Effect of Impinging Wake Turbulence on the Dynamic Stall of a Pitching Airfoil
Author:
Affiliation:
1. Arizona State University, Tempe, Arizona 85287
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J055405
Reference67 articles.
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4. BradyW.LudwigG. “Unsteady Stall of Axial Flow Compressors,” Cornell Aeronautical Lab Inc. Rept. AM-1762-A-1, Buffalo, NY, 1963.
5. Effects of Unsteady Freestream on Aerodynamic Characteristics of a Pitching Delta Wing
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