An effect of sudden circumferential strain on the laminar boundary layer on a rotating cylinder in an axial flow
The laminar boundary layer which develops on a rotating thin cylinder fitted with an aft-section rotating with an angular velocity different from that of a fore-section is examined numerically. This problem concerns a relaxation process of the boundary layer subjected to a sudden circumferential rate of strain. Two methods are adopted: one is to regard the flow on the aft-cylinder as perturbations of that on the fore- section, and the other is to approximate the discontinuous change in the angular celocity by the cumulative normal distribution function. It is shown that the flow fields are largely influenced by the degree of favorable pressure gradient produced in the boundary layer. Especially, in case of flow passing onto the aft-section with a smaller angular velocity, adverse pressure gradient is induced immediately after the junction between two cylinders, and when the degree of the discontinuity is increased, flow separation can be provoken.
flow on the aft-cylinder as perturbations of that on the fore-section
approximate the discontinuous change in the angular celocity
scientific article; zbMATH DE number 3908019