Active aeroelastic control of 2-D wing-flap systems operating in an incompressible flowfield and impacted by a blast pulse

Author:

Librescu Liviu,Na Sungsoo,Marzocca Piergiovanni,Chung Chanhoon,Kwak Moon K.

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Acoustics and Ultrasonics,Condensed Matter Physics

Reference29 articles.

1. Aeroelastic response of a 2-D lifting surfaces to gust and arbitrary explosive loading signatures;Marzocca;International Journal of Impact Engineering,2001

2. P. Marzocca, L. Librescu, G. Chiocchia, Aeroelasticity of two-dimensional lifting surfaces via indicial function approach, The Aeronautical Journal 106 (2002) 147–153.

3. An elementary explanation of the flutter mechanism with active feedback controls;Horikawa;Journal of Aircraft,1979

4. Investigation of the experimental active control of a typical section airfoil using a trailing edge flap;Vipperman;Journal of Aircraft,1998

5. Fundamental mechanisms of aeroelastic control with control surface and strain actuation;Lazaraus;Journal of Guidance, Control, and Dynamics,1995

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