：2009/07/23
Heat Transfer  Hypersonic Flow  Multi-shock Interaction  Thermal Protection  Cylindrical Leading-edge  Shock/shock Interferences