Use of measured imperfections to predict the buckling of axially loaded cylindrical shells
Analyses to predict inelastic buckling of axially loaded thin cylindrical shells are carried out using the finite element technique. The analyses use a bilinear elastic–perfectly plastic material response based upon the associated flow rule of plasticity. Nonlinear geometric effects, combined with initial imperfections, produce load-deflection curves with descending branches for which the limit points are imperfection sensitive.Results from these analyses are compared with two tests of axially loaded cylinders fabricated from 10-gauge (3.4-mm) and 5-mm plate and approximately 1525 mm in diameter. These tests were carried out in the Structural Engineering Laboratory at the University of Alberta. A rational technique for using measured imperfections to obtain effective initial imperfections for use in the analyses is investigated, and is shown to result in accurate predictions of ultimate load. Keywords: shell, cylinder, buckling, plastic, imperfection, axial load, finite element, nonlinear analysis.