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Application of the Discrete Element Method to the Buckling Analysis of Rectangular Plates under Arbitrary Membrane Loading

Published online by Cambridge University Press:  07 June 2016

D. J. Dawe
D. J. Dawe*
Affiliation:
Royal Aircraft Establishment, Farnborough
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Summary

The discrete element displacement method is used to analyse the instability of flat rectangular plates subjected to arbitrary systems of in-plane loading. Critical load intensities calculated in a range of applications, some of which include discrete reinforcing members, are compared with the predictions of past investigators and demonstrate the accuracy of the procedure.

Type
Research Article
Information
Aeronautical Quarterly , Volume 20 , Issue 2 , May 1969 , pp. 114 - 128
Copyright
Copyright © Royal Aeronautical Society. 1969

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References

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