Control of Rotorcraft Retreating Blade Stall Using Air-Jet Vortex Generators
Author:
Affiliation:
1. City University, London, England EC1V 0HB, United Kingdom
2. University of Glasgow, Glasgow, Scotland G128QQ, United Kingdom
3. University of Glasgow, London, England EC1V 0HB, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.18333
Reference28 articles.
1. Dynamic stall control for advanced rotorcraft application
2. Performance enhancement evaluation of an actuated trailing edge flap
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