Control of boundary layer flow

Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils

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244209, 244130, B64C 2106

Patent

active

052226980

ABSTRACT:
Turbulence in the boundary layer of a flow of air across a surface is controlled by sucking air from the surface. A plurality of turbulence detectors are located in the surface downstream of apertures provided in the surface. The apertures are connected to a suction pump. Air is sucked through the apertures until the air flow of the most downstream of the detectors is non-turbulent.

REFERENCES:
patent: 3362663 (1968-01-01), Wehrmann
patent: 3951360 (1976-04-01), Anxionnaz
patent: 4516747 (1985-05-01), Lurz
patent: 4749150 (1988-06-01), Rose et al.
patent: 4936146 (1990-06-01), Stack et al.
patent: 5114103 (1992-05-01), Coffinberry
"Lamina Flow a Reality", Flight International May 15, 1982, p. 1208.

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