Numerical investigation and optimization on the micro-ramp vortex generator within scramjet combustors with the transverse hydrogen jet
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DOI: 10.1016/j.ast.2018.11.011
Abstract: Abstract An effective fuel supply strategy with high mixing efficiency, large penetration depth and low stagnation pressure losses determines the overall performance of the scramjet (supersonic combustion ramjet) engine. In this paper, the transverse hydrogen… read more here.
Keywords: scramjet; transverse hydrogen; micro; micro ramp ... See more keywords