Two conceptual designs of the oblique detonation wave ramjet are presented. The performance is evaluated for stoichiometric hydrogen-air equivalence ratios of phi = 1/3, 2/3 and 1 for a range of flight Mach numbers from 6 to 10.
Oblique detonation wave ramjet
1980-01-01
Report
No indication
English
Oblique Detonation Wave Ramjet
NTIS | 1980
|Evaluation of the oblique detonation wave ramjet
NTRS | 1978
|Evaluation of the Oblique Detonation Wave Ramjet
NTIS | 1978
|