Basic Understanding of Airfoil Characteristics at Low Reynolds Numbers (104–105)
Author:
Affiliation:
1. University of Maryland, College Park, Maryland 20742
Funder
US Army/US Navy/NASA Vertical Lift Research Center of Excellence
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C034415
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3. AERODYNAMICS OF SMALL VEHICLES
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