Behavior Of Turbulent Boundary Layers On Curved Convex Walls
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Behavior of Turbulent Boundary Layers on Curved Convex Walls
The system of linear differential equations which indicated the approach of separation and the so-called "boundary-layer thickness" by Gruschwitz is extended in this report to include the case where the friction layer is subject to centrifugal forces. Evaluation of the data yields a strong functional dependence of the momentum change and wall drag on the boundary-layer thickness radius of curvature ratio for the wall. It is further shown that the transition from laminar to turbulent flow occurs at somewhat higher Reynolds Numbers at the convex wall than at the flat plate, due to the stabilizing effect of the centrifugal forces.
Technical Memorandums
Author: United States. National Advisory Committee for Aeronautics
language: en
Publisher:
Release Date: 1936
Chiefly translations from foreign aeronautical journals.