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ArticleJ-GLOBAL ID:200902165212577112整理番号:01A0649931

Modeling of propellant leakage through matrix cracks in composite laminates.

複合材積層材料の母材亀裂を通しての推進剤漏洩のモデル化

著者:KUMAZAWA H(National Aerospace Lab., Tokyo, JPN)、AOKI T(Univ. Tokyo, Tokyo, JPN)、ISHIKAWA T(National Aerospace Lab., Tokyo, JPN)・・・
資料名:Collect Tech Pap AIAA/ASME/ASCE/AHS/ASC Struct Struct Dyn Mater Conf AIAA/ASME/AHS Adapt Struct Forum 巻:42nd 号:Vol.1 ページ:307-311
発行年:2001年
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