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Buckling of Longitudinally Stiffened Plates

Published online by Cambridge University Press:  07 June 2016

Thein Wah
Thein Wah*
Affiliation:
Southwest Research Institute, San Antonio, Texas
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Summary

This paper investigates the effect of the torsional stiffness of the ribs on the buckling strength of stiffened plates compressed in the direction of the ribs. For the case of plates simply-supported on all sides, a closed form formula is derived for calculating the buckling load.

Information

Type
Research Article
Information
Aeronautical Quarterly , Volume 18 , Issue 1 , February 1967 , pp. 85 - 99
Copyright
Copyright © Royal Aeronautical Society. 1967

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References

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3. Ratzersdorfer, J. Rectangular plates with stiffeners. Aircraft Engineering, Vol. XIV, No. 163, p. 260, September 1942.Google Scholar
4. Seide, P. and Stein, M. Compressive buckling of simply supported plates with longitudinal stiffeners. NACA TN 1825, 1949.Google Scholar
5. Seide, P. The effect of longitudinal stiffeners located on one side of a plate on the compressive buckling stress of the plate stiffener combination. NACA TN 2873, January 1953.Google Scholar