Dynamic Stall on Pitching Cambered Airfoil with Phase Offset Trailing Edge Flap-Reference-Cited by-同舟云学术

Dynamic Stall on Pitching Cambered Airfoil with Phase Offset Trailing Edge Flap

Published:2020-07 Issue:7 Volume:58 Page:2844-2856
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Samara Farid¹,Johnson David A.¹

Affiliation:

1. University of Waterloo, Waterloo, Ontario N2L 3G1 Canada

Funder

Natural Sciences and Engineering Research Council of Canada

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference46 articles.

1. Review of state of the art in smart rotor control research for wind turbines

2. CarrL. W.McAlisterK. W.McCroskeyW. J. “Analysis of the Development of Dynamic Stall Based on Oscillating Airfoil Experiments,” NASA TN D-8382, 1977, pp. 59–64.

3. Unsteady Airfoils

4. Dynamic Stall in Pitching Airfoils: Aerodynamic Damping and Compressibility Effects

5. Dynamic stall experiments on the NACA 23012 aerofoil

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