Experimental Characterization of Hydrocarbon-Fueled, Axisymmetric, Scramjet Combustor Flowpaths
Simulating Inlet Distortion Effects in a Direct-Connect Scramjet Combustor
Experimental Study of Cavity-Strut Combustion in Supersonic Flow AIAA Paper
DUAL MODE SCRAMJET COMBUSTOR: ANALYSIS OF TWO CONFIGURATIONS
Optical Measurements at the Combustor Exit of the HIFiRE 2 Ground Test Engine