{"created":"2023-06-20T15:07:46.324122+00:00","id":37135,"links":{},"metadata":{"_buckets":{"deposit":"9f1c6512-cf0b-4aa8-a68b-6f2f52dd3f82"},"_deposit":{"created_by":1,"id":"37135","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37135"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037135","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["479073","479075","479077","479072","479074","479076"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"CFD analysis applied to the supersonic research airplane"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1998-02","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"61","bibliographicPageStart":"57","bibliographicVolumeNumber":"37","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_5_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 12-13 Jun. 1997 東京 日本","subitem_description_type":"Other"}]},"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":"National Aerospace Laboratory 12-13 Jun. 1997 Tokyo Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"NAL(航空宇宙技術研究所)はCFD(数値流体力学)による無人小型高速実験機の設計技術確立のための研究開発を進めている。CFD解析は高揚抗比のような高性能を有する次世代HSCT(超音速旅客機)の開発に必要である。本論文はNALの小型高速実験機の設計に適用するCFDコードの概観について述べた。CFDによる空力設計に関する最近の問題点も示した。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"National Aerospace Laboratory (NAL) conducts the research program in which the unmanned supersonic research airplane will be developed to establish the design technology composed by Computational Fluid Dynamics (CFD). CFD analysis is necessary to develop next generation High Speed Commercial Transport (HSCT) which has high performances such as high lift-to-drag ratio. This paper describes the overview of a CFD code applied to the designing of the NAL's supersonic research airplane. It is also presented the recent problems for aerodynamic design with CFD.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001433009","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: NAL SP-37","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory (NAL)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0289-260X","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":"AN10097345","subitem_source_identifier_type":"NCID"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"航空宇宙技術研究所"},{"subitem_text_value":"航空宇宙技術研究所"},{"subitem_text_value":"三向ソフトウェア開発"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"Sanko Software Ltd"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"高木, 亮治"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"岩宮, 敏幸"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"橋本, 桂子"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Takaki, Ryoji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Iwamiya, Toshiyuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hashimoto, Yoshiko","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":"2020-02-10"}],"displaytype":"detail","filename":"nalsp0037009.pdf","filesize":[{"value":"1.1 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0037009.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37135/files/nalsp0037009.pdf"},"version_id":"742063d7-4040-43e9-8455-cbcf368f1f66"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"HSCT","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速旅客機","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD","subitem_subject_scheme":"Other"},{"subitem_subject":"数値流体力学","subitem_subject_scheme":"Other"},{"subitem_subject":"小型高速実験機","subitem_subject_scheme":"Other"},{"subitem_subject":"高揚抗比","subitem_subject_scheme":"Other"},{"subitem_subject":"空力設計","subitem_subject_scheme":"Other"},{"subitem_subject":"CFDコード","subitem_subject_scheme":"Other"},{"subitem_subject":"機体形状","subitem_subject_scheme":"Other"},{"subitem_subject":"性能評価","subitem_subject_scheme":"Other"},{"subitem_subject":"非線形解析","subitem_subject_scheme":"Other"},{"subitem_subject":"逆問題最適設計法","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD設計法","subitem_subject_scheme":"Other"},{"subitem_subject":"マルチブロック構造格子","subitem_subject_scheme":"Other"},{"subitem_subject":"オーバセット格子形成","subitem_subject_scheme":"Other"},{"subitem_subject":"HSCT","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"high speed commercial transport","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computational fluid dynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic research airplane","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"high lift to drag ratio","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD code","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"airframe configuration","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"performance evaluation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"nonlinear analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"inverse optimum design method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD design method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"multiblock structured grid","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"overset grid generation","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":"小型高速実験機におけるCFD解析","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"小型高速実験機におけるCFD解析"}]},"item_type_id":"5","owner":"1","path":["1891","1915"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"37135","relation_version_is_last":true,"title":["小型高速実験機におけるCFD解析"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:25:11.610096+00:00"}