WEKO3
アイテム
Wind Tunnel Tests on Flutter Control of a High-Aspect-Ratio Cantileverd Wing, 1st Report
https://jaxa.repo.nii.ac.jp/records/45237
https://jaxa.repo.nii.ac.jp/records/4523755b54302-efeb-4f74-b76b-4593598d3965
| 名前 / ファイル | ライセンス | アクション |
|---|---|---|
naltr00978.pdf (6.6 MB)
|
|
| 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 | Wind Tunnel Tests on Flutter Control of a High-Aspect-Ratio Cantileverd Wing, 1st Report | |||||||||
| 言語 | en | |||||||||
| 言語 | ||||||||||
| 言語 | eng | |||||||||
| 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 | ||||||||||
| その他のタイトル | 高アスペクト比翼のフラッタ制御実験(第1報) | |||||||||
| 著者 |
ACT研究会
× ACT研究会
× ACT Study Group
|
|||||||||
| 著者所属 | ||||||||||
| 航空宇宙技術研究所 | ||||||||||
| 著者所属（英） | ||||||||||
| en | ||||||||||
| National Aerospace Laboratory(NAL) | ||||||||||
| 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報告 en : Technical Report of National Aerospace Laboratory TR-978 巻 978, p. 97, 発行日 1988-06 |
|||||||||
| 抄録（英） | ||||||||||
| 内容記述タイプ | Other | |||||||||
| 内容記述 | Wind tunnel test results obtained in the FY85 experiments on flutter control are presented in this paper. The test was conducted in the NAL 5.5×6.5 m Low-speed wind tunnel by the ACT study group. The wing model used in the tests assumes a future type of energy efficient transport. It has two control surfaces, one at the leading edge and the other at the trailing edge. Various control laws based on the LQG theory were implemented and tested with either control surface after reducing the order of the laws. The results showed a prominent effect of the leading edge control surface on flutter suppression. The maximum increase in flutter speed was 9.7％ of the violent bending-torsion flutter. For the test, a special device was installed in the wind tunnel to prevent this highly mechanical model from being destroyed, which enabled us to execute very efficient tests. | |||||||||
| ISSN | ||||||||||
| 収録物識別子タイプ | ISSN | |||||||||
| 収録物識別子 | 0389-4010 | |||||||||
| 資料番号 | ||||||||||
| 内容記述タイプ | Other | |||||||||
| 内容記述 | 資料番号: NALTR0978000 | |||||||||
| 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 TR-978 | |||||||||
