{"created":"2023-06-19T07:35:59.079703+00:00","id":161,"links":{},"metadata":{"_buckets":{"deposit":"e1e4ce87-012a-419a-bd1a-720e3c0bd10a"},"_deposit":{"created_by":15,"id":"161","owners":[15],"pid":{"revision_id":0,"type":"depid","value":"161"},"status":"published"},"_oai":{"id":"oai:nias.repo.nii.ac.jp:00000161","sets":["6:22:28"]},"author_link":["81","82","83","84","85"],"control_number":"161","item_1_biblio_info_14":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2009-03-24","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"1","bibliographicPageEnd":"46","bibliographicPageStart":"37","bibliographicVolumeNumber":"49","bibliographic_titles":[{"bibliographic_title":"長崎総合科学大学紀要","bibliographic_titleLang":"ja"},{"bibliographic_title":"Bulletin of the Nagasaki Institute of Applied Science","bibliographic_titleLang":"en"}]}]},"item_1_creator_6":{"attribute_name":"著者名(日)","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"星, 光","creatorNameLang":"ja"},{"creatorName":"ホシ, ヒカル","creatorNameLang":"ja-Kana"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"岩堀, 豊","creatorNameLang":"ja"},{"creatorName":"イワホリ, ユタカ","creatorNameLang":"ja-Kana"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"石川, 隆司","creatorNameLang":"ja"},{"creatorName":"イシカワ, タカシ","creatorNameLang":"ja-Kana"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"矢島, 浩","creatorNameLang":"ja"},{"creatorName":"ヤジマ, ヒロシ","creatorNameLang":"ja-Kana"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"渡邊, 栄一","creatorNameLang":"ja"},{"creatorName":"ワタナベ, エイイチ","creatorNameLang":"ja-Kana"}],"nameIdentifiers":[{},{}]}]},"item_1_description_12":{"attribute_name":"抄録(英)","attribute_value_mlt":[{"subitem_description":"Tensile tests were carried out using specimen similar to repair part of the CFRP structural component of airplane. The specimen were made by two different methods, that is, one is \"autoclave repair specimen\" performed by exclusive equipment of the airplane body maker, and the other is \"heat blanket repair specimen\" by manual labor at operation spot. In addition, \"autoclave repair specimen\" with impact damage was also tested. \n　As a result, the influences of repair method and impact damage on tensile strength of scarf repair part were clarified.","subitem_description_language":"en","subitem_description_type":"Other"}]},"item_1_publisher_20":{"attribute_name":"発行者","attribute_value_mlt":[{"subitem_publisher":"長崎総合科学大学図書刊行委員会","subitem_publisher_language":"ja"}]},"item_1_source_id_13":{"attribute_name":"雑誌書誌ID","attribute_value_mlt":[{"subitem_source_identifier":"AN00177878","subitem_source_identifier_type":"NCID"}]},"item_1_source_id_19":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0387527X","subitem_source_identifier_type":"PISSN"}]},"item_1_text_10":{"attribute_name":"著者所属(英)","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency"},{"subitem_text_language":"en","subitem_text_value":"Nagasaki Institute of Applied Science"},{"subitem_text_language":"en","subitem_text_value":"Nagasaki Institute of Applied Science"}]},"item_1_text_9":{"attribute_name":"著者所属(日)","attribute_value_mlt":[{"subitem_text_language":"ja","subitem_text_value":"宇宙航空研究開発機構"},{"subitem_text_language":"ja","subitem_text_value":"宇宙航空研究開発機構"},{"subitem_text_language":"ja","subitem_text_value":"宇宙航空研究開発機構"},{"subitem_text_language":"ja","subitem_text_value":"長崎総合科学大学"},{"subitem_text_language":"ja","subitem_text_value":"長崎総合科学大学"}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2013-11-07"}],"displaytype":"detail","filename":"49巻1号37～46.pdf","filesize":[{"value":"4.7 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"CFRP構造部材修理部の引張強さに関する実験的研究","url":"https://nias.repo.nii.ac.jp/record/161/files/49巻1号37～46.pdf"},"version_id":"385a219e-917c-461f-98eb-74ffd59d6d7e"}]},"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":"departmental bulletin paper","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"CFRP構造部材修理部の引張強さに関する実験的研究","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"CFRP構造部材修理部の引張強さに関する実験的研究","subitem_title_language":"ja"},{"subitem_title":"Experimental study on tensile strength of repair part for CFRP structural component of airplane","subitem_title_language":"en"}]},"item_type_id":"1","owner":"15","path":["28"],"pubdate":{"attribute_name":"PubDate","attribute_value":"2013-11-07"},"publish_date":"2013-11-07","publish_status":"0","recid":"161","relation_version_is_last":true,"title":["CFRP構造部材修理部の引張強さに関する実験的研究"],"weko_creator_id":"15","weko_shared_id":-1},"updated":"2024-03-15T03:02:38.999619+00:00"}