{"created":"2023-06-20T15:15:20.134749+00:00","id":45409,"links":{},"metadata":{"_buckets":{"deposit":"a9703b45-2873-4ade-8c63-ddd93bb8d35b"},"_deposit":{"created_by":1,"id":"45409","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"45409"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00045409","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["474647","474646","474657","474654","474649","474651","474655","474650","474653","474648","474652","474645","474644","474656"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Estimation of Critical Values and Vibration Characteristics on Supersonic Delta Wings Part 1 On-Line Time Series Analysis of Stationary Random Response"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1992-04","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"17","bibliographicVolumeNumber":"1153","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory TR-1153","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"振動試験や風洞試験の現場で試験中に翼の振動特性やフラッタ限界値を推定するため,自己回帰モデルによる限界値推定法をBASIC言語でプログラムし,オンライン時系列解析するシステムをパーソナルコンピュータで構築した。システムを評価するため,超音速デルタ翼模型の振動試験とサブクリティカルな風洞試験を行い,翼の定常な不規則応答データを取得した。本システムを用いて推定した結果,その実用性が十分に確かめられた。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A personal computer based, on-line time series analysis system is described which estimates the flutter boundary and vibration-mode parameter of a flutter model. The system software is written is BASIC and uses an autoregressive process. Ground vibration and wind tunnel flutter tests were conducted on supersonic delta wing models to enable system evaluation. Stationary random response of the wings was subsequently applied into the system and its practical use was confirmed using the estimated results.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTR1153000","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-1153","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機体部"},{"subitem_text_value":"名古屋大学"},{"subitem_text_value":"航空宇宙技術研究所機体部"},{"subitem_text_value":"航空宇宙技術研究所構造力学部"},{"subitem_text_value":"航空宇宙技術研究所空気力学部"},{"subitem_text_value":"航空宇宙技術研究所空気力学部"},{"subitem_text_value":"航空宇宙技術研究所空気力学部"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Airframe Division, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"Nagoya Univerisity"},{"subitem_text_language":"en","subitem_text_value":"Airframe Division, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"Structural Mechanics Division, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"Aerodynamics Division, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"Aerodynamics Division, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"Aerodynamics Division, National Aerospace Laboratory(NAL)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"安藤, 泰勝"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"松崎, 雄嗣"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"峯岸, 正勝"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"江尻, 宏"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"榊原, 盛三"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"野田, 順一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"石田, 清道"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"ANDO, Yasukatsu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"MATSUZAKI, Yuji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"MINEGISHI, Masakatsu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"EJIRI, Hiroshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"SAKAKIBARA, Seizo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"NODA, Junichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"ISHIDA, Kiyomichi","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":"naltr01153.pdf","filesize":[{"value":"1.4 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr01153.pdf","url":"https://jaxa.repo.nii.ac.jp/record/45409/files/naltr01153.pdf"},"version_id":"ea0a2a20-e527-43c2-996b-4cf57869f84e"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Supersonic delta wing;  vibration-mode parameter;  flutter boundary;  stationary random response;  autoregressive estimation method","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":"超音速デルタ翼の振動特性と安定限界の推定 第1報 定常な不規則応答のオンライン時系列解析","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"超音速デルタ翼の振動特性と安定限界の推定 第1報 定常な不規則応答のオンライン時系列解析"}]},"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":"45409","relation_version_is_last":true,"title":["超音速デルタ翼の振動特性と安定限界の推定 第1報 定常な不規則応答のオンライン時系列解析"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:40:01.815869+00:00"}