Wind tunnel tests of a hydrogen-fueled detonation ramjet model at approach air stream Mach numbers from 4 to 8
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DOI: 10.1016/j.ijhydene.2017.08.062
Abstract: Abstract Experimental studies of an axisymmetric hydrogen-fueled detonation ramjet model 1.05-m long and 0.31 m in diameter with an expanding annular combustor were performed in a pulse wind tunnel under conditions of approaching air stream Mach… read more here.
Keywords: detonation ramjet; air; hydrogen fueled; fueled detonation ... See more keywords