Membrane Wing Model for Micro Air Vehicles
Author:
Affiliation:
1. University of Florida, Gainesville, Florida 32611-6250
2. Ecole Centrale de Nantes, 44321 Nantes Cedex 3, France
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.6850
Reference12 articles.
1. Flapping and flexible wings for biological and micro air vehicles
2. Flexible-wing-based micro air vehicles
3. Finite strains and displacements of elastic membranes by the finite element method
4. Numerical analysis of three-dimensional elastic membrane wings
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