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...
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| Main Authors: | , , , |
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| 格式: | Conference or Workshop Item |
| 出版: |
2013
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| 主題: | |
| 在線閱讀: | http://eprints.utm.my/id/eprint/50954/ http://dx.doi.org/10.4028/www.scientific.net/AMM.390.3 |
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