{"created":"2023-06-19T09:51:09.563434+00:00","id":8198,"links":{},"metadata":{"_buckets":{"deposit":"e9452215-d127-4536-90e8-1650db3e6daf"},"_deposit":{"created_by":3,"id":"8198","owners":[3],"pid":{"revision_id":0,"type":"depid","value":"8198"},"status":"published"},"_oai":{"id":"oai:fukuyama-u.repo.nii.ac.jp:00008198","sets":["502:505:675:712"]},"author_link":["44047","44048","44045","44049","44044","44042","44046","44043","44050"],"item_1_biblio_info_14":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2004-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"276","bibliographicPageStart":"273","bibliographicVolumeNumber":"28","bibliographic_titles":[{"bibliographic_title":"福山大学工学部紀要"}]}]},"item_1_creator_6":{"attribute_name":"著者名(日)","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"真鍋, 圭司"}],"nameIdentifiers":[{"nameIdentifier":"44042","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"中村, 弘明"}],"nameIdentifiers":[{"nameIdentifier":"44043","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"西尾, 正富"}],"nameIdentifiers":[{"nameIdentifier":"44044","nameIdentifierScheme":"WEKO"}]}]},"item_1_description_1":{"attribute_name":"ページ属性","attribute_value_mlt":[{"subitem_description":"P(論文)","subitem_description_type":"Other"}]},"item_1_description_12":{"attribute_name":"抄録(英)","attribute_value_mlt":[{"subitem_description":"Hypersonic flow field around the re-entry capsule is analyzed by Monte Carlo Simulation. The formulation for analyzing rarefied gas flow based on statistical theory is described. This method uses random number, and dynamics of molecular is simulated considering collision and reflection. The two dimensional capsule model is made by using Finite Element mesh, and hypersonic flow field of Mach 10 is calculated. The density and velocity field around the capsule model are calculated, and the shock wave is obtained as the density concentrated filed. This Monte Carlo method is considered to be effective for simulating hypersonic flow field, although some problems are remained.","subitem_description_type":"Other"}]},"item_1_full_name_7":{"attribute_name":"著者名よみ","attribute_value_mlt":[{"nameIdentifiers":[{"nameIdentifier":"44045","nameIdentifierScheme":"WEKO"}],"names":[{"name":"マナベ, ケイジ"}]},{"nameIdentifiers":[{"nameIdentifier":"44046","nameIdentifierScheme":"WEKO"}],"names":[{"name":"ナカムラ, ヒロアキ"}]},{"nameIdentifiers":[{"nameIdentifier":"44047","nameIdentifierScheme":"WEKO"}],"names":[{"name":"ニシオ, マサトミ"}]}]},"item_1_full_name_8":{"attribute_name":"著者名(英)","attribute_value_mlt":[{"nameIdentifiers":[{"nameIdentifier":"44048","nameIdentifierScheme":"WEKO"}],"names":[{"name":"MANABE, Keiji","nameLang":"en"}]},{"nameIdentifiers":[{"nameIdentifier":"44049","nameIdentifierScheme":"WEKO"}],"names":[{"name":"NAKAMURA, Hiroaki","nameLang":"en"}]},{"nameIdentifiers":[{"nameIdentifier":"44050","nameIdentifierScheme":"WEKO"}],"names":[{"name":"NISHIO, Masatomi","nameLang":"en"}]}]},"item_1_source_id_13":{"attribute_name":"雑誌書誌ID","attribute_value_mlt":[{"subitem_source_identifier":"AN00217655","subitem_source_identifier_type":"NCID"}]},"item_1_text_10":{"attribute_name":"著者所属(英)","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Department of Mechanical System Engineering, Faculty of Engineering, Fukuyama University"},{"subitem_text_language":"en","subitem_text_value":"Fukuyama University"},{"subitem_text_language":"en","subitem_text_value":"Department of Mechanical System Engineering, Faculty of Engineering, Fukuyama University"}]},"item_1_text_9":{"attribute_name":"著者所属(日)","attribute_value_mlt":[{"subitem_text_value":"福山大学工学部機械システム工学科"},{"subitem_text_value":"福山大学大学院設計生産工学専攻"},{"subitem_text_value":"福山大学工学部機械システム工学科"}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2004-12-01"}],"displaytype":"detail","filename":"KJ00005781594.pdf","filesize":[{"value":"327.9 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"url":"https://fukuyama-u.repo.nii.ac.jp/record/8198/files/KJ00005781594.pdf"},"version_id":"4e7f4dbe-c8b0-4add-8541-b4ca3f8732b9"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"モンテカルロシミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"極超音速流","subitem_subject_scheme":"Other"},{"subitem_subject":"衝撃波","subitem_subject_scheme":"Other"},{"subitem_subject":"Monte Carlo Simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Hypersonic flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Shock wave","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":"departmental bulletin paper","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"モンテカルロ法による極超音速流の解析","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"モンテカルロ法による極超音速流の解析"},{"subitem_title":"Monte Carlo Simulation of Hypersonic Flow","subitem_title_language":"en"}]},"item_type_id":"1","owner":"3","path":["712"],"pubdate":{"attribute_name":"公開日","attribute_value":"2004-12-01"},"publish_date":"2004-12-01","publish_status":"0","recid":"8198","relation_version_is_last":true,"title":["モンテカルロ法による極超音速流の解析"],"weko_creator_id":"3","weko_shared_id":-1},"updated":"2023-06-19T10:28:05.594093+00:00"}