{"created":"2023-06-20T15:14:52.417969+00:00","id":44884,"links":{},"metadata":{"_buckets":{"deposit":"c915eb30-67c0-4a17-80bc-5432453706c1"},"_deposit":{"created_by":1,"id":"44884","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"44884"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00044884","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["471748","471747"],"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1980-09","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"11","bibliographicVolumeNumber":"629T","bibliographic_titles":[{},{"bibliographic_title":"Technical Report of National Aerospace Laboratory TR-629T","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"揚力面理論の積分方程式にCauchy積分に対するStarkの数値積分公式を適用することによって,矩形翼に対するvortex lattice法の理想的な格子配置を得た。これによって,格子渦の循環と対応する局所揚力との関係を明確に定義することができ,さらにこれからの当然の帰結として誘導抵抵の翼幅方向分布を精度よく計算できることを示した。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"An ideal lattice arrangement of the vortex-lattice method for rectangular wings is obtained by applying Stark’s quadrature formula for a Cauchy integral to the integral equation of the lifting-surface theory. The relation between the circulation of a lattice vortex and the corresponding local lift is thereby clearly defined, and the spanwise distribution of the induced drag is shown to be calculated accurately.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTR0629000","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 TR-629T","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":"0389-4010","subitem_source_identifier_type":"ISSN"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"航空宇宙技術研究所機体第一部"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"First Airframe Division, National Aerospace Laboratory(NAL)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"市川, 輝雄"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"ICHIKAWA, Teruo","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":"2020-01-29"}],"displaytype":"detail","filename":"naltr0629t.pdf","filesize":[{"value":"813.9 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr0629t.pdf","url":"https://jaxa.repo.nii.ac.jp/record/44884/files/naltr0629t.pdf"},"version_id":"0d52859a-8b91-4a59-a634-85158b3b4095"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"eng"}]},"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":"Considerations on Basis for Vortex-Lattice Method","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Considerations on Basis for Vortex-Lattice Method","subitem_title_language":"en"}]},"item_type_id":"3","owner":"1","path":["1893","1917"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"44884","relation_version_is_last":true,"title":["Considerations on Basis for Vortex-Lattice Method"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:49:09.509429+00:00"}