Numerical Investigation of a Cylinder Immersed in a Supersonic Boundary Layer-Reference-Cited by-同舟云学术

Numerical Investigation of a Cylinder Immersed in a Supersonic Boundary Layer

Published:2012-02 Issue:2 Volume:50 Page:257-270
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Dudley Jonathan G.¹,Ukeiley Lawrence²

Affiliation:

1. U.S. Air Force Research Laboratory, Eglin Air Force Base, Florida 32542

2. University of Florida, Shalimar, Florida 32579

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J050647

Reference29 articles.

1. Vortex Shedding from Smooth and Roughened Cylinders in Cross-Flow near a Plane Surface

2. Götkun, S. "The Drag and Lift Coefficients of a Cylinder Placed Near a Plane Surface," M.S. Thesis,U.S. Naval Postgraduate School, Monterey, CA, 1975.

3. Flow around a circular cylinder near a plane boundary

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