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Laminar streamwise corner flow with suction

Published online by Cambridge University Press:  04 July 2016

H. A. El-Gamal and
W. H. Barclay
H. A. El-Gamal
Affiliation:
University College London
W. H. Barclay
Affiliation:
University College London
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Extract

The flow along the corner formed by two semi-infinite intersecting flat plates is considered in which the corner line is parallel to the streamlines of a uniform incident flow and a uniform suction is applied at the plate surfaces.

Information

Type
Technical Note
Information
The Aeronautical Journal , Volume 79 , Issue 778 , October 1975, pp. 466 - 469
Copyright
Copyright © Royal Aeronautical Society 1975 

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References

1. Griffith, A. A. and Meredith, F. W. The possible improvement in aircraft performance due to the use of boundary layer suction. RAE Rep No E3501, March 1936.Google Scholar
2. Rubin, S. G. Incompressible flow along a corner. J. Fluid Mech, Vol 26, Part 1, 1966.Google Scholar
3. Rubin, S. G. and Grossman, B. Viscous flow along a corner: Numerical solution of the corner layer equations. Quart Appl Math, Vol 29, No 2, July 1971.Google Scholar