Numerical investigation of dynamic stall of an oscillating wing
Author:
Affiliation:
1. NASA Ames Research Center, Moffett Field, California 94035
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.12730
Reference35 articles.
1. Viscous-Inviscid Interaction on Oscillating Airfoils in Subsonic Flow
2. Progress in analysis and prediction of dynamic stall
3. An experimental investigation of an airfoil undergoing large-amplitude pitching motions
4. Propulsive vortical signature of plunging and pitching airfoils
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