Active Control of Nonlinear Panel Flutter Using Aeroelastic Modes and Piezoelectric Actuators
โ Scribed by Kim, M.; Li, Q.; Huang, J.-K.; Mei, C.
- Book ID
- 118035066
- Publisher
- American Institute of Aeronautics and Astronautics
- Year
- 2008
- Tongue
- English
- Weight
- 664 KB
- Volume
- 46
- Category
- Article
- ISSN
- 0001-1452
- DOI
- 10.2514/1.33803
No coin nor oath required. For personal study only.
๐ SIMILAR VOLUMES
The active flutter suppression is considered of a cantilever tube transporting high speed moving fluid by using state of the art piezoelectric ceramics as the actuators. Bernoulli-Euler beam theory is applied for the long slender cantilever tube which is discretized into finite elements to describe
This paper presents a numerical and experimental investigation on active flutter suppression of a sweptback cantilevered lifting surface using piezoelectric (PZT) actuation. A finite element method, a panel aerodynamic method, and the minimum state-space realization are involved in the development o