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On the reversed flow solutions of the Falkner-Skan equation

Published online by Cambridge University Press:  26 February 2010

S. N. Brown  and
K. Stewartson
S. N. Brown
Affiliation:
University College, Gower Street, London, W.C.1.
K. Stewartson
Affiliation:
University College, Gower Street, London, W.C.1.
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Abstract

The dependence of the skin friction on the parameter β for the reversed flow solutions found by Stewartson of the Falkner-Skan equation f′′′ + ff″ + β (1−f′2)=0 is determined in the limit as β→0−.

Type
Research Article
Information
Mathematika , Volume 13 , Issue 1 , June 1966 , pp. 1 - 6
Copyright
Copyright © University College London 1966

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References

1. Hartree, D. R., “On an equation occurring in Falkner and Skan's approximate treatment of the equations of the boundary layer“, Proc. Cambridge Phil. Soc., 33 (1937), 223–239.CrossRefGoogle Scholar
2. Stewartson, K., “Further solutions of the Falkner-Skan equation”, Proc. Cambridge Phil. Soc., 50 (1954), 454–465.CrossRefGoogle Scholar
3. Lees, L. and Reeves, B. L., “Supersonic separated and reattaching laminar flows: 1. General theory and application to adiabatic boundary layer/shock-wave interactions”, Amer. Inst. Aero. Astro. Journal, 2 (1964), 1907-1920.Google Scholar
4. Kennedy, E. D., “Wake-like solutions of the laminar boundary layer equations”, Amer. Inst. Aero. Astro. Journal, 2 (1964), 225–231.Google Scholar
5. Chapman, D. R., “Laminar mixing of a compressible fluid”, Rep. nat. adv. Comm. Aero., Wash, No. 958 (1950).Google Scholar
6. Stewartson, K., “Falkner-Skan equation for wakes”, Amer. Inst. Aero. Astro. Journal, 2 (1964), 1327–1328.Google Scholar