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
ISSN: 0002-2667
Article publication date: 1 October 1961
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
:MCB UP Ltd
Copyright © 1961, MCB UP Limited