Physics of unsteady cylinder-induced transitional shock wave boundary layer interactions

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Date

2009-12

Authors

Murphree, Zachary Ryan

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Abstract

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.

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