Approximate evaluation of slender radome performance in hypersonic flight
Author:
Affiliation:
1. Hughes Aircraft Company, El Segundo, Calif
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.2351
Reference13 articles.
1. Deissler, R G and Loeffler, A L , Jr , "Analysis of turbulent flow and heat transfer on a flat plate at high Mach numbers with variable fluid properties,;NASA TR R-17 (1959)
2. THEORY OF ENTROPY LAYERS AND NOSE BLUNTNESS IN HYPERSONIC FLOW
3. February 1962;Seiff A
4. November 1961;Witliff C E
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