A “Preview” of Three-Dimensional Shock-Wave/ Turbulent Boundary-Layer Interactions

The interaction of a shock wave with a turbulent boundary layer can drastically change aerodynamic loads, alter combustion processes, and produce intense local heating, buffeting, and loss of control. Shock-wave/ boundary-layer interactions have therefore been the subject of extensive research. For the two-dimensional case, numerous mean flow data sets exist, over a wide range of Mach and Reynolds numbers, and for a number of flows detailed turbulence measurements have become available. Recently, the unsteady nature of many two-dimensional interactions has also received considerable attention.

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