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Crossflow development at the side-edges of a corner boundary layer subjected to 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 corners formed by the intersection of two semi-infinite flat plates has been studied by many workers, notably Pearson (1957) and Rubin (1966) who treated the case of a rectangular corner. The situation is characterised by a region of three-dimensional flow in the vicinity of the intersection line bounded by regions in which the usual two-dimensional boundary layer equations are applicable. Within these boundary regions a secondary shear layer exists whose velocity is normal to the ‘two-dimensional’ vector.

Type
Research Article
Information
The Aeronautical Journal , Volume 79 , Issue 780 , December 1975 , pp. 550 - 554
Copyright
Copyright © Royal Aeronautical Society 1975 

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References

1. Pearson, J. R. Homogeneous turbulence and laminar flow. PhD thesis, Cambridge University, 1957.Google Scholar
2. Rubin, S. G. Incompressible flow along a corner. J. Fluid Mech. 26, 97, 1966.Google Scholar
3. El-Gamal, H. A. and Barclay, W. H. Laminar streamwise corner flow with suction. The Aeronautical Journal, Vol 79, No 778, p 466, October, 1975.Google Scholar
4. Rubin, S. G. and Grossman, B. Viscous flow along a corner; numerical solution of the corner layer equations. Quarterly of Applied Mathematics, July, 1971.Google Scholar
5. Pal, A. and Rubin, S. G. Asymptotic features of viscous flow along a corner. Quarterly of Applied Mathematics, April, 1971.Google Scholar
6. Iglisch, R. Exact calculations of the laminar boundary layer in longitudinal flow over a flat plate with homogeneous suction. NACA TM 1205, April 1949.Google Scholar
7. Griffith, A. A. and Meredith, F. W. The possible improvement in aircraft performance due to the use of boundary layer suction. RAE Rep No 3501, March 1936.Google Scholar