Experimental investigation of the effect of chordwise flexibility on the aerodynamics of flapping wings in hovering flight

Author:

Mazaheri K.,Ebrahimi A.

Publisher

Elsevier BV

Subject

Mechanical Engineering

Reference31 articles.

1. Ames, R.G., 2001. On the flowfield and forces generated by a rectangular wing undergoing moderate reduced frequency flapping at low Reynolds number. Ph.D. Thesis, Georgia Institute of Technology.

2. Bilyk, D.J., 2000. The development of flapping wings for a hovering micro air vehicle. Masters of Applied Science Thesis, University of Toronto.

3. Bruce, N., 1997. Micro air vehicles hold great promise. Challenges, Aviation Week & Space Technology, 14 April 1997, 67–68.

4. Into thin air: contributions of aerodynamic and inertial-elastic forces to wing bending in the hawkmoth manduca sexta;Combes;The Journal of Experimental Biology,2003

5. Flexing wings and fins: bending by inertial or fluid dynamic forces?;Daniel;Integrative and Comparative Biology,2002

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