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遷音速風洞フラッタ緊急停止装置性能試験 その1:半截模型カート用装置の効果
https://jaxa.repo.nii.ac.jp/records/39670
https://jaxa.repo.nii.ac.jp/records/39670b7a7a405-f5ea-42b2-86bd-a092cb2bddc2
名前 / ファイル | ライセンス | アクション |
---|---|---|
naltm00668.pdf (1.7 MB)
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|
Item type | テクニカルレポート / Technical Report(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 遷音速風洞フラッタ緊急停止装置性能試験 その1:半截模型カート用装置の効果 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | フラッタ抑制装置 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 緊急停止装置 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 遷音速風洞 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | フラッタ制御試験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 空力弾性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 半截模型カート | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | アクティブ制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 突風荷重 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 翼形 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ターンテーブル | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 空気圧シリンダ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 空力設計 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 制御手順 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flutter | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | emergency stopper | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | transonic wind tunnel | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flutter control test | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aeroelasticity | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | half model cart | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | active control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | gust load | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wing profile | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | turntable | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | pneumatic cylinder | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aerodynamic design | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | control scheme | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_18gh | |||||
資源タイプ | technical report | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Performance test of flutter emergency stopper for transonic wind tunnel. Part 1: Effect of half model cart device | |||||
著者 |
鈴木, 弘一
× 鈴木, 弘一× 細江, 信幸× 飯島, 由美× 小松, 行夫× 国益, 徹也× 安藤, 泰勝× 半沢, 麻雄× 鈴木, 誠三× Suzuki, Koichi× Hosoe, Nobuyuki× Iijima, Yoshimi× Komatsu, Yukio× Kunimasu, Tetsuya× Ando, Yasukatsu× Hanzawa, Asao× Suzuki, Seizo |
|||||
著者所属 | ||||||
航空宇宙技術研究所 空力性能部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 空力性能部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 空力性能部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 空力性能部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 空力性能部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 機体部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 空力性能部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 新型航空機研究グループ | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Aircraft Aerodynamic Division | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Aircraft Aerodynamic Division | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Aircraft Aerodynamic Division | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Aircraft Aerodynamic Division | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Aircraft Aerodynamic Division | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Airframe Division | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Aircraft Aerodynamic Division | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Advanced Aircraft Research Group | ||||||
出版者 | ||||||
出版者 | 航空宇宙技術研究所 | |||||
出版者(英) | ||||||
出版者 | National Aerospace Laboratory (NAL) | |||||
書誌情報 |
航空宇宙技術研究所資料 en : Technical Memorandum of National Aerospace Laboratory 巻 668, p. 1-17, 発行日 1994-11 |
|||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 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。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 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. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0452-2982 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN00314334 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0000090000 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: NAL TM-668 |