Numerical Investigation of Subsonic and Supersonic Asymmetric Vortical Flow
Author:
Affiliation:
1. Wright Laboratory, Armament Directorate, Eglin Air Force Base, Florida 32542
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.11789
Reference8 articles.
1. Asymmetric separated flows at supersonic speeds
2. 4Vanden, K. J. "Thin-Layer Navier-Stokes Solutions of the Asymmetric Vortical Flow on a Tangent Ogive Body," M.S. Thesis,Univ. of Florida, Gainsville, FL, 1989.
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