Aerofoil-Vortex Interaction Using the Compressible Vorticity Confinement Method
Author:
Affiliation:
1. University of Glasgow, Glasgow, Scotland G12 8QQ, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.5177
Reference42 articles.
1. Experimental observations of two-dimensional blade-vortex interaction
2. Flight-Path Management/Control Methodology to Reduce Helicopter Blade-Vortex Interaction Noise
3. Twenty-five years of rotorcraft aeroacoustics: Historical prospective and important issues
4. Helicopter impulsive noise: Theoretical and experimental status
5. Implicit time-stepping methods for the Navier-Stokes equations
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