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Fundamental Principles and Theorems of Thermo-Elasticity
Published online by Cambridge University Press: 07 June 2016
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.
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- Copyright © Royal Aeronautical Society. 1956
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