Determination of relative performance for two cases where each system employs isentropic spike external compression inlet and internal compression inlet; results indicate that specific impulse of supersonic ramjet will be superior to that of subsonic ramjet at Mach numbers above approximately 7 for configurations having isentropic spike external compression inlets and above 10 for those having internal compression inlets.
Relative thermodynamic efficiency of supersonic combustion and subsonic combustion hypersonic ramjets
ARS -- J
ARS Journal ; 30 , n 11
1960
3 pages
Aufsatz (Zeitschrift)
Englisch
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