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Heat Transfer to Slender Bodies at a Mach Number of 5.2

Published online by Cambridge University Press:  07 June 2016

R. K. Fancett
R. K. Fancett*
Affiliation:
Royal Armament Research and Development Establishment
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Summary

Because of the lack of reliable data on heat transfer to long bodies, measurements have been made to cone-cylinder-flares at a Mach number of 5·2. Axial heat transfer distributions were closely predicted by a modified reference enthalpy method for both laminar and turbulent flows at zero incidence and the heat transfer to the flare windward generator at incidence agreed with laminar theory.

Type
Research Article
Information
Aeronautical Quarterly , Volume 22 , Issue 1 , February 1971 , pp. 12 - 24
Copyright
Copyright © Royal Aeronautical Society. 1971

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References

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