Experimental and Computational Analysis of Rigid Flapping Wings for Micro Air Vehicles-Reference-Cited by-同舟云学术

Experimental and Computational Analysis of Rigid Flapping Wings for Micro Air Vehicles

Published:2015-07 Issue:4 Volume:52 Page:1161-1178
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Mayo David B.¹,Lankford James L.¹,Benedict Moble¹,Chopra Inderjit¹

Affiliation:

1. Department of Aerospace Engineering, University of Maryland, College Park, Maryland 20742

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C032853

Reference52 articles.

1. Progress in Astronautics and Aeronautics;Azuma A.,2001

2. AERODYNAMICS OF SMALL VEHICLES

3. OlM. V. “Unsteady Aerodynamics for Micro Air Vehicles,” Final Report of Task Group AVT-149, NATO Research and Technology Organization, TR-AC/323 (AVT-149) TP/332, Brussels, 2010.

4. Aerodynamics of Low Reynolds Number Flyers

5. LeishmanJ. G., Principles of Helicopter Aerodynamics, 2nd ed., Cambridge Univ. Press, Cambridge, England, U.K., 2006, pp. 334–337.

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