{"created":"2023-06-20T14:36:13.679886+00:00","id":2540,"links":{},"metadata":{"_buckets":{"deposit":"6e2f99c8-e465-4e88-ae84-e7e41ca78e51"},"_deposit":{"created_by":1,"id":"2540","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"2540"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00002540","sets":["1887:1893","9:1090:1186:1195"]},"author_link":["7108","7107","7106","7105"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Aerodynamic Analysis Validation of TRANAIR++ applied to NEXST-1 configuration"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2012-03-30","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"47","bibliographicPageStart":"1","bibliographicVolumeNumber":"JAXA-RM-11-015","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構研究開発資料"},{"bibliographic_title":"JAXA Research and Development Memorandum","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"JAXA航空プログラムグループ超音速機チームでは，超音速研究機の空力設計及び空力特性評価に供することを目的として，2008年に市販のフルポテンシャル空力解析ツールTRANAIR++を導入した．本報告では，その解析精度と解析効率の確認を目的として，JAXAがCFD逆問題設計技術，及び空力抵抗低減設計コンセプトを実証するために設計・製作し，2005年に飛行試験を実施した小型超音速実験機NEXST-1形状に適用した結果について報告する．TRANAIR++により解析された亜音速・遷音速・超音速領域におけるNEXST-1形状の空力特性は，小型超音速実験機空力データベース(NEXST-DB)で公開されているCFD解析結果と比較を行い，その解析精度を検証した．","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"JAXA supersonic transport team has introduced the commercially available full potential aerodynamic solver TRANAIR++ since 2008 for aerodynamic design and aerodynamic characteristics evaluation of a supersonic research airplane. In order to check the accuracy and efficiency of the TRANAIR++, it is applied to the scaled supersonic experimental airplane NEXST-1 which was designed, built, and used for flight test in 2005 to demonstrate JAXA's CFDbased inverse design technology and some supersonic low-drag design concepts. The aerodynamic characteristics from subsonic to supersonic speed regime of the NEXST-1 evaluated by the TRANAIR++ are compared to the CFD analysis results which are open to the public through the database named NEXST-DB.","subitem_description_type":"Other"}]},"item_3_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_3_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_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0065213000","subitem_description_type":"Other"}]},"item_3_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: JAXA-RM-11-015","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-1121","subitem_source_identifier_type":"ISSN"}]},"item_3_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AA11983593","subitem_source_identifier_type":"NCID"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"菱友システムズエンジニアリングソリューション事業部"},{"subitem_text_value":"宇宙航空研究開発機構航空プログラムグループ超音速機チーム (JAXA)"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Engineering Solutions Division, Ryoyu Systems"},{"subitem_text_language":"en","subitem_text_value":"Supersonic Transport Team, Aviation Program Group, Japan Aerospace Exploration Agency (JAXA)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"牧本, 卓也"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"牧野, 好和"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Makimoto, Takuya","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Makino, Yoshikazu","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":"2020-01-15"}],"displaytype":"detail","filename":"65213000.pdf","filesize":[{"value":"5.1 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"65213000.pdf","url":"https://jaxa.repo.nii.ac.jp/record/2540/files/65213000.pdf"},"version_id":"564edecd-c5bf-4dc2-b0f9-3243a8c8c7fd"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"aerodynamic analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"full potential equation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic transport","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":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"NEXST-1形状を対象としたTRANAIR++空力解析検証","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"NEXST-1形状を対象としたTRANAIR++空力解析検証"}]},"item_type_id":"3","owner":"1","path":["1195","1893"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"2540","relation_version_is_last":true,"title":["NEXST-1形状を対象としたTRANAIR++空力解析検証"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T09:20:29.214805+00:00"}