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Shear Buckling of a Clamped Infinitely Long Plate Reinforced by a Stiffener Mesh

Published online by Cambridge University Press:  07 June 2016

H. W. Parsons  and
I. T. Cook
H. W. Parsons
Affiliation:
University of Hull
I. T. Cook
Affiliation:
University of Essex
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Summary

A theoretical solution to the initial buckling under shear stress of a long clamped plate with parallel edges reinforced by a stiffener mesh is obtained. The mesh is formed by two families of stiffeners each evenly spaced. One family consists of longitudinal stiffeners parallel to the edges of the plate and the other consists of diagonal stiffeners inclined to the parallel edges. The flexural and torsional rigidity of the stiffeners are included in the analysis. Numerical results are given for the special case in which the longitudinal stiffeners are absent and the diagonal stiffeners have flexural rigidity only.

Type
Other
Information
Aeronautical Quarterly , Volume 17 , Issue 3 , August 1966 , pp. 302 - 309
Copyright
Copyright © Royal Aeronautical Society. 1966

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References

1. Cook, I. T. and Rockey, K. C. Shear buckling of clamped and simply-supported infinitely long plates reinforced by transverse stiffeners. Aeronautical Quarterly, Vol. XIII, p. 41, February 1962.CrossRefGoogle Scholar
2. Rockey, K. C. and Cook, I. T. Shear buckling of clamped and simply-supported infinitely long plates reinforced by transverse stiffeners and a central longitudinal stiffener. Aeronautical Quarterly, Vol. XIII, p. 95, May 1962.CrossRefGoogle Scholar
3. Cook, I. T. and Rockey, K. C. Shear buckling of clamped and simply-supported infinitely long plates reinforced by closed-section transverse stiffeners. Aeronautical Quarterly, Vol. XIII, p. 212, August 1962.Google Scholar
4. Skan, S. W. and Southwell, R. V. On the stability under shearing forces of a flat elastic strip. Proc. Roy. Soc. A, Vol 105, p. 382, 1924 Google Scholar