{"created":"2023-06-20T15:13:35.227646+00:00","id":43509,"links":{},"metadata":{"_buckets":{"deposit":"3ad976b3-3949-4b42-9478-720e7be81b57"},"_deposit":{"created_by":1,"id":"43509","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"43509"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00043509","sets":["1887:1893","1896:1898:1913:1915"]},"author_link":["463969","463970"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Calculations of Aerodynamic Forces on a Wing with Thrust Using B.E.M."}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1991-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"82","bibliographicPageStart":"77","bibliographicVolumeNumber":"16","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-16","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A procedure for the numerical solution of steady flow past a wing with fans is descried using a boundary element method in potential flow. The effect of thrust is represented by doublet singularities. The method employs an aerodynamic panel code to simulate the flow of fan jet stream around an aircraft configuration. The configuration of a VTOL transport in achieving a multijet lifting system is composed of lifting fans nested in the wing planform. The aerodynamic forces were calculated with the fundamental shape of FAN IN WING. The result is that there are regions of negative lift behind the position of the lift fan on the wing. The general tendency of how they interact with the wing to produce the aerodynamic forces is understood.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALSP0016013","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-16","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":"東京理科大学"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Science University of Tokyo"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"柳沢, 三憲"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yanagizawa, Mitsunori","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":"nalsp0016013.pdf","filesize":[{"value":"285.6 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0016013.pdf","url":"https://jaxa.repo.nii.ac.jp/record/43509/files/nalsp0016013.pdf"},"version_id":"59a72786-1139-466e-9dcf-1e8628f79291"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Aerodynamics; Wing; BEM; Thrust","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":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"境界要素法による推力付翼の空力計算","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"境界要素法による推力付翼の空力計算"}]},"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":"43509","relation_version_is_last":true,"title":["境界要素法による推力付翼の空力計算"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:13:07.157575+00:00"}