{"created":"2023-06-20T15:11:43.528826+00:00","id":41440,"links":{},"metadata":{"_buckets":{"deposit":"58b360d2-b6c8-4a97-8018-ad9ee09ad483"},"_deposit":{"created_by":1,"id":"41440","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"41440"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00041440","sets":["1887:1893","1896:1898:1913:1915"]},"author_link":["490037","490039","490038","490040"],"item_3_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"将来型有翼宇宙輸送システムのためのCFDの研究活動"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2000-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"186","bibliographicPageStart":"183","bibliographicVolumeNumber":"49T","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 17-19 Jan. 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 17-19 Jan. 2000 Tokyo Japan","subitem_description_type":"Other"}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"NAL(航空宇宙技術研究所)においては、NASDA(宇宙開発事業団)との共同研究として、大気圏宇宙輸送機の空気力学研究のため数値シミュレーションを行ってきた。計算機ハードウェアシステムの進歩に伴ってCFD(計算流体力学)技術はその応用範囲を広げた。そして今やCFDは強力な空力設計ツールとして発展し、打上げから再突入フェーズまでの宇宙輸送機の飛行範囲を取り扱えるようになった。ここではNALにおける数値シミュレーションの最近の進歩を紹介した。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Numerical simulation for aerodynamic study of atmospheric space transport vehicles has been conducted at NAL (National Aerospace Laboratory) as the cooperative research work with NASDA (National Space Development Agency). CFD (Computational Fluid Dynamics) technology enlarges its application area with the progress of the computer hardware systems and now CFD has been developed as the strong aerodynamic design tool which covers flight range of space transport vehicle from the launching to the re-entry phase. Here, recent progress of numerical simulations at NAL are introduced.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0028638024","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-49T","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"},{"subitem_text_value":"航空宇宙技術研究所"}]},"item_3_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"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"山本, 行光"}],"nameIdentifiers":[{"nameIdentifier":"490037","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"黒滝, 卓司"}],"nameIdentifiers":[{"nameIdentifier":"490038","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Yamamoto, Yukimitsu","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"490039","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Kurotaki, Takuji","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"490040","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":"nalsp0049024.pdf","filesize":[{"value":"3.9 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0049024.pdf","url":"https://jaxa.repo.nii.ac.jp/record/41440/files/nalsp0049024.pdf"},"version_id":"a60a3582-b980-45d8-9ec6-3a9f7ecc6227"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"CFD","subitem_subject_scheme":"Other"},{"subitem_subject":"計算流体力学","subitem_subject_scheme":"Other"},{"subitem_subject":"有翼宇宙輸送システム","subitem_subject_scheme":"Other"},{"subitem_subject":"HOPE-X形態","subitem_subject_scheme":"Other"},{"subitem_subject":"パラメトリックデザイン","subitem_subject_scheme":"Other"},{"subitem_subject":"航空機形態設計","subitem_subject_scheme":"Other"},{"subitem_subject":"表面格子","subitem_subject_scheme":"Other"},{"subitem_subject":"高温度環境","subitem_subject_scheme":"Other"},{"subitem_subject":"再突入飛行","subitem_subject_scheme":"Other"},{"subitem_subject":"数値シミュレーション","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":"winged space transport system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"HOPE X configuration","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"parametric design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aeroplane configuration design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"surface grid","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"high temperature environment","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"reentry flight","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical simulation","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":"CFD activity for future winged space transport system","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"CFD activity for future winged space transport system","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":"41440","relation_version_is_last":true,"title":["CFD activity for future winged space transport system"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:00:12.051201+00:00"}