{"created":"2023-06-20T15:03:20.025595+00:00","id":32514,"links":{},"metadata":{"_buckets":{"deposit":"1fe6d66e-e9e8-4977-b9e2-b8c868377a63"},"_deposit":{"created_by":1,"id":"32514","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"32514"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00032514","sets":["1887:1890","1896:1898:1899:1910"]},"author_link":["409642","409639","409640","409641","409635","409637","409636","409638"],"item_9_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Minimum Weight Design of Stiffened Cylindrical Shells under Pure Bending"}]},"item_9_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1979-11","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"4","bibliographicPageEnd":"878","bibliographicPageStart":"865","bibliographicVolumeNumber":"15","bibliographic_titles":[{"bibliographic_title":"東京大学宇宙航空研究所報告"}]}]},"item_9_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"曲げモーメント75 ton-mを受けるフレーム(円きょう)と縦通材で補強された直径2,440 mmの円筒殼の最小重量設計を行い,設計の妥当性を縮尺比1/3のモデルによる実験により確認した.","subitem_description_type":"Abstract"}]},"item_9_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A method of structural optimization is applied in designing circular cylindrical shells under bending. The cylindrical shells are stiffened both longitudinally and circumferentially. A one-third scale model of the designed cylindrical shell has been made and tested to check the validity of the design.","subitem_description_type":"Other"}]},"item_9_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: SA0125803000","subitem_description_type":"Other"}]},"item_9_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"東京大学宇宙航空研究所"}]},"item_9_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0563-8100","subitem_source_identifier_type":"ISSN"}]},"item_9_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN00161914","subitem_source_identifier_type":"NCID"}]},"item_9_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"東京大学宇宙航空研究所"},{"subitem_text_value":"東京大学宇宙航空研究所"},{"subitem_text_value":"東京大学宇宙航空研究所"},{"subitem_text_value":"東京大学宇宙航空研究所"}]},"item_9_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Institute of Space and Aeronautical Science, University of Tokyo"},{"subitem_text_language":"en","subitem_text_value":"Institute of Space and Aeronautical Science, University of Tokyo"},{"subitem_text_language":"en","subitem_text_value":"Institute of Space and Aeronautical Science, University of Tokyo"},{"subitem_text_language":"en","subitem_text_value":"Institute of Space and Aeronautical Science, University of Tokyo"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"平野, 陽一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"小野田, 淳次郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"橋元, 保雄"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"相原, 賢二"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"HIRANO, Yoichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"ONODA, Junjiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"HASHIMOTO, Yasuo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"AIHARA, Kenji","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2020-01-24"}],"displaytype":"detail","filename":"SA0125803.pdf","filesize":[{"value":"1.2 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"SA0125803.pdf","url":"https://jaxa.repo.nii.ac.jp/record/32514/files/SA0125803.pdf"},"version_id":"d80837cb-29eb-4790-bd43-b93c03262156"}]},"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":"<論文>曲げモーメントを受ける補強円筒殼の最小重量設計","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"<論文>曲げモーメントを受ける補強円筒殼の最小重量設計"}]},"item_type_id":"9","owner":"1","path":["1890","1910"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"32514","relation_version_is_last":true,"title":["<論文>曲げモーメントを受ける補強円筒殼の最小重量設計"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T00:30:25.898506+00:00"}