Flexible Flapping Airfoil Propulsion at Zero Freestream Velocity
Author:
Affiliation:
1. University of Bath, Bath, England BA2 7AY, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.5299
Reference20 articles.
1. Technical Aspects of Microscale Flight Systems
2. Vortical patterns in the wake of an oscillating airfoil
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