{"created":"2023-06-20T14:39:50.746005+00:00","id":6661,"links":{},"metadata":{"_buckets":{"deposit":"4e7eb6cb-4e23-43fe-9743-2ec2d4e7cdda"},"_deposit":{"created_by":1,"id":"6661","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"6661"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00006661","sets":["1887:1893","9:1368:1369:1370"]},"author_link":["34167","34166"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Aerodynamic Design of a 120-Seat Class Passenger Aircraft at Cruise"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2019-01-17","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"153","bibliographicPageStart":"1","bibliographicVolumeNumber":"JAXA-CR-18-001","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構契約報告"},{"bibliographic_title":"JAXA Contract Report","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The aerodynamic design of a 120-seat class passenger aircraft at cruise is conducted on the basis of its conceptual design data. The aircraft configuration has almost the same aerodynamic performances at cruise as existing aircraft, and it is used to evaluate the drag-reducing effects of newly-developed aerodynamic technologies with CFD and wind-tunnel testing.","subitem_description_type":"Other"}]},"item_3_description_18":{"attribute_name":"内容記述","attribute_value_mlt":[{"subitem_description":"形態: カラー図版あり","subitem_description_type":"Other"}]},"item_3_description_19":{"attribute_name":"内容記述（英）","attribute_value_mlt":[{"subitem_description":"Physical characteristics: Original contains color illustrations","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA1830012000","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: JAXA-CR-18-001","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構(JAXA)"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_3_source_id_22":{"attribute_name":"ISSNONLINE","attribute_value_mlt":[{"subitem_source_identifier":"2433-2240","subitem_source_identifier_type":"ISSN"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"宇宙航空研究開発機構航空技術部門航空システム研究ユニット(JAXA)"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Aviation Systems Research Unit, Aeronautical Technology Directorate, Japan Aerospace Exploration Agency (JAXA)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"野村, 聡幸"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nomura, Toshiyuki","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":"2020-01-16"}],"displaytype":"detail","filename":"AA1830012000.pdf","filesize":[{"value":"17.2 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"AA1830012000.pdf","url":"https://jaxa.repo.nii.ac.jp/record/6661/files/AA1830012000.pdf"},"version_id":"c1069b05-5f4c-4468-b200-a5a2405ebaf3"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Aerodynamic Design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Passenger Aircraft","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":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"120席級旅客機全機巡航形態の空力設計","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"120席級旅客機全機巡航形態の空力設計"}]},"item_type_id":"3","owner":"1","path":["1370","1893"],"pubdate":{"attribute_name":"公開日","attribute_value":"2019-01-17"},"publish_date":"2019-01-17","publish_status":"0","recid":"6661","relation_version_is_last":true,"title":["120席級旅客機全機巡航形態の空力設計"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:51:26.854468+00:00"}