Stability of the compressible laminar boundary layer with an external pressure gradient
Date published
1951-09
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College of Aeronautics, Cranfield
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Abstract
The small perturbation theory of the stability of the laminar boundary layer, as first considered in detail by Tollmien and Schlichting for incompressible flow and applied to compressible flow by Lees and Lin, is extended in this paper to include compressible flow with a pressure gradient in the main stream. Continues …