{"created":"2023-06-20T14:38:49.755723+00:00","id":5445,"links":{},"metadata":{"_buckets":{"deposit":"012a01db-3360-4507-9ab3-34b2ce6c045b"},"_deposit":{"created_by":1,"id":"5445","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"5445"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00005445","sets":["1887:1891","9:789:956:965"]},"author_link":["26441","26442","26440","26443"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Aeroelastic response of the second flight experiment of the SST experimental aircraft"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2009-02-27","bibliographicIssueDateType":"Issued"},"bibliographicVolumeNumber":"JAXA-SP-08-008","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料: 小型超音速実験機（ロケット実験機）飛行実験データ解析完了報告"},{"bibliographic_title":"JAXA Special Publication","bibliographic_titleLang":"en"}]}]},"item_5_description_14":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）","attribute_value_mlt":[{"subitem_description":"小型超音速実験機（ロケット実験機）飛行実験データ解析完了報告会(平成20年7月10日. 東京大学山上会館)","subitem_description_type":"Other"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Aeroelastic response of the small experimental supersonic transport (NEXST-1) at the 2nd flight experiment was examined. Two accelerometers were equipped on the main wings to monitor those aeroelastic responses. Dampings of the structural modes were obtained by the Random Decrement Technique. Although the damping of the symmetric first wing bending mode slightly reduced while the aircraft passed though the transonic regime, aeroelastic instability was not observed. It seems that the flow separation occurred at about two degrees of angle of attack and it excited the wing vibration. These data are reported in this paper.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0064239009","subitem_description_type":"Other"}]},"item_5_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: JAXA-SP-08-008","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-113X","subitem_source_identifier_type":"ISSN"}]},"item_5_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AA11984031","subitem_source_identifier_type":"NCID"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"宇宙航空研究開発機構"},{"subitem_text_value":"宇宙航空研究開発機構"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"齋藤, 健一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"町田, 茂"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Saito, Kenichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Machida, Shigeru","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":"2020-01-16"}],"displaytype":"detail","filename":"64239009.pdf","filesize":[{"value":"900.2 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"64239009.pdf","url":"https://jaxa.repo.nii.ac.jp/record/5445/files/64239009.pdf"},"version_id":"c42c606b-9066-45ed-a135-6cdc5ee17b73"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Supersonic transport, Flight test, Aeroelasticity","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":"conference paper","resourceuri":"http://purl.org/coar/resource_type/c_5794"}]},"item_title":"小型超音速実験機第2回飛行実験時の空力弾性応答について","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"小型超音速実験機第2回飛行実験時の空力弾性応答について"}]},"item_type_id":"5","owner":"1","path":["965","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"5445","relation_version_is_last":true,"title":["小型超音速実験機第2回飛行実験時の空力弾性応答について"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T08:14:56.046138+00:00"}