{"created":"2023-06-20T15:08:03.980496+00:00","id":37454,"links":{},"metadata":{"_buckets":{"deposit":"8a0c8f28-94a9-425c-82e9-dae63b1c61a6"},"_deposit":{"created_by":1,"id":"37454","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37454"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037454","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["480865","480866","480863","480864"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"CFD analysis of transonic, supersonic, and hypersonic flowfields around re-usable rocket and spaceplane"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1999-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"142","bibliographicPageStart":"135","bibliographicVolumeNumber":"44","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 16-18 Jun. 1999 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 16-18 Jun. 1999 Tokyo Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"将来のSSTO(単段軌道直行式)宇宙往還機の空力特性を評価するために、遷音速から極超音速流について、2種類の再利用ロケットに対しCFD(数値流体力学)解析を適用し、スペースプレーンに対して、実在気体効果を入れた極超音速流計算を行った。スペースプレーンの解析については、米国のAEDC(アーノルド・エンジニアリングディベロップメントセンター)の極超風洞試験結果との比較が行われた。今回のCFD解析においては、CATIAを用いた形状定義や格子生成法も導入された。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"In order to evaluate aerodynamic characteristics of future SSTO (Single Stage To Orbit) space transport vehicles, CFD (Computational Fluid Dynamics) analysis was conducted from transonic to hypersonic speed for two reusable rockets and hypersonic flow computations including real gas effects, were made for a space plane. Comparisons with AEDC (Arnold Engineering Development Center) hypersonic wind tunnel experiment were made for the latter space plane analysis. In the present CFD works, geometry definition by using CATIA and grid generation methods are also introduced.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001961021","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-44","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":"大興電子通信"}]},"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":"Daiko Denshi Tsushin Ltd"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"山本, 行光"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"伊藤, 良三"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamamoto, Yukimitsu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ito, Ryozo","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":"nalsp0044021.pdf","filesize":[{"value":"3.6 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0044021.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37454/files/nalsp0044021.pdf"},"version_id":"64d69bbb-827d-4f6e-b0c6-3a367166f75c"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"CFD","subitem_subject_scheme":"Other"},{"subitem_subject":"数値流体力学","subitem_subject_scheme":"Other"},{"subitem_subject":"再使用ロケット","subitem_subject_scheme":"Other"},{"subitem_subject":"スペースプレーン","subitem_subject_scheme":"Other"},{"subitem_subject":"SSTO","subitem_subject_scheme":"Other"},{"subitem_subject":"単段軌道直行式","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙往還機","subitem_subject_scheme":"Other"},{"subitem_subject":"遷音速","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速","subitem_subject_scheme":"Other"},{"subitem_subject":"リフティングボディー","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":"reusable rocket","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"spaceplane","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"SSTO","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"single stage to orbit","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"space transport vehicles","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transonic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"lifting body","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":"再使用ロケットスペース・プレーンの遷・超・極超音速流CFD解析","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"再使用ロケットスペース・プレーンの遷・超・極超音速流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":"37454","relation_version_is_last":true,"title":["再使用ロケットスペース・プレーンの遷・超・極超音速流CFD解析"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:18:30.286176+00:00"}