{"created":"2023-06-20T15:13:14.177091+00:00","id":43162,"links":{},"metadata":{"_buckets":{"deposit":"1bbad030-0a9d-40b7-b360-b9e69973a606"},"_deposit":{"created_by":1,"id":"43162","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"43162"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00043162","sets":["1887:1893","1896:1898:1913:1915"]},"author_link":["462437","462435","462438","462436"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Development of Subsonic Computational Aerodynamic Program Using Panel Method"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1984-11","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"174","bibliographicPageStart":"165","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 paper presents the Subsonic Computational Aerodynamic Program (SUSCAP) that we have developed as an effective design tool to reduce the cost and time of wind tunnel tests. This code is based on a potential flow Panel Method coupled with a vortex-sheets renewal technique. The main function of the code is aerodynamic coefficient estimation of a three dimensional flying object. Other functions are also added, that is, velocity estimation at arbitrary points apart from the boundary suface, and high subsonic flow simulation by Prandtl-Glauert transformation. In order to investigate the usefulness of the code in designing aerodynamic shapes, this code is applied to a Wing-Boby-Tail configuration and a cruciform missile configuration. Their pressure distributions and roll moments are calculated. Calculated results are compared with the measured data, and the agreement is found satisfactory.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALSP0003020","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":"三菱電機株式会社鎌倉製作所"},{"subitem_text_value":"三菱電機株式会社鎌倉製作所"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Electric Corp., Kamakura Works"},{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Electric Corp., Kamakura Works"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"黒崎, 隆二郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"片山, 雅之"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kurosaki, Ryujirou","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Katayama, Masayuki","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":"nalsp0003020.pdf","filesize":[{"value":"672.3 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0003020.pdf","url":"https://jaxa.repo.nii.ac.jp/record/43162/files/nalsp0003020.pdf"},"version_id":"7efc53cd-6ef0-459b-a334-a7d0bf766095"}]},"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":"パネル法による亜音速計算空カプログラムの開発","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"パネル法による亜音速計算空カプログラムの開発"}]},"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":"43162","relation_version_is_last":true,"title":["パネル法による亜音速計算空カプログラムの開発"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:21:23.232741+00:00"}