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48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition
A magnetically driven DC surface plasma discharge has shown promise for supersonic boundary layer control. Previous experiments in supersonic flow performed using this plasma actuator have shown significant control over the shockwaveturbulent boundary layer interaction region. In this study, the velocity of the surface jet in quiescent air is measured and compared with predictions. A time gated schlieren technique is used to visualize the jet and determine the velocity. The surface plasmadoi:10.2514/6.2010-831 fatcat:dj5mvnfuszfgbfeztsrewajwaq