{"created":"2023-06-20T14:54:12.124366+00:00","id":22482,"links":{},"metadata":{"_buckets":{"deposit":"5c603f84-ab36-437c-8a24-e5c9a57c68fb"},"_deposit":{"created_by":1,"id":"22482","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"22482"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00022482","sets":["1887:1888"]},"author_link":["210849","210847","210842","210848","210844","210845","210846","210843"],"item_7_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2014-06","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"6","bibliographicPageEnd":"1306","bibliographicPageStart":"1294","bibliographicVolumeNumber":"52","bibliographic_titles":[{},{"bibliographic_title":"AIAA Journal","bibliographic_titleLang":"en"}]}]},"item_7_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"This paper describes an effective method to create a new ideal pressure distribution for designing a three-dimensional natural-laminar-flow wing at high-Reynolds-number conditions to reduce friction drag of a large-size supersonic transport with 300 passengers. This ideal pressure distribution consists of a useful functional form with parameters that are adjusted to be widely applicable to general wing planforms. Furthermore, this research proposes an improvement to the design flow of a conventional computational-fluid-dynamics-based inverse design method developed previously by the Japan Aerospace Exploration Agency for a natural-laminarflow wing design. An idealized pressure distribution and its validity to achieve approximately 35% laminar flow region of the wing surface on a cranked arrow type planform are presented at the condition ofMach 2.0 and high Reynolds number of approximately 126 million based on mean aerodynamic chord. A representative crosssectional shape of the designed wing is introduced as an example, and it is shown that a distinguishing feature is characterized by a smaller curvature near the attachment line. A further ideal pressure distribution for an Ogeetype planform with swept angle varied continuously in spanwise direction is then created as a test case for more complicated planforms.","subitem_description_type":"Other"}]},"item_7_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: PA1420032000","subitem_description_type":"Other"}]},"item_7_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"American Institute of Aeronautics and Astronautics (AIAA)"}]},"item_7_relation_25":{"attribute_name":"DOI","attribute_value_mlt":[{"subitem_relation_name":[{"subitem_relation_name_text":"info:doi/10.2514/1.J052555"}],"subitem_relation_type":"isVersionOf","subitem_relation_type_id":{"subitem_relation_type_id_text":"https://doi.org/10.2514/1.J052555","subitem_relation_type_select":"DOI"}}]},"item_7_rights_28":{"attribute_name":"権利","attribute_value_mlt":[{"subitem_rights":"(C) 2014 by the American Institute of Aeronautics and Astronautics, Inc."}]},"item_7_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0001-1452","subitem_source_identifier_type":"ISSN"}]},"item_7_source_id_22":{"attribute_name":"ISSNONLINE","attribute_value_mlt":[{"subitem_source_identifier":"1533-385X","subitem_source_identifier_type":"ISSN"}]},"item_7_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AA00502751","subitem_source_identifier_type":"NCID"}]},"item_7_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"東京ビジネスサービス株式会社"},{"subitem_text_value":"宇宙航空研究開発機構航空本部(JAXA)"},{"subitem_text_value":"富山大学"},{"subitem_text_value":"三向ソフトウェア開発株式会社"}]},"item_7_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Tokyo Business Service Co. Ltd.,"},{"subitem_text_language":"en","subitem_text_value":"Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"University of Toyama"},{"subitem_text_language":"en","subitem_text_value":"Sankosoft Co. Ltd."}]},"item_7_version_type_30":{"attribute_name":"著者版フラグ","attribute_value_mlt":[{"subitem_version_resource":"http://purl.org/coar/version/c_ab4af688f83e57aa","subitem_version_type":"AM"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"上田, 良稲"}],"nameIdentifiers":[{"nameIdentifier":"210842","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"吉田, 憲司"}],"nameIdentifiers":[{"nameIdentifier":"210843","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"松島, 紀佐"}],"nameIdentifiers":[{"nameIdentifier":"210844","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"石川, 敬掲"}],"nameIdentifiers":[{"nameIdentifier":"210845","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Ueda, Yoshine","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"210846","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Yoshida, Kenji","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"210847","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Matsushima, Kisa","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"210848","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Ishikawa, Hiroaki","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"210849","nameIdentifierScheme":"WEKO"}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2020-01-22"}],"displaytype":"detail","filename":"PA1420032.pdf","filesize":[{"value":"7.0 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"PA1420032.pdf","url":"https://jaxa.repo.nii.ac.jp/record/22482/files/PA1420032.pdf"},"version_id":"2bbd871b-a79a-4d45-9710-aad953271aae"}]},"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":"journal article","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"Supersonic Natural-Laminar-Flow Wing-Design Concept at High-Reynolds-Number Conditions","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Supersonic Natural-Laminar-Flow Wing-Design Concept at High-Reynolds-Number Conditions","subitem_title_language":"en"}]},"item_type_id":"7","owner":"1","path":["1888"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"22482","relation_version_is_last":true,"title":["Supersonic Natural-Laminar-Flow Wing-Design Concept at High-Reynolds-Number Conditions"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:26:51.106036+00:00"}