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41st AIAA Fluid Dynamics Conference and Exhibit
An investigation of a pulse detonation combustor applied to a supersonic flow for enhanced mixing was performed both experimentally and numerically. Characterization of the high-pressure and high-temperature plume of the pulse detonation combustor through high-speed shadowgraphy showed significant penetration into the core of the M=2 flow with blow-down times greater than 4 ms. The momentary blockage from the PDC elevated the downstream pressures to between 1.5 and 2 times the static tunneldoi:10.2514/6.2011-3713 fatcat:257icwdx3ff53ajdcjoo377nwa