Laminar boundary layers on slender paraboloids.
Author:
Affiliation:
1. Douglas Aircraft Company, McDonnell Douglas Corporation, Long Beach, Calif.
2. University of Michigan, Dearborn, Mich.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference5 articles.
1. Davies, L. "The Interaction of the Reflected Shock With the Boundary Layer in a Shock Tube and Its Influence on the Duration of Hot Flow in the Reflected Shock Tunnel," 27 110-Hyp505, 1965, Aeronautical Research Council, Great Britain.
2. Boundary Layer over a Thin Needle
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