{"created":"2023-06-20T14:37:43.204885+00:00","id":4137,"links":{},"metadata":{"_buckets":{"deposit":"09ddfbe0-4554-4128-93c1-8c27d17e8a23"},"_deposit":{"created_by":1,"id":"4137","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"4137"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00004137","sets":["1887:1891","9:789:868:887"]},"author_link":["17842","17844","17846","17847","17845","17839","17843","17835","17836","17837","17840","17838","17834","17841"],"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2013-11-30","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"351","bibliographicPageStart":"343","bibliographicVolumeNumber":"JAXA-SP-13-001E","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料"},{"bibliographic_title":"JAXA Special Publication","bibliographic_titleLang":"en"}]}]},"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":"5th Symposium on Integrating CFD and Experiments in Aerodynamics (October 3-5, 2012, Chofu Aerospace Center, Japan Aerospace Exploration Agency (JAXA)), Chofu, Tokyo, Japan","subitem_description_type":"Other"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"In this research, we propose a delta wing with an arc camber to explore the Mars in flight at low Reynolds number of 1.0×10(exp 4) order. The research focuses on L/D of a cambered delta wing to get a wide cross range for the Mars exploration by computational analysis and aerodynamic force measurements using a newly developed three-component force balance. The CFD results show that L/D of the delta wing with an arc camber is much better than the no-camber delta wing at a low angle of attack. Especially, the wing with the camber rate of 5% gives the best performance. The validation results by the EFD approach supports the CFD analysis.","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: AA0062070029","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-13-001E","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":"鳥取大学"},{"subitem_text_value":"鳥取大学"},{"subitem_text_value":"鳥取大学"},{"subitem_text_value":"鳥取大学大学院工学研究科機械宇宙工学専攻"},{"subitem_text_value":"鳥取大学大学院工学研究科機械宇宙工学専攻"},{"subitem_text_value":"東北大学流体科学研究所"},{"subitem_text_value":"鳥取大学大学院工学研究科機械宇宙工学専攻"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Tottori University"},{"subitem_text_language":"en","subitem_text_value":"Tottori University"},{"subitem_text_language":"en","subitem_text_value":"Tottori University"},{"subitem_text_language":"en","subitem_text_value":"Department of Mechanical and Aerospace Engineering, Graduate School of Engineering, Tottori University"},{"subitem_text_language":"en","subitem_text_value":"Department of Mechanical and Aerospace Engineering, Graduate School of Engineering, Tottori University"},{"subitem_text_language":"en","subitem_text_value":"Institute of Fluid Science, Tohoku University"},{"subitem_text_language":"en","subitem_text_value":"Department of Mechanical and Aerospace Engineering, Graduate School of Engineering, Tottori University"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"鵜ノ口, 孝雄"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"青山, 省吾"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"末村, 紘志"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"山田, 剛治"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"松野, 隆"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"大林, 茂"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"川添, 博光"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Unoguchi, Takao","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Aoyama, Shogo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Suemura, Hiroshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamada, Gouji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Matsuno, Takashi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Obayashi, Shigeru","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kawazoe, Hiromitsu","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":"62070029.pdf","filesize":[{"value":"440.2 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"62070029.pdf","url":"https://jaxa.repo.nii.ac.jp/record/4137/files/62070029.pdf"},"version_id":"e97cc8d7-f3c5-41e1-913c-b4e3eccd0363"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Delta wing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Arc camber","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Aerodynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Mars exploration","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Three-component force balance","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"eng"}]},"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":"Aerodynamic Characteristics of a Delta Wing with Arc Camber for Mars Exploration","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Aerodynamic Characteristics of a Delta Wing with Arc Camber for Mars Exploration","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["887","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"4137","relation_version_is_last":true,"title":["Aerodynamic Characteristics of a Delta Wing with Arc Camber for Mars Exploration"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T08:46:35.108025+00:00"}