Separated flow about lifting bodies and impulsive flow about cylinders.
Author:
Affiliation:
1. University of Nebraska, Lincoln, Neb.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.3453
Reference24 articles.
1. Investigation of Normal Force Distributions and Wake Vortex Characteristics of Bodies of Revolution at Supersonic Speeds
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