{"created":"2023-06-20T15:08:35.549507+00:00","id":38080,"links":{},"metadata":{"_buckets":{"deposit":"9ff3856a-c843-448d-ab50-ef5df17d0dba"},"_deposit":{"created_by":1,"id":"38080","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"38080"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00038080","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["431606","431602","431604","431607","431603","431605"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Numerical simulation of flowfield around space plane traveling at Mach 10"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2002-01","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"261","bibliographicPageStart":"257","bibliographicVolumeNumber":"53","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所特別資料: 航空宇宙数値シミュレーション技術シンポジウム2001論文集"},{"bibliographic_title":"Special Publication of National Aerospace Laboratory: Proceedings of Aerospace Numerical Simulation Symposium 2001","bibliographic_titleLang":"en"}]}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The numerical simulation around a space plane traveling at the speed of Mach 10 was carried out based on FEM (Finite Element Method). In this FEM formulation, stress (pressure) term is partially integrated in an element by applying the weighted residual method, and the hypersonic flowfield around a space plane model including shock wave can be calculated. three-dimensional simulations were conducted for the case of the angle of attack is 0 and 10 deg. The simulation results are compared with experimental results obtained by the electric discharge method, and good correlation between them was found.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0032819044","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-53","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":"福山大学 工学部　機械工学科"},{"subitem_text_value":"福山大学 大学院工学研究科"},{"subitem_text_value":"福山大学 工学部　機械工学科"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Fukuyama University Department of Mechanical Engineering, Faculty of Engineering"},{"subitem_text_language":"en","subitem_text_value":"Fukuyama University Graduate School of Engineering"},{"subitem_text_language":"en","subitem_text_value":"Fukuyama University Department of Mechanical Engineering, Faculty of Engineering"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"真鍋, 圭司"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"瀬崎, 新士"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"西尾, 正富"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Manabe, Keiji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sezaki, Shinji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nishio, Masatomi","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":"2020-01-24"}],"displaytype":"detail","filename":"nalsp0053043.pdf","filesize":[{"value":"2.4 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0053043.pdf","url":"https://jaxa.repo.nii.ac.jp/record/38080/files/nalsp0053043.pdf"},"version_id":"41c7d53d-d9ce-484f-873d-12e42aca659f"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"数値シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"極超音速流れの分布","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙機","subitem_subject_scheme":"Other"},{"subitem_subject":"マッハ数","subitem_subject_scheme":"Other"},{"subitem_subject":"有限要素法","subitem_subject_scheme":"Other"},{"subitem_subject":"3次元モデル","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"hypersonic flow distribution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerospace plane","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"mach number","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"finite element method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"three dimensional 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":"マッハ10で飛行するスペースプレーン周りの数値シミュレーション","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"マッハ10で飛行するスペースプレーン周りの数値シミュレーション"}]},"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":"38080","relation_version_is_last":true,"title":["マッハ10で飛行するスペースプレーン周りの数値シミュレーション"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:45:29.081892+00:00"}