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PatentDOI

Control of laminar flow in fluids by means of acoustic energy

Rudolph A. Mangiarotty
- 25 Aug 1987 - 
- Vol. 86, Iss: 1, pp 450-450
TLDR
In this paper, the authors proposed to reduce the point of transition from laminar flow to turbulent flow in aerodynamic boundary layers on the surfaces of aircraft by radiating acoustic energy at frequencies greater than twice the critical TollmeinSchlichting frequency into the boundary layer.
Abstract
Retarding of the point of transition from laminar flow to turbulent flow in aerodynamic boundary layers on the surfaces of aircraft is accomplished by radiating acoustic energy at frequencies greater than twice the critical Tollmein-Schlichting frequency into the boundary layer. The acoustic energy interferes with the formation of Tollmein-Schlichting waves, thereby increasing the incidence of laminar flow and reducing aerodynamic drag.

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References
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Patent

Method of and apparatus for controlling the boundary layer flow over the surface of a body

Werner Lurz
TL;DR: In this paper, a sensor element in the surface measures certain flow values in the boundary layer, conveyed to an analyzer control circuit which, in turn, conveys a signal to an active vibration transmitter in the body for providing the required control.
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TL;DR: In this article, a low-drag surface construction using a plurality of longitudinally extending, parallel, spaced apart linear vortices extending transversely of the free stream is proposed.
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Acoustic wing stall delaying device

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TL;DR: In this article, the authors propose an apparatus for delaying the onset of wing stall in an aircraft having a plurality of acoustic resonators positioned in the forward portion of the upper surface of the wing with a movable panel to close the resonator cavities during normal flight.
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