Challenges in Understanding the Vortex Dynamics of Helicopter Rotor Wakes
Author:
Affiliation:
1. University of Maryland, College Park, Maryland 20742
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.510
Reference101 articles.
1. Helicopter impulsive noise: Theoretical and experimental status
2. Aerodynamic Interactions Between a Rotor and a Fuselage in Forward Flight
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