{"created":"2023-06-20T14:37:57.202187+00:00","id":4408,"links":{},"metadata":{"_buckets":{"deposit":"07ce2437-c3ac-4f09-b0a8-0b35af6ac41b"},"_deposit":{"created_by":1,"id":"4408","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"4408"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00004408","sets":["1398:1530:1538","1543:1874:1882","1887:1891","9:789:906:907"]},"author_link":["19808","19810","19806","19805","19804","19809","19807","19811"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Influence of Maximum Camber Position on the Aerodynamic Chacteristics of Contact Circular Arc Airfoil at Low Reynolds Number"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2012-03-30","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"213","bibliographicPageStart":"209","bibliographicVolumeNumber":"JAXA-SP-11-015","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料: 第43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2011論文集"},{"bibliographic_title":"JAXA Special Publication: Proceedings of 43rd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2011","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43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2011 (2011年7月7日-8日. 早稲田大学国際会議場) 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":"43rd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2011 (July 7-8,  2011. Waseda University, International Conference Center), Tokyo Japan","subitem_description_type":"Other"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A contact circular arc airfoil was shaped from two circular arc airfoils with different radius of curvature. We carried out two-dimensional numerical simlulation in order to clarify influences of maximum camber position on aerodymamc characteristics of the airfoil at Reymolds number of 40,000. The move of the maximum camber position brought about a change of flow field with vortices structure around the airfoll, and changes of the aerodynamic characteristics of the airfoil were observed with this flow field changing Maximum lift to drag ratio also show a maximum value when the maximum camber position has a near by 30% chord length of the airfoil.","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: AA0065207036","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-11-015","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"}]},"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":"東北大学"},{"subitem_text_value":"日本大学理工学部"},{"subitem_text_value":"日本大学理工学部"},{"subitem_text_value":"日本大学理工学部"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Tohoku University"},{"subitem_text_language":"en","subitem_text_value":"College of Science and Technology, Nihon University"},{"subitem_text_language":"en","subitem_text_value":"College of Science and Technology, Nihon University"},{"subitem_text_language":"en","subitem_text_value":"College of Science and Technology, Nihon University"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"伊丹, 達生"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"大竹, 智久"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"村松, 旦典"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"本橋, 龍郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Itami, Tatsuo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Otake, Tomohisa","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Muramatsu, Akinori","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Motohashi, Tatsuo","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":"65207036.pdf","filesize":[{"value":"552.8 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"65207036.pdf","url":"https://jaxa.repo.nii.ac.jp/record/4408/files/65207036.pdf"},"version_id":"062e40a3-51bf-4040-88f8-90e6b02074d0"}]},"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":"低Re数での連結円弧翼型の空力特性における最大キャンバー位置の影響","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"低Re数での連結円弧翼型の空力特性における最大キャンバー位置の影響"}]},"item_type_id":"5","owner":"1","path":["907","1538","1882","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"4408","relation_version_is_last":true,"title":["低Re数での連結円弧翼型の空力特性における最大キャンバー位置の影響"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T08:40:05.761886+00:00"}