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Incompressible Laminar Boundary Layers on a Parabola at Angle of Attack: A Study of the Separation Point
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1972
Year
Numerical AnalysisAeroacousticsUnsteady FlowCompressible FlowEngineeringIncompressible FlowAerospace EngineeringGoldstein-type SingularityFluid MechanicsBoundary-layer Separation ProcessAerodynamicsLaminar Boundary-layer EquationsMultiphase FlowSeparation PointBoundary LayerHydrodynamic Stability
The laminar boundary-layer equations were solved for incompressible flow past a parabola at angle of attack. Such flow experiences a region of adverse pressure gradient and thus can be employed to study the boundary-layer separation process. The present solutions were obtained numerically using both implicit and Crank-Nicolson-type difference schemes. It was found that in all cases the point of vanishing shear stress (the separation point) displayed a Goldstein-type singularity. Based on this evidence, it is concluded that a singularity is always present at separation independent of the mildness of the pressure gradient at that point.