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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

E.C. Capey (Royal Aircraft Establishment, Farnborough, Hants)

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 October 1961

35

Abstract

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.

Citation

Capey, E.C. (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", Aircraft Engineering and Aerospace Technology, Vol. 33 No. 10, pp. 282-288. https://doi.org/10.1108/eb033463

Publisher

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MCB UP Ltd

Copyright © 1961, MCB UP Limited

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