{"created":"2023-06-20T15:08:04.240718+00:00","id":37458,"links":{},"metadata":{"_buckets":{"deposit":"12bd3e86-7ad6-4c28-843c-47b08cd54d8b"},"_deposit":{"created_by":1,"id":"37458","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37458"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037458","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["480881","480882","480883","480884"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"CFD aerodynamic design analysis of improved HOPE-X configurations from low to hypersonic speeds"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1999-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"173","bibliographicPageStart":"167","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":"重量軽減や空力性能の向上のため、その形状をテイップフィンタイプから胴上双垂尾形態に変えたHOPE-X(宇宙往還技術試験機)の新しい空力学的形状設計のため、CFD(数値流体力学)を主に使い、短期間でナビエ・ストークスの解析を低速(マッハ数0.4)から極超音速領域(マッハ数26)にわたり実施した。新しいHOPE-Xの計10の形状候補に対して全部で250の計算を行い、新しい基本モデルを決めるために、空力特性に与える形状の効果を詳細に検討した。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"For the new aerodynamic configuration design of HOPE-X (H-2 Orbiting Plane Experimental), whose geometry is modified from tip fin type to two vertical tail fin type in order to reduce the weight and get high performance, CFD (Computational Fluid Dynamics) has been mainly used and Navier-Stokes calculations performed in a short term from low (Mach number 0.4) to hypersonic speed (Mach number 26). Total, 250 computations were conducted for ten candidate configurations of new HOPE-X and the geometry effects on aerodynamic characteristics were investigated in detail to determine new basic model.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001961025","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":"nalsp0044025.pdf","filesize":[{"value":"2.1 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0044025.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37458/files/nalsp0044025.pdf"},"version_id":"f7a0e132-b644-41cf-bb17-e8c52d058749"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"CFD解析","subitem_subject_scheme":"Other"},{"subitem_subject":"数値流体力学","subitem_subject_scheme":"Other"},{"subitem_subject":"空力設計","subitem_subject_scheme":"Other"},{"subitem_subject":"再突入飛行","subitem_subject_scheme":"Other"},{"subitem_subject":"ナビエ・ストークス計算","subitem_subject_scheme":"Other"},{"subitem_subject":"空力特性","subitem_subject_scheme":"Other"},{"subitem_subject":"HOPE X","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙往還技術試験機","subitem_subject_scheme":"Other"},{"subitem_subject":"胴上双垂尾形態","subitem_subject_scheme":"Other"},{"subitem_subject":"低速-極超音速領域","subitem_subject_scheme":"Other"},{"subitem_subject":"形状効果","subitem_subject_scheme":"Other"},{"subitem_subject":"新基本モデル","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":"aerodynamic design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"reentry flight","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Navier Stokes calculation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"HOPE X","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"H 2 Orbiting Plane Experimental","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"two vertical tail fin","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"low hypersonic speed","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"geometry effect","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"new basic model","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":"HOPE-X改善形状まわりのCFD空力設計解析","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"HOPE-X改善形状まわりのCFD空力設計解析"}]},"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":"37458","relation_version_is_last":true,"title":["HOPE-X改善形状まわりのCFD空力設計解析"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:18:26.350054+00:00"}