{"created":"2023-06-20T15:15:19.587882+00:00","id":45401,"links":{},"metadata":{"_buckets":{"deposit":"f4b22507-d20f-45d8-8bdc-57f990740bb3"},"_deposit":{"created_by":1,"id":"45401","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"45401"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00045401","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["474587","474586","474582","474583","474589","474588","474585","474584"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Low-Speed Wind Tunnel Study of the Direct Lift and Direct Side-Force Characteristics of a Joined-Wing Airplane"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1992-03","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"29","bibliographicVolumeNumber":"1142","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory TR-1142","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"平面と正面図が菱形をなすように配置された前方翼と後方翼を持つ結合翼機は,本来直接揚力・横力制御に適した形態である。しかしこれらの能力については,いまだ明らかでなく,検討に必要な資料も現在発表されていない。そこで,直接揚力・横力制御に関する空力データの取得と評価のために,四つの菱形結合翼機模型を用いて低速風洞試験を実施した。その中の三つの模型は,平面形において主翼と水平尾翼が重なり合うことがない結合形態で,他の一つは重なり合う形態のものである。前者は後方翼の翼幅比(後方翼/前方翼)が,それぞれ0.40,0.60および1.00であり,後者は1.00のみである。これらの模型は,その垂直尾翼の高さ,および垂直尾翼と胴体の結合位置を除いては全て同じ形状である。本報告では低速風洞試験の結果を基として,各結合翼機の直接制御揚力・横力特性を舵面の面積比(舵面面積/主翼面積)や舵面舵角に対して述べる。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Low-speed wind tunnel tests were conducted to obtain aerodynamic data for evaluating direct lift and direct side-force characteristics of four joined-wing airplane models employing a front and rear wing which form diamond shapes in the plan and front view. Three models had a joint configuration in which the front and rear wings do not overlap each other in the plan view, having a rear wing span ratio(rear/front wing) of 0.40, 0.60, and 1.00. The fourth had a joint configuration where both wings overlap with a rear wing span ratio of 1.00. Models possessed the same geometric parameters with the exception of their vertical tail height and body. Resultant direct lift and direct side-force characteristics are presented with respect to the wing area ratios (rear/front wing), and include the effect of different control surface area ratios and the angle of the control surface.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTR1142000","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-1142","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新型航空機研究グループ"},{"subitem_text_value":"航空宇宙技術研究所新型航空機研究グループ"},{"subitem_text_value":"航空宇宙技術研究所新型航空機研究グループ"},{"subitem_text_value":"元・航空宇宙技術研究所"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Advanced Aircraft Research Group, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"Advanced Aircraft Research Group, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"Advanced Aircraft Research Group, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"Former National Aerospace Laboratory(NAL)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"藤田, 敏美"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"岩崎, 昭人"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"藤枝, 郭俊"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"滝澤, 直人"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"FUJITA, Toshimi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"IWASAKI, Akihito","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"FUJIEDA, Hirotoshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"TAKIZAWA, NAOTO","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":"naltr01142.pdf","filesize":[{"value":"2.0 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr01142.pdf","url":"https://jaxa.repo.nii.ac.jp/record/45401/files/naltr01142.pdf"},"version_id":"d0bd8aa2-c4e3-441e-bf6e-ad8315312498"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Low-speed wind tunnel;  Joined-wing airplane;  Direct Lift;  Side-force","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":"菱形結合翼機の直接揚力・横力制御力の低速風洞試験","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"菱形結合翼機の直接揚力・横力制御力の低速風洞試験"}]},"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":"45401","relation_version_is_last":true,"title":["菱形結合翼機の直接揚力・横力制御力の低速風洞試験"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:40:09.522533+00:00"}