Flow-Separation Lines on Axisymmetric Bodies with Tapered Tails
Author:
Affiliation:
1. Defence Research and Development Canada—Atlantic, Dartmouth, Nova Scotia, B2Y 3Z7, Canada
2. University of New Brunswick, Fredericton, New Brunswick E3A 6S3, Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C031141
Reference24 articles.
1. Effects of vortex separation on the lift distribution on bodies of elliptic cross section
2. Streamlines, vorticity lines, and vortices around three-dimensional bodies
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