{"created":"2023-06-20T15:10:04.598178+00:00","id":39670,"links":{},"metadata":{"_buckets":{"deposit":"38747c93-d37e-49f2-bf46-f46183c96194"},"_deposit":{"created_by":1,"id":"39670","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"39670"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00039670","sets":["1887:1893","1896:1898:1913:1916"]},"author_link":["443790","443803","443804","443793","443792","443797","443800","443801","443799","443798","443795","443791","443802","443794","443796","443805"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Performance test of flutter emergency stopper for transonic wind tunnel. Part 1: Effect of half model cart device"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1994-11","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"17","bibliographicPageStart":"1","bibliographicVolumeNumber":"668","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":"2m×2m遷音速風洞で空力弾性風洞試験を行うため、フラッタを緊急に停止する装置を開発、設計および製作し、半截模型用カートに設置した。この装置は、遷音速フラッタを有効に停止させることが判明したので、装置の概要、試験および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":"This paper describes the experimental results on the effectiveness of a flutter emergency stopper for the NAL 2 m x 2 m Transonic Wind Tunnel. The stopper consists of a rising porous plate on the lower wall of the half model cart and an actuator using an air cylinder. Two rising plates were used for evaluation of the stopper. It was concluded that the larger stopper should be employed in the model cart due to its greater effectiveness.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0000090000","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-668","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 空力性能部"},{"subitem_text_value":"航空宇宙技術研究所 空力性能部"},{"subitem_text_value":"航空宇宙技術研究所 空力性能部"},{"subitem_text_value":"航空宇宙技術研究所 空力性能部"},{"subitem_text_value":"航空宇宙技術研究所 空力性能部"},{"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 空力性能部"},{"subitem_text_value":"航空宇宙技術研究所 新型航空機研究グループ"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aircraft Aerodynamic Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aircraft Aerodynamic Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aircraft Aerodynamic Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aircraft Aerodynamic Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aircraft Aerodynamic Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Airframe Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aircraft Aerodynamic Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Advanced Aircraft Research Group"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"鈴木, 弘一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"細江, 信幸"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"飯島, 由美"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"小松, 行夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"国益, 徹也"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"安藤, 泰勝"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"半沢, 麻雄"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"鈴木, 誠三"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Suzuki, Koichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hosoe, Nobuyuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Iijima, Yoshimi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Komatsu, Yukio","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kunimasu, Tetsuya","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ando, Yasukatsu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hanzawa, Asao","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Suzuki, Seizo","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":"naltm00668.pdf","filesize":[{"value":"1.7 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltm00668.pdf","url":"https://jaxa.repo.nii.ac.jp/record/39670/files/naltm00668.pdf"},"version_id":"7eaefc53-e807-4eca-bbb0-db1dbde169c1"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"フラッタ抑制装置","subitem_subject_scheme":"Other"},{"subitem_subject":"緊急停止装置","subitem_subject_scheme":"Other"},{"subitem_subject":"遷音速風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"フラッタ制御試験","subitem_subject_scheme":"Other"},{"subitem_subject":"空力弾性","subitem_subject_scheme":"Other"},{"subitem_subject":"半截模型カート","subitem_subject_scheme":"Other"},{"subitem_subject":"アクティブ制御","subitem_subject_scheme":"Other"},{"subitem_subject":"突風荷重","subitem_subject_scheme":"Other"},{"subitem_subject":"翼形","subitem_subject_scheme":"Other"},{"subitem_subject":"ターンテーブル","subitem_subject_scheme":"Other"},{"subitem_subject":"空気圧シリンダ","subitem_subject_scheme":"Other"},{"subitem_subject":"空力設計","subitem_subject_scheme":"Other"},{"subitem_subject":"制御手順","subitem_subject_scheme":"Other"},{"subitem_subject":"flutter","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"emergency stopper","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transonic wind tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flutter control test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aeroelasticity","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"half model cart","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"active control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"gust load","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wing profile","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"turntable","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"pneumatic cylinder","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"control scheme","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 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