Composite wing flutter speed and frequency due to variable control surface deflection in low speed wind tunnel
Flutter is a dynamic instability problem represents the interaction among structural, aerodynamic, elastic and inertial forces and occurred when the energy is continuously transformed by the surrounding fluids to a flying structure in the form of kinetic energy. The study was conducted to investigat...
保存先:
| 主要な著者: | , , , |
|---|---|
| フォーマット: | Conference or Workshop Item |
| 出版事項: |
2013
|
| 主題: | |
| オンライン･アクセス: | http://eprints.utm.my/id/eprint/50954/ http://dx.doi.org/10.4028/www.scientific.net/AMM.390.3 |
| タグ: |
タグ追加
タグなし, このレコードへの初めてのタグを付けませんか!
|