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Thermal–Structural Coupled Analysis and Design of a Reentry Capsule with Ablative Thermal Protection Systems

International Journal of Aeronautical and Space Sciences Pub Date : 2024-07-23 DOI:10.1007/s42405-024-00789-3
Yerin Park, Eui-Sup Shin
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带有烧蚀热保护系统的再入太空舱的热结构耦合分析与设计
本文章由计算机程序翻译，如有差异，请以英文原文为准。
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International Journal of Aeronautical and Space Sciences
International Journal of Aeronautical and Space Sciences
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