Two methods for calculating the velocities induced by a constant diameter far-wake
Author:
Affiliation:
1. University of Newcastle, Newcastle, New South Wales, 2308, Australia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.46058
Reference14 articles.
1. The Wake Geometry of a Hovering Helicopter Rotor and Its Influence on Rotor Performance
2. Marine Propellers
3. Calculation of steady flow about propellers using a surface panel method
4. Three-dimensional calculation of windmill surface pressures
5. A Simplified Free Wake Method for Horizontal-Axis Wind Turbine Performance Prediction
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1. Free-Vortex Filament Methods for the Analysis of Helicopter Rotor Wakes;Journal of Aircraft;2002-09
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