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Comparison of Strategies for Coupled Flow-Thermal Analysis of Thermal Protection System at Hypersonic Flight Condition
期刊论文
INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, 2020, 卷号: 21, 期号: 2, 页码: 347-362
Authors:
Wang RX(王睿星)
;
Wang, ZW
;
Zheng HW(郑洪伟)
;
Song HW(宋宏伟)
Adobe PDF(4182Kb)
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View/Download:291/88
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Submit date:2020/06/22
Coupled flow-thermal analysis
Thermal protection system
Basic direct correction method (BDCM)
Improved DCM (IDCM)
Iteration solution method (ISM)
Numerical investigation on the thermal protection mechanism for blunt body with forward-facing cavity
期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2016, 卷号: 59, 期号: 7, 页码: 1120-1129
Authors:
Li, XD
;
Hu ZM(胡宗民)
;
Jiang ZL(姜宗林)
;
Hu, ZM (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
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View/Download:292/95
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Submit date:2016/09/14
Hypersonic Flow
Aerodynamic Heating
Thermal Protection System
Forward-facing Cavity
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:1397/500
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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