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The spark ignition process in the scramjet combustor fueled by hydrogen equipped with multi-cavities at Mach 4 flight condition was observed by high speed photography and Schlieren system, at the inflow conditions of Ma=1.92 with stagnation state T 0 =846K, P 0 =0.7MPa. The spark kernel, the flame spreading process and shock structures in the combustor with different ignition and injection...
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