The effects of the initial imperfections on the nonlinear behaviors and ult
imate strength of the thin-walled members subjected to the axial loads, obt
ained by the finite element stability analysis, are examined. As the initia
l imperfections, the buckling mode shapes of the members are adopted. The b
uckling mode shapes of the thin-walled members are obtained by the transfer
matrix method. In the finite element stability analysis, isoparametric deg
enerated shell element is used, and the geometrical and material nonlineari
ty are considered based on the Green Lagrange strain definition and the Pra
ndtl-Reuss stress-strain relation following the von Mises yield criterion.
The U-, box- and I-section members subjected to the axial loads are adopted
for numerical examples, and the effects of the initial imperfections on th
e nonlinear behaviors and ultimate strength of the members are examined.