Modified Unsteady Vortex-Lattice Method to Study Flapping Wings in Hover Flight
Author:
Affiliation:
1. Structures Department, National University of Córdoba, 5000 Córdoba, Argentina
2. Department of Engineering Science and Mechanics (MC 0219), Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24061
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J052262
Reference59 articles.
1. The aerodynamics of hovering insect flight. IV. Aerodynamic mechanisms
2. The three–dimensional leading–edge vortex of a ‘hovering’ model hawkmoth
3. Leading-edge vortices in insect flight
4. Unsteady aerodynamic model of flapping wings
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