Investigation of Combustion Structure and Flame Stabilization in an Axisymmetric Scramjet
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DOI: 10.2514/1.j062192
Abstract: The combustion characteristics and flame stabilization mechanisms in an axisymmetric scramjet with a high-enthalpy inflow are investigated numerically in this paper. To consider the strong compressibility induced by the high Mach number, a pressure-related flamelet/progress… read more here.
Keywords: combustion; flame stabilization; axisymmetric scramjet; structure ... See more keywords