{"created":"2023-07-25T10:04:59.747806+00:00","id":949,"links":{},"metadata":{"_buckets":{"deposit":"b3b06df1-a211-4ac5-a61a-2b0f39536433"},"_deposit":{"created_by":3,"id":"949","owners":[3],"pid":{"revision_id":0,"type":"depid","value":"949"},"status":"published"},"_oai":{"id":"oai:sojo-u.repo.nii.ac.jp:00000949","sets":["1:35"]},"author_link":["2119","2120"],"item_20_biblio_info_4":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2016","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"125","bibliographicPageStart":"119","bibliographicVolumeNumber":"41","bibliographic_titles":[{"bibliographic_title":"崇城大学紀要"},{"bibliographic_title":"Bulletin of Sojo University","bibliographic_titleLang":"en"}]}]},"item_20_creator_2":{"attribute_name":"作成者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"松尾, 健輔"}],"nameIdentifiers":[{"nameIdentifier":"2119","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"田邉 和寛"}],"nameIdentifiers":[{"nameIdentifier":"2120","nameIdentifierScheme":"WEKO"}]}]},"item_20_description_1":{"attribute_name":"内容記述","attribute_value_mlt":[{"subitem_description":"本研究は、１枚翼面からなるセイルウイングを対象に、その前後縁形状が空力性能に及ぼす影響を明らかにすることを目的としている。前報１）においては、通常の航空機と同様に、機体の左右に１枚翼面構造のセイルウイングを取り付けた供試模型を用いた風洞試験を実施した。続いて、文献２および３では、１枚翼面構造のセイルウイング単体の空力性能を求めるために製作した供試模型を用いて、風洞試験を実施した。これらの結果から、１枚翼面構造のセイルウイングの空力特性が、前後縁形状に大きく影響されることを示した。さらに、文献４では、数値解析を実施することによって、それまでに実施した実験によって得られた知見の正当性を確認した。本報では、これらの手法を組み合わせると共に、新たに地面効果による影響を考慮することによって、１枚翼面構造のセイルウイングの実用性について示している。","subitem_description_type":"Other"}]},"item_20_publisher_5":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"崇城大学"}]},"item_20_source_id_6":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"2185-7903","subitem_source_identifier_type":"ISSN"}]},"item_20_subject_9":{"attribute_name":"国立情報学研究所 メタデータ主題語彙集","attribute_value_mlt":[{"subitem_subject":"Departmental Bulletin Paper","subitem_subject_scheme":"Other"}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2016-07-07"}],"displaytype":"detail","filename":"10 sojokiyou_41_Kensuke MATSUO.pdf","filesize":[{"value":"2.5 MB"}],"format":"application/pdf","licensetype":"license_8","mimetype":"application/pdf","url":{"label":"セイルウイングの空力性能に関する研究 ―続報","url":"https://sojo-u.repo.nii.ac.jp/record/949/files/10 sojokiyou_41_Kensuke MATSUO.pdf"},"version_id":"31cea813-5380-402a-b18a-575f951b4c62"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Sailwing ","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":" Ground effect ","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":" Openfoam ","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":" Numerical ","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":" analysis","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":"departmental bulletin paper","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"セイルウイングの空力性能に関する研究 ―続報","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"セイルウイングの空力性能に関する研究 ―続報"},{"subitem_title":"A Study of Sailwing Performance - Continued Paper","subitem_title_language":"en"}]},"item_type_id":"20","owner":"3","path":["35"],"pubdate":{"attribute_name":"公開日","attribute_value":"2016-07-07"},"publish_date":"2016-07-07","publish_status":"0","recid":"949","relation_version_is_last":true,"title":["セイルウイングの空力性能に関する研究 ―続報"],"weko_creator_id":"3","weko_shared_id":-1},"updated":"2023-07-25T10:16:29.805869+00:00"}