{"created":"2023-06-20T15:10:25.370036+00:00","id":40003,"links":{},"metadata":{"_buckets":{"deposit":"7f20429a-6564-43d2-9baa-e3f8e5118390"},"_deposit":{"created_by":1,"id":"40003","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"40003"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00040003","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["445955","445952","445953","445954"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Sting supporting system with controllable roll mode"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1997-09","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"22","bibliographicPageStart":"1","bibliographicVolumeNumber":"1335","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"逆対称モードフラッタの特性を把握するために特殊な支持装置を開発した。この支持装置はロール方向に自由度を有しており、その自由度をサーボモータによりコントロールできる機構を持ち、対称モードフラッタとの限界動圧の差を利用したフラッタ停止装置の機能も併せ持つ。航空宇宙技術研究所の遷音速風洞でダミーの全機模型を用いて風洞実験を行った結果、逆対称モードフラッタをクリティカルなモードとして捕らえることができ、さらにフラッタの停止を図ることができ機構の有効性が確認された。また、DPM(Doublet Point Method)を用いて胴体面をも含めて非定常空気力を解析し、逆対称モードフラッタ特性を求めた。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"To address the wing flutter problem, it is important to take into consideration the anti-symmetric mode since it sometimes becomes the most critical mode. For wind tunnel experiments, a peculiar supporting system is made, which allows motion of the model about its roll axis. This system also has a function that can constrain rolling motion to stop anti-symmetric mode flutter. Flutter experiments were conducted in TWT (Transonic Wind Tunnel) at NAL. It was confirmed that anti-symmetric mode flutter occurred at the flutter boundary and that the supporting system worked successfully. Moreover, flutter characteristics were analytically examined by DPM (Doublet Point Method).","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001145000","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-1335","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":"航空宇宙技術研究所 機体部"}]},"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"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"神田, 淳"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"上田, 哲彦"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kanda, Atsushi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ueda, Tetsuhiko","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":"naltr0001335.pdf","filesize":[{"value":"844.2 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr0001335.pdf","url":"https://jaxa.repo.nii.ac.jp/record/40003/files/naltr0001335.pdf"},"version_id":"ce6c8f6e-bd98-462a-abce-b1900e4bb2c3"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"逆対称モードフラッタ","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞試験","subitem_subject_scheme":"Other"},{"subitem_subject":"DPM","subitem_subject_scheme":"Other"},{"subitem_subject":"ダブレットポイント法","subitem_subject_scheme":"Other"},{"subitem_subject":"スティング支持装置","subitem_subject_scheme":"Other"},{"subitem_subject":"ロール制御機構","subitem_subject_scheme":"Other"},{"subitem_subject":"サーボモータ","subitem_subject_scheme":"Other"},{"subitem_subject":"翼フラッタ","subitem_subject_scheme":"Other"},{"subitem_subject":"ローリング運動","subitem_subject_scheme":"Other"},{"subitem_subject":"遷音速風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"全機模型","subitem_subject_scheme":"Other"},{"subitem_subject":"振動実験","subitem_subject_scheme":"Other"},{"subitem_subject":"振動解析","subitem_subject_scheme":"Other"},{"subitem_subject":"フラッタ実験","subitem_subject_scheme":"Other"},{"subitem_subject":"フラッタ解析","subitem_subject_scheme":"Other"},{"subitem_subject":"anti symmetric mode flutter","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"DPM","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"doublet point method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"sting supporting system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"roll control mechanism","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"servomotor","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wing flutter","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"rolling motion","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transonic wind tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"airframe full scale model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"vibration experiment","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"vibration analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flutter experiment","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flutter analysis","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":"ロール自由度制御機構を有するスティング支持装置","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"ロール自由度制御機構を有するスティング支持装置"}]},"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":"40003","relation_version_is_last":true,"title":["ロール自由度制御機構を有するスティング支持装置"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:17:27.250091+00:00"}