{"_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": []}, "author_link": ["102090", "102091", "102092"], "item_9_biblio_info_6": {"attribute_name": "\u66f8\u8a8c\u60c5\u5831", "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"}]}]}, "item_9_description_4": {"attribute_name": "\u6284\u9332", "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\u00d710[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\u767b\u9332", "attribute_value_mlt": [{"subitem_identifier_reg_text": "10.18999/memfenu.37.2.203", "subitem_identifier_reg_type": "JaLC"}]}, "item_9_publisher_32": {"attribute_name": "\u51fa\u7248\u8005", "attribute_value_mlt": [{"subitem_publisher": "Faculty of Engineering, Nagoya University"}]}, "item_9_select_15": {"attribute_name": "\u8457\u8005\u7248\u30d5\u30e9\u30b0", "attribute_value_mlt": [{"subitem_select_item": "publisher"}]}, "item_9_source_id_7": {"attribute_name": "ISSN\uff08print\uff09", "attribute_value_mlt": [{"subitem_source_identifier": "0027-7657", "subitem_source_identifier_type": "PISSN"}]}, "item_creator": {"attribute_name": "\u8457\u8005", "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": "\u30d5\u30a1\u30a4\u30eb\u60c5\u5831", "attribute_type": "file", "attribute_value_mlt": [{"accessrole": "open_date", "date": [{"dateType": "Available", "dateValue": "2020-11-04"}], "displaytype": "detail", "download_preview_message": "", "file_order": 0, "filename": "37-2-03.pdf", "filesize": [{"value": "1.4 MB"}], "format": "application/pdf", "future_date_message": "", "is_thumbnail": false, "licensetype": "license_note", "mimetype": "application/pdf", "size": 1400000.0, "url": {"label": "37-2-03.pdf", "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": "\u8a00\u8a9e", "attribute_value_mlt": [{"subitem_language": "eng"}]}, "item_resource_type": {"attribute_name": "\u8cc7\u6e90\u30bf\u30a4\u30d7", "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": "\u30bf\u30a4\u30c8\u30eb", "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": ["320/2524/2544/2557"], "permalink_uri": "https://doi.org/10.18999/memfenu.37.2.203", "pubdate": {"attribute_name": "PubDate", "attribute_value": "2020-11-04"}, "publish_date": "2020-11-04", "publish_status": "0", "recid": "30787", "relation": {}, "relation_version_is_last": true, "title": ["Turbulent transonic flow for NACA 0012/RAE 2822 airfoils under Baldwin-Lomax model"], "weko_shared_id": -1}