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Cylindrical Bending of a Heated Long Rectangular Plate*

Published online by Cambridge University Press:  04 July 2016

Burton A. Lieb
Burton A. Lieb*
Affiliation:
Department of Engineering, University of California, at Los Angeles, Aerospace Engineering Division, Hughes Aircraft Company
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Extract

The design of structures for operation at increasingly higher temperatures and under exposure to severe heating requires more detailed and more exact analysis to determine the most severe conditions under which a given structure is operationally effective. To meet this need, the following analysis has been devised, with the determination of stresses and deflections in plates due to non-uniform heating as its purpose. The analysis results also in the determination of the maximum loads which may be imposed on the supporting members by the plate due to its thermal deformations.

Type
Research Article
Information
The Aeronautical Journal , Volume 65 , Issue 601 , January 1961 , pp. 26 - 30
Copyright
Copyright © Royal Aeronautical Society 1961

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References

1.Timoshenko, S. (1936). Theory of Elastic Stability, McGraw-Hill, New York, Section 87, 1936.Google Scholar
2.Timoshenko, S. (1940). Theory of Plates and Shells, McGraw-Hill, New York, pp. 311–322, 1940.Google Scholar
3.Sechler, E. E. (1952). Elasticity in Engineering, John Wiley, New York, Section 15.2, 1952.Google Scholar