{"created":"2023-06-20T14:47:02.300147+00:00","id":14656,"links":{},"metadata":{"_buckets":{"deposit":"eaaf7c84-b5e7-4d22-a643-f819dcbf9a97"},"_deposit":{"created_by":1,"id":"14656","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"14656"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00014656","sets":["1543:1656:1669","1887:1891"]},"author_link":["133914","133918","133916","133919","133917","133915"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Experimental study on aerodynamic characteristics of rotary wings for a miniature Mars exploration rotorcraft at ultra-low Reynolds numbers"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2004-05","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"42","bibliographicPageStart":"39","bibliographic_titles":[{"bibliographic_title":"宇宙航行の力学シンポジウム　平成15年度"},{"bibliographic_title":"Symposium on Flight Mechanics and Astrodynamics 2003","bibliographic_titleLang":"en"}]}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Understanding on an efficient small-scale hovering rotor is required to make a miniature rotorcraft probe to explore the Martian surface. For this purpose, an experimental measurement of the aerodynamic characteristics of a small-scale rotor at ultra-low Reynolds numbers (Re = 2,000, 4,000, 8,000) was performed. The experimental results show that the airflow around the rotor is subject to the leading-edge vortex (LEV) and that the Blade Element Momentum Theory (BEMT) is valid at moderate collective pitch angles and that the capability of the rotor required for the rotorcraft probe is within reach.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0047120011","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本部"}]},"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/ISAS)"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"東京大学 大学院"},{"subitem_text_value":"宇宙航空研究開発機構 宇宙科学研究本部"},{"subitem_text_value":"宇宙航空研究開発機構 宇宙科学研究本部"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"University of Tokyo Graduate School"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Space and Astronautical Science"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Space and Astronautical Science"}]},"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":"都築, 範明"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"佐藤, 俊逸"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"安部, 隆士"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tsuzuki, Noriaki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sato, Shunichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Abe, Takashi","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"空力特性","subitem_subject_scheme":"Other"},{"subitem_subject":"超低レイノルズ数","subitem_subject_scheme":"Other"},{"subitem_subject":"回転翼","subitem_subject_scheme":"Other"},{"subitem_subject":"火星探査機","subitem_subject_scheme":"Other"},{"subitem_subject":"前縁剥離渦","subitem_subject_scheme":"Other"},{"subitem_subject":"ピッチ角","subitem_subject_scheme":"Other"},{"subitem_subject":"Knudsen数","subitem_subject_scheme":"Other"},{"subitem_subject":"翼素運動量理論","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"ultra-low Reynolds number","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"rotary wing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Mars exploration rotorcraft","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"leading edge vortex","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"pitch angle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Knudsen number","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"blade element momentum theory","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":"火星探査機用回転翼の超低レイノルズ数空力特性","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"火星探査機用回転翼の超低レイノルズ数空力特性"}]},"item_type_id":"5","owner":"1","path":["1669","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"14656","relation_version_is_last":true,"title":["火星探査機用回転翼の超低レイノルズ数空力特性"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T05:31:22.635933+00:00"}