Multiscale Vortex Characteristics of Dynamic Stall from Empirical Mode Decomposition-Reference-Cited by-同舟云学术

Multiscale Vortex Characteristics of Dynamic Stall from Empirical Mode Decomposition

Published:2020-02 Issue:2 Volume:58 Page:600-617
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Ansell Phillip J.¹,Mulleners Karen²

Affiliation:

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

2. École Polytechnique Fédérale de Lausanne, 1015 Lausanne, Switzerland

Funder

Schweizerischer Nationalfonds zur Förderung der Wissenschaftlichen Forschung

Air Force Office of Scientific Research

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/am-pdf/10.2514/1.J057800

Reference83 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 a NACA 0012 Airfoil,” NASA TP-1100, 1978.

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

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