A feasibility study of a post-buckled beam for actuating helicopter trailing edge flap

Author:

Mallick Rajnish,Ganguli Ranjan,Bhat M. Seetharama

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,Computational Mechanics

Reference6 articles.

1. Lee T., Chopra I.: Design of piezostack-driven trailing-edge flap actuator for helicopter rotors. Smart Mater. Struct. 10, 15–24 (2001)

2. Kim J.-S., Wang K.W., Smith E.C.: Synthesis and control of piezoelectric resonant actuation systems with buckling-beam motion amplifier. AIAA J. 46, 787–791 (2007)

3. Jiang J., Mockensturm E.: A motion amplifier using an axially driven buckling beam I: design and experiments. Nonlinear Dyn. 43, 391–409 (2006)

4. Mallick, R., Ganguli, R., Bhat, M.S.: An innovative motion amplification mechanism using nonlinear buckling vibrations of a post-buckled beam for helicopter trailing edge flap actuation. In: 3rd Asian Conference on Mechanics of Functional Materials and Structures, New Delhi, India, 5th–8th December (2012)

5. Mallick, R., Ganguli, R., Bhat, M.S.: Nonlinear dynamics of a post-buckled beam for actuating helicopter trailing edge flap. In: 69th Annual Forum of the American Helicopter Society, Phoenix, Arizona, USA, May 21–23 (2013)

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