{"created":"2023-06-20T15:15:00.449723+00:00","id":45039,"links":{},"metadata":{"_buckets":{"deposit":"22cd0557-1302-4819-8de8-23608fb6ab74"},"_deposit":{"created_by":1,"id":"45039","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"45039"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00045039","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["472607","472606"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Doublet Point Method for Calculations on Oscillatory Lifting Surfaces Part 1. Subsonic Flow"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1983-10","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"13","bibliographicVolumeNumber":"781","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory TR-781","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A simple method for calculating the unsteady aerodynamic loadings on harmonically oscillating thin wings in subsonic flow has been developed. The method is basaed on a concept of concentrated lift forces. The wing is divided into the element surfaces on which lift distributions are represented by single concentrated lift forces. Since the procedure does not include any quadratures, it can easily be applied to calculate the unsteady aerodynamic loadings on complex planform wings even when they have partial span control surfaces. Numerical calculations are carried out for various wing geometries and are compared with other analyses and experiments.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTR0781000","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-781","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":"上田, 哲彦"}],"nameIdentifiers":[{"nameIdentifier":"472606","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"UEDA, Tetsuhiko","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"472607","nameIdentifierScheme":"WEKO"}]}]},"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":"naltr00781.pdf","filesize":[{"value":"867.3 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr00781.pdf","url":"https://jaxa.repo.nii.ac.jp/record/45039/files/naltr00781.pdf"},"version_id":"d67c7db2-a702-4efc-b47c-fadeb2bf2ce9"}]},"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":"振動揚力面計算のダブレット・ポイント法 その1.亜音速流","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"振動揚力面計算のダブレット・ポイント法 その1.亜音速流"}]},"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":"45039","relation_version_is_last":true,"title":["振動揚力面計算のダブレット・ポイント法 その1.亜音速流"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:46:24.138423+00:00"}