{"created":"2023-06-20T15:15:16.273816+00:00","id":45342,"links":{},"metadata":{"_buckets":{"deposit":"f314797f-14b4-4ce8-8e49-1fa7d6141304"},"_deposit":{"created_by":1,"id":"45342","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"45342"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00045342","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["474251","474252"],"item_3_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"飛行試験結果により推定したSTOL実験機″飛鳥″の空力弾性特性"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1990-10","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"39","bibliographicVolumeNumber":"1083","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory TR-1083","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Flight tests of the STOL research aircraft \"ASKA\" developed by the National Aerospace Laboratory were conducted in 1986. Acceleration responses due to turbulence at subcritical speeds of ASKA were obtained during the flight tests. To estimate the aeroelastic characteristics from the flight tests of ASKA, the obtained acceleration responses were applied to the method for estimating flutter or divergence boundary from random responses with the aid of the autoregressive(AR) process and the mixed autoregressive moving average(ARMA) process. The procedures and results of the estimations are presented in this report.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTR1083000","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-1083","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"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory(NAL)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"STOLプロジェクト推進本部"}],"nameIdentifiers":[{"nameIdentifier":"474251","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"STOL Research Aircraft Project Group","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"474252","nameIdentifierScheme":"WEKO"}]}]},"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":"naltr01083.pdf","filesize":[{"value":"2.1 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr01083.pdf","url":"https://jaxa.repo.nii.ac.jp/record/45342/files/naltr01083.pdf"},"version_id":"b05c15cc-2572-4043-a7f5-a076c2413228"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"eng"}]},"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":"Estimation of the Aeroelastic Characteristics from Flight Test Data of the STOL Research Aircraft″ASKA″","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Estimation of the Aeroelastic Characteristics from Flight Test Data of the STOL Research Aircraft″ASKA″","subitem_title_language":"en"}]},"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":"45342","relation_version_is_last":true,"title":["Estimation of the Aeroelastic Characteristics from Flight Test Data of the STOL Research Aircraft″ASKA″"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:42:35.739181+00:00"}