{"created":"2023-06-20T15:13:14.861430+00:00","id":43176,"links":{},"metadata":{"_buckets":{"deposit":"1adda12e-e513-4350-b6a6-fdc6ef04cf1b"},"_deposit":{"created_by":1,"id":"43176","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"43176"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00043176","sets":["1887:1893","1896:1898:1913:1915"]},"author_link":["462490","462492","462489","462491"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"A Wing Design Based on the Three-Dimensional Transonic Inverse Method and the Comparison with the Wind Tunnel Testing Data"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1984-11","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"304","bibliographicPageStart":"293","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":"Along with the recent progress in computational aerodynamics, aircraft designers have paid great attention to inverse methods. Inverse methods, which determine wing geometries under prescribed target pressure distributions, are considered important design techniques because of the applicabilities of experience and knowledge of aircraft de-signers. Although several two-dimensional methods have already been established, there exist only a few reports about three-dimensional transonic inverse methods, and the three-dimensional technique has not been established yet, This report deseribes wing design by the three-dimensional transonic inverse method using the integral equation formulation which was developed by one of the authors. The method has the great advantage that various flow-solvers can be applied. Also wind tunnel testing was condueted with the designed wing to investigate the capability of the method. The comparison of design and test results shows a good agreement and the method proves to be very effective in three-dimensional transonic wing design.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALSP0003034","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":"三菱重工業株式会社"},{"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":"National Aerospace Laboratory"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"巽, 重文"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"高梨, 進"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tatsumi, Shigefumi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Takanashi, Susumu","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":"nalsp0003034.pdf","filesize":[{"value":"618.9 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0003034.pdf","url":"https://jaxa.repo.nii.ac.jp/record/43176/files/nalsp0003034.pdf"},"version_id":"410eef57-053f-4166-bbdd-082d7d53504f"}]},"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":"三次元遷音速逆解法を用いた翼の設計と風洞試験","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"三次元遷音速逆解法を用いた翼の設計と風洞試験"}]},"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":"43176","relation_version_is_last":true,"title":["三次元遷音速逆解法を用いた翼の設計と風洞試験"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:21:03.026334+00:00"}