1952•NASA STI Repository (National Aeronautics and Space Administration)Open access

Development of a laminar boundary layer behind a suction point

Walter Wuest

Abstract

A theoretical investigation is made of the development of a laminar boundary layer behind a suction slot that is assumed to cut off part of the boundary layer without exerting any sink effect. The development, which is approximate, is based on the heat conduction equation. The heat conduction equation enters the analysis through a linearization of the Prandtl-Mises form of the boundary-layer equation.

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Key concepts: Laminar flow, Boundary layer, Thermal conduction, Blasius boundary layer, Boundary layer control, Mathematics, Mechanics, Linearization