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Physics of unsteady cylinder-induced transitional shock wave boundary layer interactionsMurphree, Zachary Ryan 27 May 2010 (has links)
The mean flowfield and time-dependent characteristics of a Mach 5 cylinder-induced transitional shock-wave/boundary-layer interaction have been studied experimentally. The objectives of the study were to: (i) provide a detailed description of the mean flow structure of the interaction, and (ii) characterize the unsteadiness of the interaction based on fluctuating pressure measurements. / text
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