Performance of ramjet having detonation wave combustion process; flight speeds from Mach 2.5 to 10 are examined and thermodynamic property changes presented; engine cycle performance characteristics are computed including air specific impulse, specific fuel consumption and thermal efficiency; subsonic burning ramjet is shown to have superior performance compared to detonation wave engine; differences and some design features.
Detonation wave hypersonic ramjet
ARS -- J
ARS Journal ; 30 , n 6
1960
7 pages
Aufsatz (Zeitschrift)
Englisch
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Hypersonic ramjet using normal detonation wave
Engineering Index Backfile | 1960
|Oblique detonation wave ramjet
NTRS | 1980
|