Measurements of supersonic wing tip vortices
Author:
Affiliation:
1. Polytechnic University, Brooklyn, New York 11201
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.12725
Reference24 articles.
1. Airfoil pressure measurements during oblique shock-wave/vortex interaction in a Mach 3 stream
2. The effect of shock strength on oblique shock wave-vortex interaction
3. Structure of trailing vortices.
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