Analysis and Design of a Flap-Equipped Low-Twist Rotor for Hover
Author:
Affiliation:
1. Glasgow University, Glasgow, Scotland G12 8QQ, United Kingdom
2. Liverpool University, Liverpool, England L69_3GH, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.34275
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5. Caradonna, F. X, and Tung. C. "A Review of Current Finite Difference Rotor Flow Methods," 42nd Annual Forum,AHSInternational, Alexandria,VA, June 1986, pp.967-983.
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