{"created":"2023-06-20T15:13:35.993578+00:00","id":43524,"links":{},"metadata":{"_buckets":{"deposit":"ee5c583f-26bb-4eaf-97e3-245e6559a6f9"},"_deposit":{"created_by":1,"id":"43524","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"43524"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00043524","sets":["1887:1893","1896:1898:1913:1915"]},"author_link":["464062","464059","464060","464057","464058","464061"],"item_3_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"NACA-0012翼周りの遷音速流の計算"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1991-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"184","bibliographicPageStart":"177","bibliographicVolumeNumber":"16","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所特別資料"},{"bibliographic_title":"Special Publication of National Aerospace Laboratory SP-16","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Two turbulence models have been used to simulate a typical flow around NACA-0012 at zero angle of attack. Those turbulence models are the Cebeci-Smith Model (CSM) and the Baldwin-Lomax Model (BLM). Analysis of these models in terms of turbulent boundary layer has also been carried out in which the differences in the predicted turbulent characteristics are made clear. The computed result is compared with the experimental data obtained from the transonic tunnel at Nagoya University.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALSP0016028","subitem_description_type":"Other"}]},"item_3_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: NAL SP-16","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory(NAL)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0289-260X","subitem_source_identifier_type":"ISSN"}]},"item_3_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN10097345","subitem_source_identifier_type":"NCID"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"名古屋大学"},{"subitem_text_value":"名古屋大学"},{"subitem_text_value":"名古屋大学"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Department of Aeronautical Engineering Nagoya University"},{"subitem_text_language":"en","subitem_text_value":"Department of Aeronautical Engineering Nagoya University"},{"subitem_text_language":"en","subitem_text_value":"Department of Aeronautical Engineering Nagoya University"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"サキャ, アンデイ エカ"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"中村, 佳朗"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"保原, 充"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sakya, Andi Eka","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nakamura, Yoshiaki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yasuhara, Michiru","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2020-01-28"}],"displaytype":"detail","filename":"nalsp0016028.pdf","filesize":[{"value":"1.1 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0016028.pdf","url":"https://jaxa.repo.nii.ac.jp/record/43524/files/nalsp0016028.pdf"},"version_id":"8e54f24e-b046-48f6-b11e-94813c6c5bfa"}]},"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":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"Transonic Flow Calculation around NACA-0012","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Transonic Flow Calculation around NACA-0012","subitem_title_language":"en"}]},"item_type_id":"3","owner":"1","path":["1893","1915"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"43524","relation_version_is_last":true,"title":["Transonic Flow Calculation around NACA-0012"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:12:42.329729+00:00"}