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Note on Cylindrical Bending of a Heated Long Rectangular Plate

Published online by Cambridge University Press:  04 July 2016

J. S. Przemieniecki*
Affiliation:
United States Air Force Institute of Technology

Extract

In reference 1 a general analysis was presented for the calculation of thermal stresses and deflections due to temperature gradients in long rectangular plates having lengthwise edges supported elastically. The edge support was idealised as equivalent rotational and extensional stiffnesses depending on the elastic characteristics of the surrounding structure. The special case of infinite extensional stiffness and freely hinged edges (see Fig. 1) was discussed in greater detail and a number of graphs were included for the calculation of edge reactions in terms of the thermal force and thermal moment parameters. Since these graphs used an excessive number of non-dimensional parameters their practical application is unwieldy; four non-dimensional parameters were used instead of three parameters which would be sufficient to describe the required functional relationship. This note shows an alternative presentation of the results which can be used more conveniently in any design calculations.

Type
Technical Notes
Copyright
Copyright © Royal Aeronautical Society 1963

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References

1.Lieb, B. A. (1961). Cylindrical Bending of a Heated Long Rectangular Plate. Journal of the Royal Aeronautical Society, Vol. 65, pp. 2630, Jan. 1961.CrossRefGoogle Scholar
2. Royal Aeronautical Society, Structures Data Sheets H 02.00.00 to H 02.00.04, February 1962.Google Scholar
3.Williams, M. L. (1958). Further Large Deflection Analysis for Plate Strip Subjected to Normal Pressure and Heating. Journal of Applied Mechanics, Vol. 25, pp. 251258, June 1958.Google Scholar