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Approximate Calculations of the Incompressible Laminar Boundary Layer

Published online by Cambridge University Press:  07 June 2016

M. R. Head  and
N. Hayasi
M. R. Head
Affiliation:
Lockheed-Georgia Aerospace Sciences Laboratory
N. Hayasi
Affiliation:
Lockheed-Georgia Aerospace Sciences Laboratory
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Summary

A recent calculation method proposed by Curle has been applied to the flow U=U0ξe-ξ for which a computer solution exists. An earlier approximate method due to Head, presented here in a simplified form, has been applied to the same problem. All three solutions are found to be in close agreement. A further problem, already examined by Curle, is treated by Head’s method. Again the results are in good agreement with each other and with an exact solution obtained subsequently.

Type
Research Article
Information
Aeronautical Quarterly , Volume 18 , Issue 3 , August 1967 , pp. 259 - 272
Copyright
Copyright © Royal Aeronautical Society. 1967

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References

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An addendum has been issued for this article:

Errata and Addendum