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A Comparison Between Some Approximate and Exact Solutions of the Laminar Boundary-Layer Equations

Published online by Cambridge University Press:  04 July 2016

J. L. Stollery*
Affiliation:
Department of Aeronautics, Imperial College of Science and Technology, London

Extract

There are many approximate methods for solving the laminar boundary-layer equations. They vary greatly in complexity and ingenuity but are similar in that most of them use the momentum integral equation together with data culled from Cohen and Reshotko's valuable catalogue of similarity solutions. Further details may be found, for example, in the book by Curle.

Perhaps one of the simplest approximate methods to use is that due to Luxton and Young. More recently Luxton has extended the method so that heat transfer rate distributions also can be obtained. He is careful to point out that, since his method depends on correlations obtained from similar solutions, it cannot be claimed a priori that the method gives an accurate result. Until recently there have been few “exact” calculations against which approximate methods may be tested. Indeed when Morduchow made his review of boundary-layer calculations in 1965 he quoted only two exact results for non-zero Mach number (by NPL) and cast doubt on one of those. Fitzhugh has now computed a number of solutions of the laminar boundary-layer equations using the finite-difference program of Sells. Further solutions have recently been obtained by F. Smith.

Type
Technical Notes
Copyright
Copyright © Royal Aeronautical Society 1970 

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References

1. Curle, N. The Laminar Boundary-Layer Equations. Oxford Mathematical Monographs, Clarendon Press, Oxford 1962.Google Scholar
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