{"created":"2023-06-19T09:51:11.596553+00:00","id":8246,"links":{},"metadata":{"_buckets":{"deposit":"a8628f51-ddd4-4ba4-996a-beddb6a5675a"},"_deposit":{"created_by":3,"id":"8246","owners":[3],"pid":{"revision_id":0,"type":"depid","value":"8246"},"status":"published"},"_oai":{"id":"oai:fukuyama-u.repo.nii.ac.jp:00008246","sets":["502:505:675:713"]},"author_link":["44368","44361","44364","44366","44362","44365","44360","44367","44363"],"item_1_biblio_info_14":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2005-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"317","bibliographicPageStart":"311","bibliographicVolumeNumber":"29","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":"44360","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"真鍋, 圭司"}],"nameIdentifiers":[{"nameIdentifier":"44361","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"西尾, 正富"}],"nameIdentifiers":[{"nameIdentifier":"44362","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":"The flowfield analysis around a model of space plane traveling at Mach 10 has been carried out utilizing an Electrical Discharge Method and a Finite Element Method (FEM) scheme. The Electrical Discharge Method can be visualized almost all important hypersonic flowfield phenomena, such as three-dimensional shock shapes, streamlines near wall surface, distant streamlines from wall surface, and boundary layers etc. In this study, the experiments and the numerical simulations were carried out under the conditions the angle of attack were 0 and 10 deg. Furthermore, the experimental results were compared with the numerical ones. In these comparisons, it was found that they were relatively in good agreement.","subitem_description_type":"Other"}]},"item_1_full_name_7":{"attribute_name":"著者名よみ","attribute_value_mlt":[{"nameIdentifiers":[{"nameIdentifier":"44363","nameIdentifierScheme":"WEKO"}],"names":[{"name":"ナカムラ, ヒロアキ"}]},{"nameIdentifiers":[{"nameIdentifier":"44364","nameIdentifierScheme":"WEKO"}],"names":[{"name":"マナベ, ケイジ"}]},{"nameIdentifiers":[{"nameIdentifier":"44365","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":"44366","nameIdentifierScheme":"WEKO"}],"names":[{"name":"NAKAMURA, Hiroaki","nameLang":"en"}]},{"nameIdentifiers":[{"nameIdentifier":"44367","nameIdentifierScheme":"WEKO"}],"names":[{"name":"MANABE, Keiji","nameLang":"en"}]},{"nameIdentifiers":[{"nameIdentifier":"44368","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":"Fukuyama University"},{"subitem_text_language":"en","subitem_text_value":"Department of Mechanical System Engineering, Faculty of Engineering, 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":"福山大学大学院工学研究科設計生産工学専攻"},{"subitem_text_value":"福山大学工学部機械システム工学科"},{"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":"2005-12-01"}],"displaytype":"detail","filename":"KJ00005781661.pdf","filesize":[{"value":"1.5 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"url":"https://fukuyama-u.repo.nii.ac.jp/record/8246/files/KJ00005781661.pdf"},"version_id":"fa7d48fe-215a-4e45-9daf-471ac6d3f1d2"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"スペースプレーン","subitem_subject_scheme":"Other"},{"subitem_subject":"放電発光法","subitem_subject_scheme":"Other"},{"subitem_subject":"有限要素法","subitem_subject_scheme":"Other"},{"subitem_subject":"Space Plane","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Hypersonic Flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Electrical Discharge Method","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":"完全再使用型単段式宇宙航空機(SSTO)周りの流れ場解析","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"完全再使用型単段式宇宙航空機(SSTO)周りの流れ場解析"},{"subitem_title":"Flowfield Analysis around Space Plane","subitem_title_language":"en"}]},"item_type_id":"1","owner":"3","path":["713"],"pubdate":{"attribute_name":"公開日","attribute_value":"2005-12-01"},"publish_date":"2005-12-01","publish_status":"0","recid":"8246","relation_version_is_last":true,"title":["完全再使用型単段式宇宙航空機(SSTO)周りの流れ場解析"],"weko_creator_id":"3","weko_shared_id":-1},"updated":"2023-06-19T10:27:09.171487+00:00"}