{"created":"2023-06-20T15:13:14.759542+00:00","id":43174,"links":{},"metadata":{"_buckets":{"deposit":"dcd82498-f997-4d98-9a5d-a0b7cb1064d5"},"_deposit":{"created_by":1,"id":"43174","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"43174"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00043174","sets":["1887:1893","1896:1898:1913:1915"]},"author_link":["462486","462485"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Application of Computational Aerodynamics to Wing Design"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1984-11","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"278","bibliographicPageStart":"271","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":"Recent progress in Computational Aerodynamics has enabled the engineers of air-craft manufacturers to utilize transonic aerodynamic analysis programs in designing wings. When using these programs in wing design, points like (Configuration modelling) effects of fuselage, effects of control surfaces, effects of nacelle, etc (Computational method) effects of viscosity, effects of separation, etc. should be taken into account to select a program or to model a configuration. Effectiveness of control surfaces (spoiler, aileron), which is greatly influenced by the characteristics of the wing, is another important problem. This paper introduces application of transonic aerodynamic analysis programs to the computation of control surface effective-ness.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALSP0003032","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":"富士重工業株式会社"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Fuji Heavy Industries Ltd."}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"中舘, 正顯"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nakadate, Masaaki","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":"nalsp0003032.pdf","filesize":[{"value":"333.5 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0003032.pdf","url":"https://jaxa.repo.nii.ac.jp/record/43174/files/nalsp0003032.pdf"},"version_id":"a4b71a7f-d713-4f96-b8e5-90eecc6af0c0"}]},"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":"主翼設計における空力計算の利用について","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"主翼設計における空力計算の利用について"}]},"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":"43174","relation_version_is_last":true,"title":["主翼設計における空力計算の利用について"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:21:06.421321+00:00"}