{"created":"2023-06-20T15:17:11.085036+00:00","id":47338,"links":{},"metadata":{"_buckets":{"deposit":"0253c619-b63b-4f74-b492-acda21aca7cb"},"_deposit":{"created_by":1,"id":"47338","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"47338"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00047338","sets":["1398:1530:2108","1543:1874:2109","1887:1891","9:789:2068:2106"]},"author_link":["532214","532218","532221","532210","532212","532213","532211","532215","532217","532219","532216","532220"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Wind Tunnel Testing of a Multicopter with Box Wing"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2021-02-08","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"136","bibliographicPageStart":"129","bibliographicVolumeNumber":"JAXA-SP-20-008","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料: 流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2020オンライン論文集"},{"bibliographic_title":"JAXA Special Publication: Proceedings of Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2020 Online","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":"流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2020オンライン (2020年9月28日-30日. 日本航空宇宙学会 : 宇宙航空研究開発機構(JAXA)オンライン会議)","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":"Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2020 Online (September 28-30, 2020. The Japan Society for Aeronautical and Space Sciences : Japan Aerospace Exploration Agency (JAXA), Online meeting)","subitem_description_type":"Other"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The aerodynamic characteristics including high angle of attack condition up to 95 degrees of the Box wing, in which the electric multicopter was surrounded by a duct like annular wing, were acquired by a wind tunnel test for use in a quiet Electric Vertical Take Off and Landing (eVTOL) aircraft. The Box wing is expected to be quieter by shielding the aerodynamic noise from the propeller. It was shown that the Box wing has a mild stall characteristic, the lift of the Box wing increases due to the effect of the propeller thrust, and that the current Box wing has no effect of improving the hovering ability.","subitem_description_type":"Other"}]},"item_5_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_5_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_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA2030013017","subitem_description_type":"Other"}]},"item_5_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: JAXA-SP-20-008","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(JAXA)"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_5_source_id_22":{"attribute_name":"ISSNONLINE","attribute_value_mlt":[{"subitem_source_identifier":"2433-2232","subitem_source_identifier_type":"ISSN"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"宇宙航空研究開発機構(JAXA)"},{"subitem_text_value":"電力中央研究所(CRIEPI)"},{"subitem_text_value":"工学院大学"},{"subitem_text_value":"工学院大学"},{"subitem_text_value":"宇宙航空研究開発機構(JAXA)"},{"subitem_text_value":"宇宙航空研究開発機構(JAXA)"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Central Research Institute of Electric Power Industry (CRIEPI)"},{"subitem_text_language":"en","subitem_text_value":"Kogakuin University"},{"subitem_text_language":"en","subitem_text_value":"Kogakuin University"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_5_version_type_30":{"attribute_name":"著者版フラグ","attribute_value_mlt":[{"subitem_version_resource":"http://purl.org/coar/version/c_970fb48d4fbd8a85","subitem_version_type":"VoR"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"嶋, 英志"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"米澤, 宏一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"西田, 涼馬"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"佐藤, 允"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"堤, 誠司"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"藤本, 圭一郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"SHIMA, Eiji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"YONEZAWA, Koichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"NISHIDA, Ryoma","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"SATO, Makoto","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"TSUTSUMI, Seiji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"FUJIMOTO, Keiichiro","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":"2021-02-08"}],"displaytype":"detail","filename":"AA2030013017.pdf","filesize":[{"value":"3.1 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"AA2030013017.pdf","url":"https://jaxa.repo.nii.ac.jp/record/47338/files/AA2030013017.pdf"},"version_id":"a57c40bd-505d-4b8e-9c0c-cc2fee2a8be5"}]},"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":"Box翼を持つマルチコプタの風洞試験","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Box翼を持つマルチコプタの風洞試験"}]},"item_type_id":"5","owner":"1","path":["1891","2106","2108","2109"],"pubdate":{"attribute_name":"公開日","attribute_value":"2021-02-08"},"publish_date":"2021-02-08","publish_status":"0","recid":"47338","relation_version_is_last":true,"title":["Box翼を持つマルチコプタの風洞試験"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:41:01.650658+00:00"}