{"created":"2023-06-20T14:46:46.343676+00:00","id":14351,"links":{},"metadata":{"_buckets":{"deposit":"9b11556e-0f18-47e6-9bb6-10622935a093"},"_deposit":{"created_by":1,"id":"14351","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"14351"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00014351","sets":["1543:1656:1662","1887:1891"]},"author_link":["131373","131375","131377","131374","131372","131376","131369","131378","131379","131380","131370","131371"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Low Reynolds-Number Airfoil Testing in a Mars Wind Tunnel"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2011-08","bibliographicIssueDateType":"Issued"},"bibliographic_titles":[{"bibliographic_title":"宇宙航行の力学シンポジウム: 平成22年度"},{"bibliographic_title":"Symposium on Flight Mechanics and Astrodynamics: 2010","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":"宇宙航行の力学シンポジウム 平成22年度 (2010年12月16-17日. 宇宙航空研究開発機構宇宙科学研究所), 相模原市, 神奈川県","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":"Symposium on Flight Mechanics and Astrodynamics,  2010 (December 16-17, 2010. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)(ISAS)), Sagamihara, Kanagawa Japan","subitem_description_type":"Other"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The aerodynamic charactetistics of a 5% flat plate and an NACA0012-34 airfoil in low Reynolds number (Re=0.43x10(exp 4)-4.1x10(exp 4)) and high subsonic flow (M=0.1-0.65) were investigated in the Mars Wind Tunnel (MWT) at Tohoku University. A two-component balance system and Pressure-Sensitive Paint (PSP) technique have been developed to measure the lift and drag forces and pressure profiles on the models. For the flat plate, Mach number effect does not have much effect on its aerodynamic performance while Reynolds number affects the lift slope and the drag characteristics. On the contrary, for the NACA00121-34 airfoil, both Reynolds and Mach number effects become more prominent. The lift curve is highly nonlinear and the drag polar is affected by behaviors of a laminar separation bubble. It was suggested that Mach number has efects to delay transition of the shear layer from laminar to turbulent state.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0065106032","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宇宙科学研究所"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"東北大学"},{"subitem_text_value":"東北大学"},{"subitem_text_value":"東北大学"},{"subitem_text_value":"東北大学"},{"subitem_text_value":"東北大学"},{"subitem_text_value":"東北大学"}]},"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":"Tohoku University"},{"subitem_text_language":"en","subitem_text_value":"Tohoku University"},{"subitem_text_language":"en","subitem_text_value":"Tohoku University"},{"subitem_text_language":"en","subitem_text_value":"Tohoku University"},{"subitem_text_language":"en","subitem_text_value":"Tohoku University"}]},"item_access_right":{"attribute_name":"アクセス権","attribute_value_mlt":[{"subitem_access_right":"metadata only access","subitem_access_right_uri":"http://purl.org/coar/access_right/c_14cb"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"浅井, 圭介"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"永井, 大樹"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"沼田, 大樹"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"安養寺, 正之"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"伊田, 真悟"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"野瀬, 慶"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Asai, Keisuke","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nagai, Hiroki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Numata, Daijyu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Anyoji, Masayuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ida, Shingo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nose, Kei","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Mars alrplane","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Wind tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Low Reynolds number","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Airfoil testing","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"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":"火星大気風洞における低レイノルズ数翼型実験","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"火星大気風洞における低レイノルズ数翼型実験"}]},"item_type_id":"5","owner":"1","path":["1662","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"14351","relation_version_is_last":true,"title":["火星大気風洞における低レイノルズ数翼型実験"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T05:35:48.132657+00:00"}