Experimental studies of separated flows at hypersonic speeds. I - Separated flows over axisymmetric spiked bodies.
Author:
Affiliation:
1. Cornell Aeronautical Laboratory, Inc., Buffalo, N. Y.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference20 articles.
1. Crawford, D. H. "Investigation of the flow over a spikednose hemisphere-cylinder at a Mach number of 6.8,"NASA TND-118(1959).
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