Unsteady aerodynamic and stall effects on helicopter rotor blade airfoil sections.
Author:
Affiliation:
1. The Boeing Company, Verlol Division, Philadelphia, Pa.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.44000
Reference10 articles.
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