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On Similar Solutions of the Boundary Layer Equations for Air in Dissociation Equilibrium

Published online by Cambridge University Press:  04 July 2016

R. L. Dommett
R. L. Dommett*
Affiliation:
Royal Aircraft Establishment, Farnborough
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Extract

Using a Stewartson transformation defined by

it is straightforward to show that in the two cases for which it is possible to find similar solutions to the laminar boundary layer equations with Pr≠1, Le=1, that is stagnation flows Ue∝X and flat plate flows Ue=constant, it is not necessary to assume anything about the specific heats to derive the equations given and solved by Beckwith.

Type
Technical Notes
Information
The Aeronautical Journal , Volume 64 , Issue 589 , January 1960 , pp. 36 - 37
Copyright
Copyright © Royal Aeronautical Society 1960

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References

1.Beckwith, I. E. (1958). Similar solutions for the compressible boundary layer on a yawed cylinder with transpiration cooling. N.A.C.A. T.N. 4345, September 1958.Google Scholar
2.Young, G. B. W. and Janssen, E. (1952). The compressible boundary layer. Journal of the Aeronautical Sciences, Vol. 19, April 1952.Google Scholar
3.Van Driest, E. R. (1954). The laminar boundary layer with variable fluid properties. N.A.A. Report AL-1866, 1954.Google Scholar
4.Fay, J. A. and Riddeix, F. R. (1958). Theory of stagnation point heat transfer in dissociated air. Journal of the Aeronautical Sciences, Vol. 25, p. 73, February 1958.Google Scholar
5.Romig, M. F. and Dore, F. J. (1954). Solutions of the compressible laminar boundary layer including the case of a dissociating free stream. CONVAIR Report ZA-7-012, August 1954.Google Scholar
6.Mark, R. (1955). Compressible laminar heat transfer near the stagnation point of blunt bodies of revolution. CON VAIR Report ZA-7-016, April 1955.Google Scholar
7.Hansen, C. F. (1958). Approximations for die thermodynamic and transport properties of high temperature air. N.A.C.A. T.N. 4150, March 1958.Google Scholar
8.Beckwith, I. E. (1958). The effect of gas properties on the heat transfer in stagnation flows. Journal of the Aeronautical Sciences, Vol. 25, p. 533, August 1958.Google Scholar