Aeronautical Quarterly · 1967 · 237 citations · 7 references
EngineeringAerospace EngineeringPhysicsAerodynamicsComputational Fluid DynamicsFluid DynamicsBoundary Layer FlowBoundary LayersBoundary-layer StructureBoundary-layer TheoryExperimental AerodynamicsVortex DynamicsBleedBoundary Layer ThicknessDragEdge Pressure EffectsReynolds NumberTrailing-edge VorticesVortex Dynamics In Boundary LayersVortex Formation
Summary The effects of base bleed on the flow about a two-dimensional model with a blunt trailing edge were examined at Reynolds numbers, based on model base height, between 1·3×10 4 and 4·1×10 4 . The ratio of boundary layer thickness at the trailing edge to half the model base height was approximately 0·4. Measurements were made of base pressure, vortex shedding frequency and the distance to vortex formation. With a sufficiently large bleed quantity the regular vortex street pattern disappeared and the base drag of the section was reduced to about a third of its value without bleed. The base pressure was found to vary linearly with the inverse of the vortex formation distance. Results of a previous splitter plate investigation were found to agree closely with those of the present experiments.
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The formation of vortex streets
Frederick H Abernathy, Richard E. Kronauer · Journal of Fluid Mechanics · 1962 · 182 citations