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Fundamental Principles and Theorems of Thermo-Elasticity

Published online by Cambridge University Press:  07 June 2016

W. S. Hemp
W. S. Hemp*
Affiliation:
College of Aeronautics
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Extract

Kinetic heating associated with supersonic flight presents new problems to the aircraft structural engineer. Some of these can be resolved by the use of the theorems of thermo-elasticity. This paper outlines the foundations of this subject and derives generalisations of the usual variational theorems, which are so often used in structural analysis.

Type
Research Article
Information
Aeronautical Quarterly , Volume 7 , Issue 3 , August 1956 , pp. 184 - 192
Copyright
Copyright © Royal Aeronautical Society. 1956

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References

1. Love, A. E. H. A Treatise on the Mathematical Theory of Elasticity. Cambridge University Press, Fourth Edition, 1927.Google Scholar
2. Sokolnikoff, I. S. and Specht, R. D. Mathematical Theory of Elasticity. McGraw-Hill, 1946.Google Scholar
3. Roberts, J. K. Heat and Thermodynamics. Blackie, Fourth Edition, 1951.Google Scholar
4. Carslaw, H. S. and Jaeger, J. C. Conduction of Heat in Solids. Clarendon Press, 1947.Google Scholar