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Buckling of Oblique Plates with Clamped Edges under Uniform Compression

Published online by Cambridge University Press:  07 June 2016

W. H. Wittrick
W. H. Wittrick*
Affiliation:
Department of Aeronautical Engineering, University of Sydney
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Summary

The problem of the buckling of flat oblique plates (i.e. in the shape of parallelograms) with all edges clamped under a uniform system of stress is considered. An energy method of calculating the critical stresses is developed and applied to the particular case of a clamped oblique plate under uniform compression parallel to two of the sides. Numerical values for the buckling stress coefficient are obtained for plates having acute angles of 60° and 45°, and side ratios varying between 3/5 and 5/3.

Type
Research Article
Information
Aeronautical Quarterly , Volume 4 , Issue 2 , August 1953 , pp. 151 - 163
Copyright
Copyright © Royal Aeronautical Society. 1953

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References

1. Southwell, R. V. (1936). Theory of Elasticity. Oxford University Press, 1936.Google Scholar
2. Iguchi, S. (1933). Eine Lösung fur die Berechnung der biegsamen rechteckigen Flatten. Julius Springer, Berlin, 1933.CrossRefGoogle Scholar
3. Smith, R. C. T. (1944). The Buckling of Flat Plywood Plates in Compression. Report ACA-12, Australia, 1944.Google Scholar
4. Crout, P. D. (1941). A Short Method for Evaluating Determinants and Solving Systems of Linear Equations with Real or Complex Coefficients. Transactions of the American Institution of Electrical Engineers, p. 1235, 1941.CrossRefGoogle Scholar
5. Levy, S. (1942). Buckling of Rectangular Plates with Built-in Edges. Journal of Applied Mechanics, Vol. 9, p. A-171, 1942.CrossRefGoogle Scholar
6. Anderson, R. A. (1951). Charts Giving Critical Compressive Stress of Continuous Flat Sheet Divided into Parallelogram-Shaped Panels. N.A.C.A. Technical Note 2392, 1951.Google Scholar
7. Guest, J. (1951). The Buckling of Uniformly Compressed Parallelogram Plates having all Edges Clamped. Aeronautical Research Laboratories Report S.M.172, Australia, 1951.Google Scholar
8. Budiansky, B., Connor, R. W. and Stein, M. (1948). Buckling in Shear of Continuous Flat Plates. N.A.C.A. Technical Note 1565, 1948.Google Scholar