Hypersonic similarity law, as developed by H.S.TSIEN for bodies of revolution at zero angle of attack, is tested by comparing pressure distributions obtained using method of characteristics; results indicate that, in spite of assumptions made in its development, hypersonic similarity law is valid for relatively wide ranges of Mach number and finenss ratio.
Similarity laws for slender bodies of revolution in hypersonic flows
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 18 , n 8
1951
Aufsatz (Zeitschrift)
Englisch
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Hypersonic minimum-drag slender bodies of revolution
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