Flow Evolution and Unsteady Spectra of Dynamic Stall at Transitional Reynolds Numbers-Reference-Cited by-同舟云学术

Flow Evolution and Unsteady Spectra of Dynamic Stall at Transitional Reynolds Numbers

Published:2020-08 Issue:8 Volume:58 Page:3272-3285
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Gupta Rohit¹,Ansell Phillip J.¹

Affiliation:

1. University of Illinois at Urbana–Champaign, Urbana, Illinois 61801

Funder

U.S. Air Force Office of Scientific Research

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference45 articles.

1. Aerodynamic loading on a two-dimensional airfoil during dynamic stall.

2. Dynamic Stall Experiments on Oscillating Airfoils

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

4. McAlisterK. W.CarrL. W.McCroskeyW. J. “Dynamic Stall Experiments on the NACA 0012 Airfoil,” NASA TP-1100, 1978.

5. McCroskeyW. J. “The Phenomenon of Dynamic Stall,” NASA TM-81264, 1981.

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