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Volume 33, Issue 10
1 October 1961
This article was originally published in
Aircraft Engineering
Aircraft Engineering Cover Image for Volume 33, Issue 10
Review Article| October 01 1961

Transient Temperature Distributions in an Insulated Multi‐Spar Wing: An Approximate Method of Solution for a Structure Subjected to Aerodynamic Heating Based on a System of Regions Having Similar Rates of Temperature Rise

Publisher: Emerald Publishing
Online ISSN: 2059-9366
Print ISSN: 0002-2667
© MCB UP Limited
1961
Aircraft Engineering (1961) 33 (10): 282–288.
https://doi.org/10.1108/eb033463

An approximate method is employed to derive the transient temperature distributions and thermal stresses in an idealized insulated multi‐spar wing subjected to aerodynamic heating. Approximate formulae obtained by this method arc compared with exact solutions for a number of special cases, and are found to be in good agreement.

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© MCB UP Limited
1961
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