Optimization of Flapping Airfoils For Maximum Thrust and Propulsive Efficiency
Author:
Affiliation:
1. Middle East Technical University, 06531 Ankara, Turkey
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.816
Reference20 articles.
1. Fixed and Flapping Wing Aerodynamics for Micro Air Vehicle Applications
2. Flapping and flexible wings for biological and micro air vehicles
3. Jet Characteristics of a Plunging Airfoil
4. Experimental and Computational Investigation of the Knoller-Betz Effect
5. Oscillating foils of high propulsive efficiency
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