{"created":"2021-03-01T06:39:08.647404+00:00","id":30787,"links":{},"metadata":{"_buckets":{"deposit":"398e838c-bcd2-408f-a6ae-1113baefc09d"},"_deposit":{"id":"30787","owners":[],"pid":{"revision_id":0,"type":"depid","value":"30787"},"status":"published"},"_oai":{"id":"oai:nagoya.repo.nii.ac.jp:00030787","sets":["320:2524:2544:2557"]},"author_link":["102090","102091","102092"],"item_1615768549627":{"attribute_name":"出版タイプ","attribute_value_mlt":[{"subitem_version_resource":"http://purl.org/coar/version/c_970fb48d4fbd8a85","subitem_version_type":"VoR"}]},"item_9_biblio_info_6":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1986-03-31","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"2","bibliographicPageEnd":"218","bibliographicPageStart":"203","bibliographicVolumeNumber":"37","bibliographic_titles":[{"bibliographic_title":"Memoirs of the Faculty of Engineering, Nagoya University","bibliographic_titleLang":"en"}]}]},"item_9_description_4":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"The Beam-Warming scheme was applied to transonic flows around two-dimensional airfoils NACA 0012 and RAE 2822, taking account of the Baldwin-Lomax turbulence model. After appropriate grid generation techniques, the calculation successfully lead to steady flows containing a shock wave and flow separation, for a uniform flow Mach number 0.75, the Reynolds number 6×10[6] , and angles of attack 0 to 15 degrees. Note that periodical oscillations were observed at high angles of attack.","subitem_description_language":"en","subitem_description_type":"Abstract"}]},"item_9_identifier_registration":{"attribute_name":"ID登録","attribute_value_mlt":[{"subitem_identifier_reg_text":"10.18999/memfenu.37.2.203","subitem_identifier_reg_type":"JaLC"}]},"item_9_publisher_32":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"Faculty of Engineering, Nagoya University","subitem_publisher_language":"en"}]},"item_9_select_15":{"attribute_name":"著者版フラグ","attribute_value_mlt":[{"subitem_select_item":"publisher"}]},"item_9_source_id_7":{"attribute_name":"ISSN（print）","attribute_value_mlt":[{"subitem_source_identifier":"0027-7657","subitem_source_identifier_type":"PISSN"}]},"item_access_right":{"attribute_name":"アクセス権","attribute_value_mlt":[{"subitem_access_right":"open access","subitem_access_right_uri":"http://purl.org/coar/access_right/c_abf2"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"Fujiwara, Toshi","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"102090","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Wang, Yi-Yun","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"102091","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Ohmori, Yasunori","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"102092","nameIdentifierScheme":"WEKO"}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2020-11-04"}],"displaytype":"detail","filename":"37-2-03.pdf","filesize":[{"value":"1.4 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"37-2-03.pdf","objectType":"fulltext","url":"https://nagoya.repo.nii.ac.jp/record/30787/files/37-2-03.pdf"},"version_id":"bf6b0060-dd1c-43fd-958e-9da6e1360a6d"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"eng"}]},"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":"Turbulent transonic flow for NACA 0012/RAE 2822 airfoils under Baldwin-Lomax model","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Turbulent transonic flow for NACA 0012/RAE 2822 airfoils under Baldwin-Lomax model","subitem_title_language":"en"}]},"item_type_id":"9","owner":"1","path":["2557"],"pubdate":{"attribute_name":"PubDate","attribute_value":"2020-11-04"},"publish_date":"2020-11-04","publish_status":"0","recid":"30787","relation_version_is_last":true,"title":["Turbulent transonic flow for NACA 0012/RAE 2822 airfoils under Baldwin-Lomax model"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-01-16T04:24:20.702879+00:00"}