Aeronautical Quarterly · 1975 · 81 citations · 16 references
Natural SciencesPhysicsAcousticsAerodynamicsFluid DynamicsBoundary Layer FlowBoundary LayersBoundary-layer DynamicsBoundary-layer TheoryTurbulenceTurbulent FlowBoundary Layer InstabilityBoundary Layer MeasurementsBoundary Layer TurbulenceCurvatureTurbulent Boundary LayersVelocityVelocity Profile In Boundary LayersWall Turbulence
Summary The present experiment describes the behaviour of a turbulent boundary layer on a concave wall. At the onset of curvature there appears a fairly coherent wavelike transverse profile of mean velocity. This disturbance might be interpreted as a kind of large scale Taylor-Görtler type instability superimposed on a conventional turbulent boundary layer; further downstream the coherence degenerates as the turbulence level increases. Boundary-layer profile measurements were made at positions of maxima and minima of transverse profiles of (U-component) mean velocity. The boundary layer at the minima positions is found to be twice as thick as that at the maxima positions. Also, turbulent intensities inside the boundary layer are substantially increased as a result of the concave curvature of the surface.
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