Device for regulating and recovering the boundary layer over the

Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils

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114 67R, B64C 2108

Patent

active

039513602

ABSTRACT:
In order to control the boundary layer of air over the outer surface of an airframe and to recover some of its energy, portions of this boundary layer are sucked at a multiplicity of locations distributed over this surface and thereafter discharged rearwardly as a jet contributing to propulsion. Such suction takes place through orifices having inlets directed towards the rear and the sucked flow is adjusted so as to draw off only a part of the boundary layer whose velocity relative to the airframe is but a minor fraction of the absolute velocity of the latter, thereby leaving a substantial thickness of boundary layer.

REFERENCES:
patent: 1957413 (1934-05-01), Price
patent: 2041786 (1936-05-01), Stalker
patent: 2071744 (1937-02-01), Henrikson
patent: 2406920 (1946-09-01), Stalker
patent: 2443936 (1948-06-01), Stalker
patent: 2568813 (1951-09-01), Lundberg
patent: 2742247 (1956-04-01), Lachmann
patent: 2751168 (1956-06-01), Stalker

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