A theory of space curved beams with arbitrary cross-sections and an associa
ted finite element formulation is presented. Within the present beam theory
the reference point, the centroid, the centre of shear and the loading poi
nt are arbitrary points of the cross-section. The beam strains are based on
a kinematic assumption where torsion-warping deformation is included. Each
node of the derived finite element possesses seven degrees of freedom. The
update of the rotational parameters at the finite element nodes is achieve
d in an additive way. Applying the isoparametric concept the kinematic quan
tities are approximated using Lagrangian interpolation functions. Since the
reference curve lies arbitrarily with respect to the centroid the develope
d element can be used to discretize eccentric stiffener of shells. Due to t
he implemented constitutive equations for elastoplastic material behaviour
the element can be used to evaluate the load-carrying capacity of beam stru
ctures. Copyright (C) 2000 John Wiley & Sons, Ltd.