Performance Analysis of a Flapping-Wing Vehicle Based on Experimental Aerodynamic Data-Reference-Cited by-同舟云学术

Performance Analysis of a Flapping-Wing Vehicle Based on Experimental Aerodynamic Data

Published:2012-01 Issue:1 Volume:25 Page:45-50
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Mazaheri K.¹²³,Ebrahimi A.¹²³,Karimian S.¹²³

Affiliation:

1. Professor, Dept. of Aerospace Engineering, Aerospace Systems Center of Excellence, Sharif Univ. of Technology, Tehran, Iran.

2. Dept. of Aerospace Engineering, Aerospace Systems Center of Excellence, Sharif Univ. of Technology, Tehran, Iran (corresponding author).

3. Ph.D. Candidate, Dept. of Aerospace Engineering, Aerospace Systems Center of Excellence, Sharif Univ. of Technology, Tehran, Iran.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000102

Reference23 articles.

1. Ames R. (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 Atlanta.

2. Object-Oriented Unsteady Vortex Lattice Method for Flapping Flight

3. An Experimental Study of Flapping Membrane Wings

4. Gebert G. Gallmeier P. and Evers J. (2002). “Equations of motion for flapping flight.” AIAA Atmospheric Flight Mechanics Conf. Monterey CA.

5. Ho S. (2003). “Unsteady aerodynamics and adaptive flow control of micro air vehicles.” Ph.D. thesis Univ. of California Berkeley CA.

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