{"created":"2023-06-20T14:36:52.423722+00:00","id":3240,"links":{},"metadata":{"_buckets":{"deposit":"96f6adfe-8a87-42f0-9812-061fbcb6466d"},"_deposit":{"created_by":1,"id":"3240","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"3240"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00003240","sets":["1398:1530:1532","1543:1874:1876","1887:1891","9:789:806:1978"]},"author_link":["12436","12428","12427","12433","12437","12431","12434","12429","12430","12438","12432","12435"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Study of Influence of Phase-angle Differences on Aerodynamic Interactions between Rotors"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2017-12-27","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"59","bibliographicPageStart":"53","bibliographicVolumeNumber":"JAXA-SP-17-004","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料: 第49回流体力学講演会/第35回航空宇宙数値シミュレーション技術シンポジウム論文集"},{"bibliographic_title":"JAXA Special Publication: Proceedings of the 49th Fluid Dynamics Conference / the 35th Aerospace Numerical Simulation Symposium","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":"第49回流体力学講演会/第35回航空宇宙数値シミュレーション技術シンポジウム (2017年6月28日-36日. 国際オリンピック記念青少年総合センター), 渋谷区, 東京","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":"49th Fluid Dynamics Conference /the 35th Aerospace Numerical Simulation Symposium (June 28-30, 2017. National Olympics Memorial Youth Center), Shibuya-ku, Tokyo, Japan","subitem_description_type":"Other"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Aerodynamic interactions between 6 rotors on a multi-copter type drone are numerically simulated. The phase angles of the rotors and the pitch angles of the rotor blades are varied. The total thrust changes about 3% due to phase angle differences. With the phase angle differences between the neighboring rotors fixed to the smallest angle about 0 degrees (Worstcase), as the pitch angle approaches 16deg, the oscillating forces become relatively low. This property of the oscillating forces depends on the phase angle differences between the rotors, which is considered to be due to the shape change of the tip vortices.","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: AA1730011006","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-17-004","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":"大阪府立大学"},{"subitem_text_value":"宇宙航空研究開発機構(JAXA)"},{"subitem_text_value":"名古屋大学"},{"subitem_text_value":"電力中央研究所 (CRIEPI)"},{"subitem_text_value":"金沢大学"},{"subitem_text_value":"大阪府立大学"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Osaka Prefecture University"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Nagoya University"},{"subitem_text_language":"en","subitem_text_value":"Central Research Institute of Electric Power Industry (CRIEPI)"},{"subitem_text_language":"en","subitem_text_value":"Kanazawa University"},{"subitem_text_language":"en","subitem_text_value":"Osaka Prefecture University"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"田中, 陸久"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"田辺, 安忠"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"砂田, 茂"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"米澤, 宏一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"得竹, 浩"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"新井, 隆景"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tanaka, Riku","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tanabe, Yasutada","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sunada, Shigeru","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yonezawa, Koichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tokutake, Hiroshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Arai, Takakage","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":"2020-01-15"}],"displaytype":"detail","filename":"AA1730011006.pdf","filesize":[{"value":"2.7 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"AA1730011006.pdf","url":"https://jaxa.repo.nii.ac.jp/record/3240/files/AA1730011006.pdf"},"version_id":"54d51dde-5f8f-4742-b647-f8be4bd4a92b"}]},"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":"ロータ間の空力干渉における位相角差の影響に対する考察","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"ロータ間の空力干渉における位相角差の影響に対する考察"}]},"item_type_id":"5","owner":"1","path":["1532","1876","1891","1978"],"pubdate":{"attribute_name":"公開日","attribute_value":"2017-12-28"},"publish_date":"2017-12-28","publish_status":"0","recid":"3240","relation_version_is_last":true,"title":["ロータ間の空力干渉における位相角差の影響に対する考察"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T09:06:31.015099+00:00"}