TECHNICAL PAPERS
May 1, 1989

Exact or Lower Bound Tapered Column Buckling Loads

Publication: Journal of Structural Engineering
Volume 115, Issue 5

Abstract

The curves presented enable the buckling loads to be found for tapered columns with a uniform axial force P applied over all their length L or over all except βL (for 0β0.9) of their length. The main curves cover six combinations of end conditions, 0.05r1 and h=2,3, or 4, where r is the ratio of the second moment of area at the smaller end to the second moment of area at the larger end and h is the power which governs the variation of second moment of area with length. An evaluation is also undertaken of the accuracy of a method which uses the curves to obtain lower bound approximations to the critical load factor for stepped distributions of axial force. These lower bounds are on the safe side, so that they can cause loss of economy but not loss of safety, and for most practical problems they are within 10% of the exact answer.

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References

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Anderson, M. S., and Williams, F. W. (1987). “BUNVIS‐RG: Exact frame buckling and vibration program, with repetitive geometry and substructuring.” J. Spacecr. Rockets, 24(4), 353–361.
2.
Banerjee, J. R., and Williams, F. W. (1986). “Exact Bernoulli‐Euler static stiffness matrix for a range of tapered beam‐columns.” Int. J. Numer. Methods Eng., 23(9), 1615–1628.
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Go to Journal of Structural Engineering
Journal of Structural Engineering
Volume 115Issue 5May 1989
Pages: 1088 - 1100

History

Published online: May 1, 1989
Published in print: May 1989

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Authors

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Frederic W. Williams
Prof., School of Engrg., Univ. of Wales College of Cardiff, Cardiff CF2 1TA, Wales, U.K.
Gary Aston
Res. Student, School of Engrg., Univ. of Wales College of Cardiff, Cardiff CF2 1TA, Wales, U.K.

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