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On Transient Temperatures and Thermal Stresses in an Idealised Wing Structure

Published online by Cambridge University Press:  04 July 2016

J. P. H. Webber  and
D. S. Houghton
J. P. H. Webber
Affiliation:
Royal Military College of Science, Shrivenham
D. S. Houghton
Affiliation:
Royal Military College of Science, Shrivenham
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Summary

An analytical solution is given for the one-dimensional distribution of temperature in a web of an idealised multi-cell wing structure when the adiabatic wall temperature variation is assumed to be either an instantaneous or a linear function of time. The maximum temperature difference between skin and web centre is computed for a range of structural geometries and thermal parameters. Thermal stresses are calculated assuming a parabolic temperature distribution in the web.

Type
Technical Notes
Information
The Aeronautical Journal , Volume 69 , Issue 653 , May 1965 , pp. 347 - 350
Copyright
Copyright © Royal Aeronautical Society 1965

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References

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