{"created":"2023-06-20T14:36:52.378441+00:00","id":3239,"links":{},"metadata":{"_buckets":{"deposit":"474e3bc0-27d1-4b4c-bcff-ed993c99167c"},"_deposit":{"created_by":1,"id":"3239","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"3239"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00003239","sets":["1398:1530:1532","1543:1874:1876","1887:1891","9:789:806:1978"]},"author_link":["12426","12423","12424","12425"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Enhancement of a Rotorcraft CFD tool for Ducted Rotors"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2017-12-27","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"52","bibliographicPageStart":"47","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-35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":"A rotorcraft flow solver, rFlow3D, has been extended for ducted rotors. A circular grid topology has been implemented to enable a body grid solver to compute the duct shape. A background cylindrical grid is adopted for fine grid resolution of the clearance between the blade tip and the duct. Octree based interpolation processing is utilized for a fast interpolation between the body grid and the background cylindrical grid. The validation about the new adopted grid and the prediction accuracy of the ducted rotor performance is carried out based on an experiment of ducted rotor at Osaka University. A hovering rotor on a background cartesian and a cylindrical grid are simulated and compared reasonably well. The predicted ducted rotor performance is shown a good agreement with the experimental data.","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: AA1730011005","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":"株式会社菱友システムズ"},{"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":"Ryoyu Systems Co., Ltd."},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"菅原, 瑛明"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"田辺, 安忠"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sugawara, Hideaki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tanabe, Yasutada","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":"AA1730011005.pdf","filesize":[{"value":"1.2 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"AA1730011005.pdf","url":"https://jaxa.repo.nii.ac.jp/record/3239/files/AA1730011005.pdf"},"version_id":"79321b85-2d57-441d-9ba7-ef7b9cc714dc"}]},"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":"ダクテッド・ロータ解析に向けた回転翼用CFD ツールの開発","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"ダクテッド・ロータ解析に向けた回転翼用CFD ツールの開発"}]},"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":"3239","relation_version_is_last":true,"title":["ダクテッド・ロータ解析に向けた回転翼用CFD ツールの開発"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T09:06:32.055045+00:00"}