Hostname: page-component-66644f4456-kglw6 Total loading time: 0 Render date: 2025-02-13T10:32:20.325Z Has data issue: true hasContentIssue false
  • English
  • Français

On Transient Temperatures and Thermal Stresses in an Idealised Wing Structure

Published online by Cambridge University Press:  04 July 2016

J. P. H. Webber  and
D. S. Houghton
J. P. H. Webber
Affiliation:
Royal Military College of Science, Shrivenham
D. S. Houghton
Affiliation:
Royal Military College of Science, Shrivenham
Get access Rights & Permissions [Opens in a new window]

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.

Type
Technical Notes
Information
The Aeronautical Journal , Volume 69 , Issue 653 , May 1965 , pp. 347 - 350
Copyright
Copyright © Royal Aeronautical Society 1965

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

1.Hoff, N. J.Structural Problems of Future Aircraft. Third Anglo-American Aeronautical Conference, Brighton, 1951.Google Scholar
2.Parkes, E. W. Transient Thermal Stresses in Wings. Aircraft Engineering, December 1953.CrossRefGoogle Scholar
3.Pohle, F. V. and Oliver, H.Temperature Distribution and Thermal Stresses in a Model of a Supersonic Wing. Journal of the Aeronautical Sciences, Vol. 21, January 1954.CrossRefGoogle Scholar
4.Schuh, H.Transient Temperature Distributions and Thermal Stresses in a Skin-Shear Web Configuration at High-Speed Flight for a Wide Range of Parameters. Journal of the Aeronautical Sciences, Vol. 22, December 1955.CrossRefGoogle Scholar
5.Capey, E. C. Transient Temperature Distributions in an Insulated Multi-Spar Wing. Aircraft Engineering, October 1961.CrossRefGoogle Scholar
6.Carslaw, H. S. and Jaeger, J. C.Conduction of Heat in Solids.Chapter III. Oxford University Press, 1947.Google Scholar
7.Biot, A.New Methods in Heat Flow Analysis with Application to Flight Structures. Journal of the Aeronautical Sciences, December 1957.CrossRefGoogle Scholar