{"created":"2023-06-20T15:11:41.868983+00:00","id":41404,"links":{},"metadata":{"_buckets":{"deposit":"3b65bd39-9ac1-4ece-8fc2-5a22b8bc5575"},"_deposit":{"created_by":1,"id":"41404","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"41404"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00041404","sets":["1887:1893","1896:1898:1913:1915"]},"author_link":["489889","489888"],"item_3_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"実験機(NEXST)を用いた超音速研究計画"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2000-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"50","bibliographicPageStart":"47","bibliographicVolumeNumber":"48T","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所特別資料"},{"bibliographic_title":"Special Publication of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_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":"航空宇宙技術研究所 27-29 Sept.2000 東京 日本","subitem_description_type":"Other"}]},"item_3_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":"National Aerospace Laboratory 27-29 Sept.2000 Tokyo Japan","subitem_description_type":"Other"}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"1997年にNALは次世代超音速輸送機(SST)に対する研究開発計画を開始した。計画は無推力機および双発ジェット機からなる2種の無人実験機の開発と飛行試験で構成される。NAL開発のCFD(数値流体力学)技術に基づく先端的計算設計システムは実験機によりその有効性を検証する主要な課題である。逆問題法、最適化および多専門分野処理を含むシステム統合が研究され、成果を実験機の空力設計に適用する。無推力機は自然層流翼に適した逆問題法を扱い、また双発ジェット機は全機ならびに重要な構成要素技術に適した空力最適化設計を扱う。無推力機の飛行試験は2002年にオーストラリアで実施する予定である。引き続いて、ジェットエンジン搭載機を計画の最終段階で試験する予定である。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A R&D program for the next generation Supersonic Transport (SST) was initiated in NAL of Japan in 1997. The program comprises development and flight tests of two types of unmanned experimental airplanes consisting of a non-powered and a twinjet ones. The advanced computational design system based on NAL's original CFD (Computational Fluid Dynamics) technology is the main subject to be validated by the experimental airplanes. The inverse method, optimization and system integration including multi-disciplinary treatment are being studied and the fruits are applied to the aerodynamic design of the experimental airplanes. The non-powered airplane deals with inverse method for the natural laminar flow wing and the twinjet powered one will do with aerodynamic optimization design for whole airplane and some important component technologies. The flight tests of the non-powered airplane will be conducted in 2002 in Australia. Successively, the jet-powered airplane will be tested as the final phase of the program.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0028637018","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: NAL SP-48T","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory (NAL)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0289-260X","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":"AN10097345","subitem_source_identifier_type":"NCID"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"航空宇宙技術研究所 次世代超音速プロジェクトセンター"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Next Generation Supersonic Transport Project Center"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"坂田, 公夫"}],"nameIdentifiers":[{"nameIdentifier":"489888","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Sakata, Kimio","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"489889","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":"2020-02-10"}],"displaytype":"detail","filename":"nalsp0048019.pdf","filesize":[{"value":"412.0 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0048019.pdf","url":"https://jaxa.repo.nii.ac.jp/record/41404/files/nalsp0048019.pdf"},"version_id":"d4636a51-377a-4943-b46d-09fe882d880d"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"SST","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速輸送機","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速研究計画","subitem_subject_scheme":"Other"},{"subitem_subject":"無人超音速実験機","subitem_subject_scheme":"Other"},{"subitem_subject":"先端的計算設計システム","subitem_subject_scheme":"Other"},{"subitem_subject":"空力設計","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行試験","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD設計","subitem_subject_scheme":"Other"},{"subitem_subject":"数値流体力学","subitem_subject_scheme":"Other"},{"subitem_subject":"自然層流","subitem_subject_scheme":"Other"},{"subitem_subject":"逆問題法","subitem_subject_scheme":"Other"},{"subitem_subject":"SST","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic transport","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic research program","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"unmanned supersonic experimental airplane","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"advanced computational design system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flight test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computational fluid dynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"natural laminar flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"inverse method","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":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"Supersonic research program with the experimental airplanes: NEXST","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Supersonic research program with the experimental airplanes: NEXST","subitem_title_language":"en"}]},"item_type_id":"3","owner":"1","path":["1893","1915"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"41404","relation_version_is_last":true,"title":["Supersonic research program with the experimental airplanes: NEXST"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:01:03.152639+00:00"}