Flutter control based on ultrasonic motor for a two-dimensional airfoil section

Author:

Yu Mingli,Hu Haiyan

Publisher

Elsevier BV

Subject

Mechanical Engineering

Reference23 articles.

1. An investigation into the effects of unsteady parameters on the aerodynamics of a low Reynolds number pitching airfoil;Amiralaei;Journal of Fluids and Structures,2010

2. Ardelean, E.V., et al., 2003. Flutter suppression using V-stack piezoelectric actuator. In: Proceedings of the 44th AIAA/ASME/ASCE/AHS Structures, Structural Dynamics, and Materials Conference, April 2003, Norfolk, Virginia, AIAA 2003-1796.

3. Active wing flutter suppression using a trailing edge flap;Borglund;Journal of Fluids and Structures,2002

4. Derham, R., Weems, D., Mathew, M.B., et al., 2001. The design evolution of an active materials rotor. In: Proceedings of the American Helicopter Society 57th Annual Forum, Washington, DC.

5. Dancila, D.S., Armanios, E.A., 1998. Large displacement piezoelectric actuator configurations. In: Proceedings of the Adaptive Structures and Material Systems Symposium at the International Mechanical Engineering Congress and Exposition, Winter Annual Meeting of the ASME, Anaheim, pp. 83–87.

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