{"created":"2023-06-19T09:51:07.766346+00:00","id":8156,"links":{},"metadata":{"_buckets":{"deposit":"40de0e87-f214-4225-8487-d9e3757bc5a3"},"_deposit":{"created_by":3,"id":"8156","owners":[3],"pid":{"revision_id":0,"type":"depid","value":"8156"},"status":"published"},"_oai":{"id":"oai:fukuyama-u.repo.nii.ac.jp:00008156","sets":["502:505:675:711"]},"author_link":["43792","43789","43798","43796","43793","43788","43795","43797","43787","43794","43791","43790"],"item_1_biblio_info_14":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2003-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"266","bibliographicPageStart":"259","bibliographicVolumeNumber":"27","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":"中村, 弘明"}],"nameIdentifiers":[{"nameIdentifier":"43787","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"真鍋, 圭司"}],"nameIdentifiers":[{"nameIdentifier":"43788","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"瀬崎, 新士"}],"nameIdentifiers":[{"nameIdentifier":"43789","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"西尾, 正富"}],"nameIdentifiers":[{"nameIdentifier":"43790","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":"A calculation method of flowfield around supersonic/hypersonic vehicles based on the finite element method (FEM) has been presented. In this study, the pressure term of Navier-Stokes equations was included in the flux vector. By performing this scheme, the pressure term could be expressed as a non-differential form in the weighted residual equations. This idea made it possible to calculate compressible flowfields including a shock wave with dramatic less error and better stability with a very small artificial viscosity, compared to conventional FEM calculations. The correctness of the present method was confirmed by comparing shock shapes obtained by the Schlieren system and by comparing streamlines obtained by the electric discharge method. The comparisons were carried out by investigating the flowfield around a Mach 10 MESUR capsule.","subitem_description_type":"Other"}]},"item_1_full_name_7":{"attribute_name":"著者名よみ","attribute_value_mlt":[{"nameIdentifiers":[{"nameIdentifier":"43791","nameIdentifierScheme":"WEKO"}],"names":[{"name":"ナカムラ, ヒロアキ"}]},{"nameIdentifiers":[{"nameIdentifier":"43792","nameIdentifierScheme":"WEKO"}],"names":[{"name":"マナベ, ケイジ"}]},{"nameIdentifiers":[{"nameIdentifier":"43793","nameIdentifierScheme":"WEKO"}],"names":[{"name":"セザキ, シンジ"}]},{"nameIdentifiers":[{"nameIdentifier":"43794","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":"43795","nameIdentifierScheme":"WEKO"}],"names":[{"name":"NAKAMURA, Hiroaki","nameLang":"en"}]},{"nameIdentifiers":[{"nameIdentifier":"43796","nameIdentifierScheme":"WEKO"}],"names":[{"name":"MANABE, Keiji","nameLang":"en"}]},{"nameIdentifiers":[{"nameIdentifier":"43797","nameIdentifierScheme":"WEKO"}],"names":[{"name":"SEZAKI, Shinji","nameLang":"en"}]},{"nameIdentifiers":[{"nameIdentifier":"43798","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 Engineering, Faculty of Engineering, Fukuyama University"},{"subitem_text_language":"en","subitem_text_value":"Department of Mechanical Engineering, Faculty of Engineering, Fukuyama University"},{"subitem_text_language":"en","subitem_text_value":"Department of Mechanical Engineering, Faculty of Engineering, Fukuyama University"},{"subitem_text_language":"en","subitem_text_value":"Department of Mechanical Engineering, Faculty of Engineering, Fukuyama University"}]},"item_1_text_9":{"attribute_name":"著者所属(日)","attribute_value_mlt":[{"subitem_text_value":"福山大学工学部工学部機械工学科"},{"subitem_text_value":"福山大学工学部工学部機械工学科"},{"subitem_text_value":"福山大学工学部工学部機械工学科"},{"subitem_text_value":"福山大学工学部工学部機械工学科"}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2003-12-01"}],"displaytype":"detail","filename":"KJ00005781552.pdf","filesize":[{"value":"983.8 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"url":"https://fukuyama-u.repo.nii.ac.jp/record/8156/files/KJ00005781552.pdf"},"version_id":"8b4ea124-eeaa-412f-b27b-0f607f684d4e"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"超音速流","subitem_subject_scheme":"Other"},{"subitem_subject":"極超音速流","subitem_subject_scheme":"Other"},{"subitem_subject":"再突入カプセル","subitem_subject_scheme":"Other"},{"subitem_subject":"有限要素法","subitem_subject_scheme":"Other"},{"subitem_subject":"Supersonic Flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Hypersonic Flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Re-entry capsule","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Finite Element Method","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":"超音速/極超音速飛翔体周りの流れ場の新しい計算手法","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"超音速/極超音速飛翔体周りの流れ場の新しい計算手法"},{"subitem_title":"A New Calculation Method of Flowfield around Supersonic/Hypersonic Vehicles","subitem_title_language":"en"}]},"item_type_id":"1","owner":"3","path":["711"],"pubdate":{"attribute_name":"公開日","attribute_value":"2003-12-01"},"publish_date":"2003-12-01","publish_status":"0","recid":"8156","relation_version_is_last":true,"title":["超音速/極超音速飛翔体周りの流れ場の新しい計算手法"],"weko_creator_id":"3","weko_shared_id":-1},"updated":"2023-06-19T10:28:53.186626+00:00"}