Thrust imparted to an airfoil by passage through a sinusoidal upwashfield
Author:
Affiliation:
1. University of Toronto, Downsview, Ontario M3H 5T6, Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.11860
Reference20 articles.
1. Propulsive effects due to flight through turbulence
2. Some Aspects of Non-Stationary Airfoil Theory and Its Practical Application
3. Airfoil Theory for Non-Uniform Motion
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2. Unsteady Leading-Edge Suction Effects on Rotor-Stator Interaction Noise;AIAA Journal;2000-09
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4. Numerical Simulation of Flowfield Around Airfoil with Stationary or Oscillating Spoiler;Journal of Aircraft;1998-09
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