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Skin Friction and Heat Transfer at an Infinite Swept Attachment Line

Published online by Cambridge University Press:  07 June 2016

D.I.A. Poll
D.I.A. Poll*
Affiliation:
College of Aeronautics, Cranfield Institute of Technology
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Summary

Simple, yet reasonably accurate, expressions have been developed for the prediction of skin friction and heat transfer coefficient at an infinite swept attachment line using the concepts of ‘reference temperature’ and ‘Reynolds analogy’. The formulae have then been used to investigate the effect of varying sweep angle with constant undisturbed free stream conditions in the limits of very low and very high Mach number.

Type
Research Article
Information
Aeronautical Quarterly , Volume 32 , Issue 4 , November 1981 , pp. 299 - 318
Copyright
Copyright © Royal Aeronautical Society. 1981

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References

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