Orthogonal Blade-Vortex Interaction on a Helicopter Tail Rotor
Author:
Affiliation:
1. University of Manchester, Manchester, England M60 1QD, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.32690
Reference34 articles.
1. Effects of Perpendicular Blade-Vortex Interaction, Part 1: Turbulence Structure and Development
2. Effects of Perpendicular Blade-Vortex Interaction, Part 2: Parameter Study
3. Aerodynamic Interactions Between a Rotor and a Fuselage in Forward Flight
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