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On Transient Temperatures and Thermal Stresses in an Idealised Wing Structure
Published online by Cambridge University Press: 04 July 2016
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.
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- Copyright © Royal Aeronautical Society 1965
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