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Experimental investigation of combustion mechanisms of kerosene-fueled scramjet engines with double-cavity flameholders
Scramjet Supersonic combustion Flame structure Cavity flameholder
2012/2/28
A scramjet combustor with double cavitybased flameholders was experimentally studied in a directconnected test bed with the inflow conditions of M = 2.64, Pt = 1.84MPa, Tt = 1300 K. Successful ignitio...