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Aerodynamic Aspects of Boundary Layer Control for High Lift at Low Speeds*
Published online by Cambridge University Press: 04 July 2016
Summary:
The usefulness of boundary-layer control (B.L.C.) at the knee of a trailing-edge flap, over the wing nose close to the leading-edge or at the knee of a leading-edge flap is first noted. Various methods of providing B.L.C. are outlined, comprising slot blowing, slot suction, area suction, inclined air-jets, and specially-designed aerofoil shapes. The aerodynamic aspects of slot blowing over trailing-edge flaps and the wing nose are then examined in detail and both slot suction and area suction are also considered. The associated practical design features required for good performance are discussed and some flight-handling implications are mentioned.
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- Research Article
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- Copyright
- Copyright © Royal Aeronautical Society 1963
Footnotes
Much of this paper formed the basis of an unpublished lecture to the Royal Aeronautical Society, four years ago. Suitable additions and amendments have been incorporated to bring it up to date.
References
References
This list mainly refers to R.A.E. and N.P.L. papers issued since 1950, but more comprehensive bibliographies of British and Foreign work have been included in Refs. 1 to 6.
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