{"created":"2023-06-20T15:07:30.706064+00:00","id":36878,"links":{},"metadata":{"_buckets":{"deposit":"1793923e-e953-4700-bb57-9a87541b91a2"},"_deposit":{"created_by":1,"id":"36878","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"36878"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00036878","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["477974","477975","477972","477971","477973","477978","477977","477976"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"On an inverse problem for a low aspect ratio wing"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1997-01","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"106","bibliographicPageStart":"101","bibliographicVolumeNumber":"34","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","bibliographic_titleLang":"en"}]}]},"item_5_description_14":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）","attribute_value_mlt":[{"subitem_description":"航空宇宙技術研究所 6-7 JUN. 1996 東京 日本","subitem_description_type":"Other"}]},"item_5_description_15":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）（英）","attribute_value_mlt":[{"subitem_description":"National Aerospace Laboratory 6-7 JUN. 1996 Tokyo Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"遷音速時において目標圧力分布を有する翼形状を計算するための高梨法は大アスペクト比の翼に対しては有用である。しかし、低アスペクト比翼に対してはこの方法による計算はしばしば発散してしまう。この方法を低アスペクト比翼に適用できるように修正した。計算例を紹介した。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Takanashi's method for calculating wing geometry having prescribed pressure distribution at transonic speed is useful for wings of large aspect ratio. The calculations by this method, however, sometimes diverge for wings of low aspect ratio. In this paper, this method is modified to be able to apply to the wings of low aspect ratio. Examples of the calculations are presented.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0000685019","subitem_description_type":"Other"}]},"item_5_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: NAL SP-34","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory (NAL)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0289-260X","subitem_source_identifier_type":"ISSN"}]},"item_5_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_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"名古屋大学 工学部"},{"subitem_text_value":"三菱重工業"},{"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_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Nagoya University School of Engineering"},{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Heavy Industries 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":"神谷, 信彦"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"服部, 恵介"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"高梨, 進"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"廣瀬, 直喜"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kamiya, Nobuhiko","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hattori, Keisuke","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Takanashi, Susumu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hirose, Naoki","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":"2020-02-10"}],"displaytype":"detail","filename":"nalsp0034019.pdf","filesize":[{"value":"396.8 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0034019.pdf","url":"https://jaxa.repo.nii.ac.jp/record/36878/files/nalsp0034019.pdf"},"version_id":"ee8bd656-7aca-4718-a89a-86e4e4d302fb"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"低アスペクト比翼","subitem_subject_scheme":"Other"},{"subitem_subject":"翼形状","subitem_subject_scheme":"Other"},{"subitem_subject":"表面圧力分布","subitem_subject_scheme":"Other"},{"subitem_subject":"逆問題","subitem_subject_scheme":"Other"},{"subitem_subject":"残差修正法","subitem_subject_scheme":"Other"},{"subitem_subject":"遷音速","subitem_subject_scheme":"Other"},{"subitem_subject":"目標翼形状","subitem_subject_scheme":"Other"},{"subitem_subject":"高梨法","subitem_subject_scheme":"Other"},{"subitem_subject":"low aspect ratio wing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wing geometry","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"surface pressure distribution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"inverse problem","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"residual correction method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transonic speed","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"specified wing shape","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Takanashi's method","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"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":"conference paper","resourceuri":"http://purl.org/coar/resource_type/c_5794"}]},"item_title":"低アスペクト比翼の逆問題解法について","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"低アスペクト比翼の逆問題解法について"}]},"item_type_id":"5","owner":"1","path":["1891","1915"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"36878","relation_version_is_last":true,"title":["低アスペクト比翼の逆問題解法について"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:29:59.534598+00:00"}