{"created":"2023-06-20T15:13:14.078316+00:00","id":43160,"links":{},"metadata":{"_buckets":{"deposit":"32cbb35c-684c-4f3b-b161-7857b83eb351"},"_deposit":{"created_by":1,"id":"43160","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"43160"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00043160","sets":["1887:1893","1896:1898:1913:1915"]},"author_link":["462431","462432"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Investigations on Efficient Numerical Method For Subsonic Lifting Surfaces"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1984-11","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"162","bibliographicPageStart":"149","bibliographicVolumeNumber":"3","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-3","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"This is an intermediate summary report on the numerical investigation of subsonic unsteady lifting surface, made by our group in Nagoya University Aeronautical Department. Our interest has been concentrated on simple planar cases because this enables us to investigate the condition economically and thoroughly and thus maximize convergence and accuracy. We, however, believe that most of the results thus obtained would be fundamentally useful even for more complicated problems, such as non-planar wings or wings with finite thickness. The results are divided into the following three main parts: 1) Introduction of error-index parameters E, and development of an adaptive numerical method for lifting surfaces 2) Improvement of numerical calculation of the subsonic kernerl function. 3) Development of new, accurate, fast-converging numerical methods for lifting surfaces. For two-dimensional airfoils a \"DLM-C\" method has been developed. For finite span wings a finite aerodynamic element method (\"DSM-CLS\") and two pressure mode methods (\"NAM\", \"NAS\") have been developed.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALSP0003018","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-3","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":"名古屋大学工学部"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"安東, 茂典"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ando, Shigenori","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":"nalsp0003018.pdf","filesize":[{"value":"831.2 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0003018.pdf","url":"https://jaxa.repo.nii.ac.jp/record/43160/files/nalsp0003018.pdf"},"version_id":"5c85d3b3-2350-4cc8-b082-f3b22a490b67"}]},"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":"亜音速揚力面の数値計算法に関する研究","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"亜音速揚力面の数値計算法に関する研究"}]},"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":"43160","relation_version_is_last":true,"title":["亜音速揚力面の数値計算法に関する研究"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:21:26.225858+00:00"}