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ArticleJ-GLOBAL ID:200902165016806499整理番号:97A0914395

超軌道速度再突入カプセル前面の空力加熱環境解析とアブレーションの影響

Prediction of Aerodynamic Heating Environment over Forebody of Super-orbital Reentry Capsule with Ablation Injection.

著者:鈴木宏二郎(東大)、藤田和央(宇宙科研)、安部隆士(宇宙科研)
資料名:流体力学講演会講演集 巻:29th ページ:205-208
発行年:1997年
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About J-GLOBAL

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J-GLOBAL links information that represents the key to research and development. For example, linking articles and patents with people (authors and inventors) enables the extraction of a sequence of information.
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The system enables searches of similar kinds of content through linkage with external sites.
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