{"created":"2023-06-20T15:11:45.797568+00:00","id":41490,"links":{},"metadata":{"_buckets":{"deposit":"fdac12d0-e377-40a2-9a3f-92e20efde733"},"_deposit":{"created_by":1,"id":"41490","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"41490"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00041490","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["452676","452675","452670","452673","452679","452678","452674","452671","452672","452677"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Model with turbine powered simulators at NAL's low speed wind tunnel facility"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2000-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"63","bibliographicPageStart":"1","bibliographicVolumeNumber":"1421","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"この技術論文は、航空宇宙技術研究所の大型低速風洞(6.5m×5.5m)における模擬エンジン付き模型の試験装置について述べる。この実験装置の目的は、配管干渉を除去することによって模型に加わる空気力を高精度で計測するものである。模型は、8%STOL実験機'飛鳥'模型を用いた。本論文では、配管干渉除去機能と試験装置全体について説明する。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"This paper describes a test system of an eight percent scale model of STOL (Short Take-Off and Landing) aircraft 'ASKA' with turbine powered simulators tested at the low speed wind tunnel (6.5 m x 5.5 m) of National Aerospace Laboratory (NAL). The purpose of the system is to achieve high accurate measurements of aerodynamic forces by eliminating piping interferences. The paper also describes performance of the piping interference elimination function and overall system test results.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0028666000","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-1421","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"},{"subitem_text_value":"航空宇宙技術研究所"},{"subitem_text_value":"航空宇宙技術研究所"},{"subitem_text_value":"航空宇宙技術研究所"},{"subitem_text_value":"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":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"中谷, 輝臣"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"野中, 修"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"室田, 勝一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"近藤, 洋史"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"林, 良生"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nakaya, Teruomi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nonaka, Osamu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Murota, Shoichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kondo, Hirofumi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hayashi, Yoshio","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":"2020-01-27"}],"displaytype":"detail","filename":"naltr0001421.pdf","filesize":[{"value":"8.3 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr0001421.pdf","url":"https://jaxa.repo.nii.ac.jp/record/41490/files/naltr0001421.pdf"},"version_id":"fb00560f-4e48-48cc-a6eb-fb4980290bc4"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"模擬エンジン","subitem_subject_scheme":"Other"},{"subitem_subject":"低速風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"STOL機","subitem_subject_scheme":"Other"},{"subitem_subject":"短距離離着陸","subitem_subject_scheme":"Other"},{"subitem_subject":"空気力","subitem_subject_scheme":"Other"},{"subitem_subject":"高精度計測","subitem_subject_scheme":"Other"},{"subitem_subject":"配管干渉","subitem_subject_scheme":"Other"},{"subitem_subject":"空気軸受","subitem_subject_scheme":"Other"},{"subitem_subject":"高圧空気","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞試験システム","subitem_subject_scheme":"Other"},{"subitem_subject":"turbine powered simulator","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"low speed wind tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"STOL aircraft","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"short takeoff and landing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic force","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"high accurate measurement","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"piping interference","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"air bearing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"pressurized air","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel test system","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":"大型低速風洞の動力付模型試験システム","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"大型低速風洞の動力付模型試験システム"}]},"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":"41490","relation_version_is_last":true,"title":["大型低速風洞の動力付模型試験システム"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:10:34.676708+00:00"}