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宋宏伟 [1]
王睿星 [1]
郑洪伟 [1]
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Source Publication：INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES
Creator：宋宏伟
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Language：英语
Community：高温气体动力学国家重点实验室
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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)
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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)
