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A Correlation between Pressure and Heat Transfer Distributions at Supersonic and Hypersonic Speeds

Published online by Cambridge University Press:  07 June 2016

J L Stollery and
G T Coleman
J L Stollery
Affiliation:
College of Aeronautics, Cranfield
G T Coleman
Affiliation:
Royal Aircraft Establishment, Farnborough
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Summary

The “reference enthalpy” and local flat plate concepts are used to derive some simple expressions for the turbulent heat transfer rate distribution over an arbitrary body at supersonic and hypersonic speeds. The connection between pressure and heat transfer rate is established and tested against a number of experimental data.

Information

Type
Research Article
Information
Aeronautical Quarterly , Volume 26 , Issue 4 , November 1975, pp. 304 - 312
Copyright
Copyright © Royal Aeronautical Society. 1975

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References

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