AIAA Journal · 1984 · 47 citations · 9 references
EngineeringAerospace EngineeringAerodynamicsComputational Fluid DynamicsFluid DynamicsBoundary Layer FlowBoundary-layer StructureBoundary-layer TheoryTurbulenceTurbulent FlowWind-tunnel TestingBoundary Layer ReattachmentBoundary Layer Shear StressFlow ReattachmentPressure Coefficient DistributionReattachment Pressure DistributionSeparation In Turbulent Boundary LayersSkin FrictionSkin-friction Coefficient
The reattachment of a fully turbulent, two-dimentional shear layer downstream of a backward-facing step has been studied experimentally. The work examines the effect of variations in inlet conditions on the process of reattachment. A series of experiments was conducted in a low-speed wind tunnel using specialized instrumentation suited to the highly turbulent reversing flow near reattachment. Accurate characterization of the time-mean features of the reattaching flows was possible. Assuming linear scaling normalized on distance from reattachment, distributions of normalized pressure coefficient and forward flow fraction, and time-averaged skin friction coefficient appear universal for two-dimensional reattachment, independent of initial conditions and step height, for given duct geometry (area ratio) and for high step-height Reyolds numbers with thin separating boundary layers. The results suggest universal flow structure in the reattachment zone.
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Turbulence structure of a reattaching mixing layer
C. Chandrsuda, P. Bradshaw · Journal of Fluid Mechanics · 1981 · 190 citations