Aerodynamics of Airfoils at High and Reverse Angles of Attack
Author:
Affiliation:
1. Georgia Institute of Technology, Atlanta, Georgia 30332-0150
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C031428
Reference32 articles.
1. Estimating the angle of attack from blade pressure measurements on the NREL Phase VI rotor using a free wake vortex model:axial conditions
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