Tailoring Flapping Wings to Facilitate Desired Deformed Shapes
Author:
Affiliation:
1. Department of Mechanical and Aerospace Engineering, University of Florida, Gainesville, Florida 32611
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J052298
Reference9 articles.
1. StanfordB.BeranP.KobayashiM. “Aeroelastic Optimization of Flapping Wing Venation: A Cellular Division Approach,” AIAA Paper 2011-2094, 2011.
2. Shape, Structure, and Kinematic Parameterization of a Power-Optimal Hovering Wing
3. AonoH.ChimakurthiS. K.WuP.SällströmE.StanfordB. K.CesnikC. E. S.IfjuP.LawrenceU.ShyyW. “A Computational and Experimental Study of Flexible Flapping Wing Aerodynamics,” AIAA Paper 2010-554, 2010.
4. Insect-Based Hover-Capable Flapping Wings for Micro Air Vehicles: Experiments and Analysis
5. Study of Biologically Inspired Flapping Mechanism for Micro Air Vehicles
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