Three-Dimensional Separation for Interaction of Shock Waves with Turbulent Boundary Layers
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For the interaction of shock waves with turbulent boundary layers, obtained experimental three-dimensional separation results and correlations with earlier two-dimensional and three-dimensional data are presented. It is shown that separation occurs much earlier for turbulent three-dimensional than for two-dimensional flow at hypersonic speeds.
[1] A. McCabe,et al. The Three-Dimensional Interaction of a Shock Wave with a Turbulent Boundary Layer , 1966 .
[2] M. Holden,et al. Shock Wave Turbulent Boundary Layer Interaction in Hypersonic Flow , 1972 .
[3] Francis C. Moon,et al. Wave Surfaces Due to Impact on Anisotropic Plates , 1972 .
[4] K. Wang,et al. Separation Patterns of Boundary Layer over an Inclined Body of Revolution , 1971 .
[5] G. Moretti,et al. A time-dependent computational method for blunt body flows. , 1966 .