{"created":"2023-06-20T14:47:22.511973+00:00","id":15031,"links":{},"metadata":{"_buckets":{"deposit":"22568c3c-9135-4231-979a-e1d2514e8253"},"_deposit":{"created_by":1,"id":"15031","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"15031"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00015031","sets":["1543:1671:1681","1887:1891"]},"author_link":["136760","136766","136767","136763","136764","136762","136761","136765"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"An experimental study on onset of skin/stiffener delamination in a stiffened panel under compressive loading"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2010-03","bibliographicIssueDateType":"Issued"},"bibliographicVolumeNumber":"25","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25回)(2009年12月4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":"25th Symposium on Aerospace Structure and Materials (December 4, 2009. 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":"The objectives of the present study are to clarify the failure mechanism of stiffened panel under compressive load. The compression tests of the stiffened panels with and without impact damage were conducted. The experiment showed that the failure started from the debonding between the stiffener flange and skin panel due to the significant bending caused by the buckling. A simultaneous unstable damage propagation in the transverse direction all the through-width of panel to the final failure occurred following the debondlng. It showed that the key of the compressive strength of the buckled stiffened panels was the debonding between the skin panel and the flange of the stiffener. Following the fact, bending tests for specimens with three different thickness of skin panels were carried out to reveal the mechanism of the onset and the growth of skin/stiffener debondlng. Owing to the singular nature of the stress at the bonded edge, a limiting energy release rate as zero crack length was used. Only the energy release rate, showing some correlation with the failure loads obtained, was not sufficient to explain the onset of the debonding.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0064732009","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"},{"subitem_text_value":"宇宙航空研究開発機構"},{"subitem_text_value":"上智大学"},{"subitem_text_value":"宇宙航空研究開発機構"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Sophia University"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Sophia University"},{"subitem_text_language":"en","subitem_text_value":"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":"田中, 太朗"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"青木, 雄一郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"末益, 博志"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"永尾, 陽典"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tanaka, Taro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Aoki, Yuichiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Suemasu, Hiroshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nagao, Yosuke","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"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":"補強部材の剥離発生メカニズムに関する一考察","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"補強部材の剥離発生メカニズムに関する一考察"}]},"item_type_id":"5","owner":"1","path":["1681","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"15031","relation_version_is_last":true,"title":["補強部材の剥離発生メカニズムに関する一考察"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T05:24:59.213360+00:00"}