{"created":"2023-06-20T14:47:24.189361+00:00","id":15068,"links":{},"metadata":{"_buckets":{"deposit":"3d609189-63a2-4494-952a-b0f886026d2f"},"_deposit":{"created_by":1,"id":"15068","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"15068"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00015068","sets":["1543:1671:1682","1887:1891"]},"author_link":["137033","137035","137036","137031","137032","137034"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"A Numerical Study on Debonding at the neiborhood of the Cap of Cryogenic Filament Wound Composite Pressure Vessel"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2009-03","bibliographicIssueDateType":"Issued"},"bibliographicVolumeNumber":"24","bibliographic_titles":[{"bibliographic_title":"宇宙構造・材料シンポジウム"},{"bibliographic_title":"Symposium on Aerospace Structure and Materials","bibliographic_titleLang":"en"}]}]},"item_5_description_14":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）","attribute_value_mlt":[{"subitem_description":"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)","subitem_description_type":"Other"}]},"item_5_description_15":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）（英）","attribute_value_mlt":[{"subitem_description":"24th Symposium on Aerospace Structure and Materials (December 12, 2008. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)), Sagamihara, Kanagawa Japan","subitem_description_type":"Other"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"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.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0064731009","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構宇宙科学研究本部"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)"}]},"item_5_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AA11398254","subitem_source_identifier_type":"NCID"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"上智大学理工学部"},{"subitem_text_value":"上智大学大学院"},{"subitem_text_value":"宇宙航空研究開発機構総合技術研究本部"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Faculty of Science and Technology, Sophia University"},{"subitem_text_language":"en","subitem_text_value":"Graduate School, Sophia University"},{"subitem_text_language":"en","subitem_text_value":"Institute of Aerospace Technology, Japan Aerospace Exploration Agency (JAXA)"}]},"item_access_right":{"attribute_name":"アクセス権","attribute_value_mlt":[{"subitem_access_right":"metadata only access","subitem_access_right_uri":"http://purl.org/coar/access_right/c_14cb"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"末益, 博志"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"和羅, 貴之"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"青木, 雄一郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Suemasu, Hiroshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Wara, Takayuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Aoki, Yuichiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Pressure vessel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Cryogenic temperature","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Debonding","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Energy release rate","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Finite element analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"jpn"}]},"item_resource_type":{"attribute_name":"資源タイプ","attribute_value_mlt":[{"resourcetype":"conference paper","resourceuri":"http://purl.org/coar/resource_type/c_5794"}]},"item_title":"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","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"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"}]},"item_type_id":"5","owner":"1","path":["1682","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"15068","relation_version_is_last":true,"title":["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"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T05:24:26.298926+00:00"}