The potential performance of oblique detonation wave ramjets is analyzed in terms of multishock diffusion, oblique detonation waves, and heat release. Results are presented in terms of thrust coefficients and specific impulses for a range of flight Mach numbers of 6 to 16.
Evaluation of the oblique detonation wave ramjet
1978-01-01
Report
No indication
English
Oblique detonation wave ramjet
NTRS | 1980
|Oblique Detonation Wave Ramjet
NTIS | 1980
|Evaluation of the Oblique Detonation Wave Ramjet
NTIS | 1978
|