{"created":"2023-06-20T15:14:29.446234+00:00","id":44484,"links":{},"metadata":{"_buckets":{"deposit":"91d3c387-44d9-40b9-8611-26057cb96c97"},"_deposit":{"created_by":1,"id":"44484","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"44484"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00044484","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["469695","469694","469693","469696","469692","469697"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Full-Scale Fatigue Test of YS-11A-500/600 Turboprop Transport Wing(I Safe-Life Fatigue Test Loads and Test Method)"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1971-07","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"23","bibliographicVolumeNumber":"241","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory TR-241","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"I was required to perform the full-scale fatigue test(the safe-life and fail-safe tests) of YS-11-500/600 transport wing, because the maximum take-off weight of the aircraft was increased by 2.2 tons compared with the prototype and accordingly some strength members of the wing were re-designed. In order to perform the full-scale fatigue test, the safe-life fatigue loads and test method were investigated and the fatigue loads and program sequence of the test are decided were follows:(1)Gust loads, maneuver loads and ground-air-ground loads are taken into consideration as fatigue test loads. (2)The flight loads of one block corresponding to 100 flights are applied in an ascending-descending sequence in which ground-air-ground loads are inserted.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTR0241000","subitem_description_type":"Other"}]},"item_3_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: NAL TR-241","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory(NAL)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0389-4010","subitem_source_identifier_type":"ISSN"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"航空宇宙技術研究所機体第一部"},{"subitem_text_value":"航空宇宙技術研究所機体第一部"},{"subitem_text_value":"航空宇宙技術研究所機体第一部"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"First Airframe Division, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"First Airframe Division, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"First Airframe Division, National Aerospace Laboratory(NAL)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"竹内, 和之"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"野原, 利雄"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"朝田, 洋雄"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"TAKEUCHI, Kazuyuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"NOHARA, Toshio","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"ASADA, Hiroo","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":"2020-01-29"}],"displaytype":"detail","filename":"naltr00241.pdf","filesize":[{"value":"3.3 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr00241.pdf","url":"https://jaxa.repo.nii.ac.jp/record/44484/files/naltr00241.pdf"},"version_id":"6b3c27ea-be33-4cc6-aab6-c4a4b0d63ef0"}]},"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":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"YS-11A-500/600型主翼疲れ試験Ⅰ.セーフライフ試験荷重と試験方式","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"YS-11A-500/600型主翼疲れ試験Ⅰ.セーフライフ試験荷重と試験方式"}]},"item_type_id":"3","owner":"1","path":["1893","1917"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"44484","relation_version_is_last":true,"title":["YS-11A-500/600型主翼疲れ試験Ⅰ.セーフライフ試験荷重と試験方式"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:56:13.373774+00:00"}