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
01.01.1978
Report
Keine Angabe
Englisch
Oblique Detonation Wave Ramjet
NTIS | 1980
|Oblique detonation wave ramjet
NTRS | 1980
|Evaluation of the Oblique Detonation Wave Ramjet
NTIS | 1978
|