NASA NTRS · 19800005874
Oblique detonation wave ramjet
Abstract
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.
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Morrison, R. B.. 1980-01-01. Oblique detonation wave ramjet. https://ntrs.nasa.gov/citations/19800005874
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