{"created":"2023-06-20T15:14:04.635557+00:00","id":44046,"links":{},"metadata":{"_buckets":{"deposit":"21503c27-dbac-4268-ba3f-b74581ada430"},"_deposit":{"created_by":1,"id":"44046","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"44046"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00044046","sets":["1887:1893","1896:1898:1913:1916"]},"author_link":["467271","467270","467266","467267","467269","467268"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"A Dynamic Model Wind-Tunnel Experiment with Gust Alleviation System"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1982-05","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"23","bibliographicVolumeNumber":"463","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所資料"},{"bibliographic_title":"Technical Memorandum of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"In this paper the results of wind-tunnel experiments of a dynamic model with a gust alleviator are reported. The experiments were planned on the basis of previously reported examinations and experiments. The gust alleviation system was a simple verical acceleration feedback system to the flap and elevator. The originally planned system, in which the elevator control law was to have canceled the quasi steady pitching moment produced by the flap,failed during the experiments. The system that succeeded resulted in an elevator control almost 180 degree oppositely phased to the planned system. This inconsistency was in some degree analytically resolved by describing realistic filter characteristics. The experiments was made in the NAL Gust-Wind-Tunnel,using a heave-and-pitchi free 0.1 dynamically rough-scaled model of a Beech Queen Air. As a whole result,the simple model system adopting micromotor serbos,showed possibilities for an economic dyanamic model wind-tunnel experiment.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTM0463000","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 TM-463","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":"0452-2982","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":"AN00314334","subitem_source_identifier_type":"NCID"}]},"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"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"西村, 博史"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"松下, 洸"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"岩崎, 昭人"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"NISHIMURA, Hiroshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"MATSUSHITA, Hiroshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"IWASAKI, Akihito","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":"naltm00463.pdf","filesize":[{"value":"2.6 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltm00463.pdf","url":"https://jaxa.repo.nii.ac.jp/record/44046/files/naltm00463.pdf"},"version_id":"579aa29a-9df5-4ccd-a797-799e7dd168ff"}]},"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":"突風軽減装置付き動的模型の実験","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"突風軽減装置付き動的模型の実験"}]},"item_type_id":"3","owner":"1","path":["1893","1916"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"44046","relation_version_is_last":true,"title":["突風軽減装置付き動的模型の実験"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:03:33.037676+00:00"}