{"created":"2023-06-20T15:10:11.895651+00:00","id":39793,"links":{},"metadata":{"_buckets":{"deposit":"45f2f5e0-ac80-4b4e-b102-c74acb1cb29b"},"_deposit":{"created_by":1,"id":"39793","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"39793"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00039793","sets":["1887:1893","1896:1898:1913:1916"]},"author_link":["444431","444441","444435","444428","444429","444430","444436","444438","444437","444427","444432","444439","444426","444433","444434","444440"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Development of a flutter emergency stopper for the supersonic wind tunnel"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1996-05","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"8","bibliographicPageStart":"1","bibliographicVolumeNumber":"693","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_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"航空宇宙技術研究所の吹出式超音速風洞で、フラッタ限界値推定法の研究を風洞試験で実証するに当たり、供試翼の破損を回避して試験データを安全確実に取得するため、超音速フラッタ停止装置を開発し、翼模型出し入れ装置の翼模型取付けブロックに一体化して設置した。この装置を用いることで、超音速フラッタを有効に停止出来ることが判明した。ここでは、超音速フラッタ停止装置の概要、フラッタ抑止効果の機能確認試験およびその結果について報告する。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A new system of a flutter emergency stopper is developed for preventing catastrophic failure of wing models when they burst into flutter during supersonic blowdown in wind tunnel tests. This system is used in the tests of flutter boundary estimation of supersonic delta wings and is found to yield good results. The details of this system with some experimental results are described in this paper.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0000554000","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-693","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 機体部"},{"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 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"},{"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":"National Aerospace Laboratory Airframe Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Airframe Division"},{"subitem_text_language":"en","subitem_text_value":"Nagoya University"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Structural Mechanics Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aerodynamics Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aerodynamics Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aerodynamics Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aerodynamics Division"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"峯岸, 正勝"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"安藤, 泰勝"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"松崎, 雄嗣"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"江尻, 宏"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"野田, 順一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"関根, 英夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"楯, 篤志"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"渡辺, 光則"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Minegishi, Masakatsu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ando, Yasukatsu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Matsuzaki, Yuji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ejiri, Hiroshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Noda, Junichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sekine, Hideo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tate, Atsushi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Watanabe, Mitsunori","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":"naltm00693.pdf","filesize":[{"value":"1.3 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltm00693.pdf","url":"https://jaxa.repo.nii.ac.jp/record/39793/files/naltm00693.pdf"},"version_id":"20e3ba03-6c12-4e31-b227-f72356bf5ecc"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"超音速デルタ翼","subitem_subject_scheme":"Other"},{"subitem_subject":"フラッタ試験","subitem_subject_scheme":"Other"},{"subitem_subject":"フラッタ緊急停止装置","subitem_subject_scheme":"Other"},{"subitem_subject":"吹出式超音速風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速吹出し","subitem_subject_scheme":"Other"},{"subitem_subject":"フラッタ限界値測定","subitem_subject_scheme":"Other"},{"subitem_subject":"フラッタ抑止効果","subitem_subject_scheme":"Other"},{"subitem_subject":"フラッタ振動数","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞試験","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic delta wing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flutter test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flutter emergency stopper","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"blowdown supersonic wind tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic blowdown","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flutter boundary estimation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flutter prevention effect","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flutter vibration frequency","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel test","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":"超音速フラッタ停止装置の開発","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"超音速フラッタ停止装置の開発"}]},"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":"39793","relation_version_is_last":true,"title":["超音速フラッタ停止装置の開発"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:19:15.012404+00:00"}