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極低温用フィラメントワインディング圧力容器の口金部のはく離に関する一考察
https://jaxa.repo.nii.ac.jp/records/15068
https://jaxa.repo.nii.ac.jp/records/15068bf569a1a-b7fa-4348-a401-8c3bad99abd4
Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 極低温用フィラメントワインディング圧力容器の口金部のはく離に関する一考察 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Pressure vessel | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Cryogenic temperature | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Debonding | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Energy release rate | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Finite element analysis | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_5794 | |||||
資源タイプ | conference paper | |||||
アクセス権 | ||||||
アクセス権 | metadata only access | |||||
アクセス権URI | http://purl.org/coar/access_right/c_14cb | |||||
その他のタイトル(英) | ||||||
その他のタイトル | A Numerical Study on Debonding at the neiborhood of the Cap of Cryogenic Filament Wound Composite Pressure Vessel | |||||
著者 |
末益, 博志
× 末益, 博志× 和羅, 貴之× 青木, 雄一郎× Suemasu, Hiroshi× Wara, Takayuki× Aoki, Yuichiro |
|||||
著者所属 | ||||||
上智大学理工学部 | ||||||
著者所属 | ||||||
上智大学大学院 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構総合技術研究本部 | ||||||
著者所属(英) | ||||||
en | ||||||
Faculty of Science and Technology, Sophia University | ||||||
著者所属(英) | ||||||
en | ||||||
Graduate School, Sophia University | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Aerospace Technology, Japan Aerospace Exploration Agency (JAXA) | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構宇宙科学研究本部 | |||||
出版者(英) | ||||||
出版者 | Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
宇宙構造・材料シンポジウム en : Symposium on Aerospace Structure and Materials 巻 24, 発行日 2009-03 |
|||||
会議概要(会議名, 開催地, 会期, 主催者等) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 宇宙構造・材料シンポジウム(第24回)(2008年12月12日、宇宙航空研究開発機構宇宙科学研究本部) | |||||
会議概要(会議名, 開催地, 会期, 主催者等)(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 24th Symposium on Aerospace Structure and Materials (December 12, 2008. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)), Sagamihara, Kanagawa Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Debonding problem of cryogenic carbon fiber reinforced composite vessels with aluminium liner subjected to thermal stress and internal pressure is studied fracture-mechanically by using a finite element analysis. The dome portions of the vessel whose shape is derived based on the orthotropic membrane theory [1] are assumed to be axi-symmetric and the geometric nonlinearity is considered. The energy release rate is obtained by using virtual crack closure technique. The energy release rate due to the thermal stress is found to be significant to cause debonding at the cap portion. For types of shapes are studied to show the feasibility of the reduction of the energy release rate by the design of the boss shape. | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11398254 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0064731009 |