{"created":"2023-06-20T15:13:17.721152+00:00","id":43220,"links":{},"metadata":{"_buckets":{"deposit":"0af7e301-fd3a-4850-b70f-ad958f3f2ba7"},"_deposit":{"created_by":1,"id":"43220","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"43220"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00043220","sets":["1887:1893","1896:1898:1913:1915"]},"author_link":["462667","462668","462673","462672","462669","462671","462666","462670"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Practical Application of Two-Dimensional Viscous Flow Computation"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1986-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"38","bibliographicPageStart":"33","bibliographicVolumeNumber":"7","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-7","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Computational aerodynamics as an aircraft design tool now stands shoulder to shoulder with wind tunnel testing due to the rapid progress of computer software and hardware. In particular, the Navier-Stokes computation which has been researched re-cently, enables us to analyze airflow not only at a design point but also in off-design regions. NSFOIL, the high Reynolds number transonic airfoil analysis code developed at NAL, has been verified by comparing computations based on the code with results obtained from actual wind tunnel tests. This paper presents a validative discussion of the NSFOIL code in the region of low speed and high attack angle. The computational results are compared with results of wind tunnel tests and the vortex method, which is a separated flow analysis method, to in-vestigate the validity of the code and to further the development of future improvements. NSFOIL is found to be able to predict non-linear characteristics, in which conventional numerical methods are powerless. There is still some room for improvement to be able to calculate an exact stall angle.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALSP0007004","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-7","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":"三菱重工業株式会社"},{"subitem_text_value":"三菱重工業株式会社"},{"subitem_text_value":"航空宇宙技術研究所"},{"subitem_text_value":"航空宇宙技術研究所"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Heavy Industries Co.Ltd."},{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Heavy Industries Co.Ltd."},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"海田, 武司"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"宮川, 淳一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"廣瀬, 直喜"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"河合, 伸坦"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kaiden, Takeshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Miyakawa, Jun-ichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hirose, Naoki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kawai, Nobuhiro","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":"nalsp0007004.pdf","filesize":[{"value":"719.4 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0007004.pdf","url":"https://jaxa.repo.nii.ac.jp/record/43220/files/nalsp0007004.pdf"},"version_id":"14ba1281-9562-46a4-a310-d736fb75f072"}]},"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":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"二次元粘性流計算ソフトウェアの実用化","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"二次元粘性流計算ソフトウェアの実用化"}]},"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":"43220","relation_version_is_last":true,"title":["二次元粘性流計算ソフトウェアの実用化"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:19:59.492818+00:00"}