Comparison of Laminar Separation Bubble Measurements on a Low Reynolds Number Airfoil in Three Facilities
Author:
Affiliation:
1. U.S. Air Force Reseach Laboratory
2. Carleton University
3. Institute for Aerospace Research/NRC
4. Technical University at Braunschweig
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2005-5149
Reference29 articles.
1. Flapping and flexible wings for biological and micro air vehicles
2. Shape Memory Alloy Actuators as Locomotor Muscles
3. Membrane wing aerodynamics for micro air vehicles
4. Aerohydrodynamics of flapping-wing propulsors
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