Effects of compressibility on dynamic stall
Author:
Affiliation:
1. University of Arizona, Tucson, Arizona 85721
2. 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/10.2514/3.10578
Reference13 articles.
1. Progress in analysis and prediction of dynamic stall
2. 3Dadone, L. U. *Two-Dimensional Wind Tunnel Test of an Oscillating Rotor Airfoil," NASA CR-2914, Dec. 1977.
3. Airfoil dynamic stall at constant pitch rate and high Reynolds number
4. Dynamic Stall on Advanced Airfoil Sections
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