Circular Scramjet Combustor Transition Lengths at Mach 8 and 12.8 Flight Conditions
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DOI: 10.2514/1.j059177
Abstract: This paper presents an experimental study of laminar-to-turbulent boundary-layer transition in a circular duct at high supersonic Mach number. The experiments were conducted as an essential precurs... read more here.
Keywords: transition; combustor transition; transition lengths; circular scramjet ... See more keywords