{"created":"2023-06-20T14:37:35.120816+00:00","id":4001,"links":{},"metadata":{"_buckets":{"deposit":"40daee6e-4acc-4a27-bb37-b0a4699f9b07"},"_deposit":{"created_by":1,"id":"4001","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"4001"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00004001","sets":["1398:1530:1536","1543:1874:1880","1887:1891","9:789:868:877"]},"author_link":["17079","17076","17077","17081","17080","17078"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Application of a Rotorcraft Aeroelastic Analysis Code to Wind Turbines"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2014-03-31","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"5","bibliographicPageStart":"1","bibliographicVolumeNumber":"JAXA-SP-13-011","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料: 第45回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2013論文集"},{"bibliographic_title":"JAXA Special Publication","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45回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2013 (2013年7月4日-5日. タワーホール船堀), 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":"45th Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2013 (July 4-5, 2013. Tower Hall Funabori), Tokyo, Japan","subitem_description_type":"Other"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Application of the CFD/CSD coupling analysis code rFlow3D which was originally developed for rotorcraft to the wind turbines is described in this paper. NREL Phase VI wind turbine is selected as the test case to validate the accuracy of the analyses. It is found that even with a relative coarse resolution blade grid, the Euler solver can predict the performance of the wind turbine quite satisfactory when the wind turbine is operated in attached flow or deep stall conditions, but the discrepancies in the incipient stall flow region are remarkable where the highest power is generated. With a Navier-Stokes solver, the prediction accuracy is improved with the refinement of the blade grid and the highest power can be predicted satisfactorily.","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: AA0062268001","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-13-011","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_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-113X","subitem_source_identifier_type":"ISSN"}]},"item_5_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AA11984031","subitem_source_identifier_type":"NCID"}]},"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航空本部機体システム研究グループ"},{"subitem_text_value":"宇宙航空研究開発機構航空本部機体システム研究グループ"},{"subitem_text_value":"菱友システムズ"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Aircraft Systems Research Group, Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Aircraft Systems Research Group, Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Ryoyu Systems, Co., Ltd"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"田辺, 安忠"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"杉浦, 正彦"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"菅原, 瑛明"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tanabe, Yasutada","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sugiura, Masahiko","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sugawara, Hideaki","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":"62268001.pdf","filesize":[{"value":"737.6 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"62268001.pdf","url":"https://jaxa.repo.nii.ac.jp/record/4001/files/62268001.pdf"},"version_id":"a0b89403-6fbe-4053-abee-ae427bb22201"}]},"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":"回転翼空力弾性解析コードの風車への適用","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"回転翼空力弾性解析コードの風車への適用"}]},"item_type_id":"5","owner":"1","path":["877","1536","1880","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"4001","relation_version_is_last":true,"title":["回転翼空力弾性解析コードの風車への適用"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T08:50:19.707020+00:00"}