Understanding Abrupt Wing Stall with Computational Fluid Dynamics.

Author:

Woodson S. H.1,Green B. E.1,Chung J. J.1,Grove D. V.1,Parikh P. C.2,Forsythe J. R.3

Affiliation:

1. U.S. Naval Air Systems Command, Patuxent River, Maryland 20670

2. NASA Langley Research Center, Hampton, Virginia 23681

3. U.S. Air Force Academy, Colorado Springs, Colorado 80840

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

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1. Study on Wing Rock Phenomenon of a Fighter Aircraft Using Free-To-Roll Wind Tunnel Test and Dynamic CFD Method;AIAA Aviation 2019 Forum;2019-06-15

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3. CFD Analysis of a Maneuvering F/A-18E Super Hornet;55th AIAA Aerospace Sciences Meeting;2017-01-05

4. Enhanced multi-fidelity model for flight simulation using global exploration and the Kriging method;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2016-08-06

5. Navier–Stokes predictions of dynamic stability derivatives for air-breathing hypersonic vehicle;Acta Astronautica;2016-01

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