The paper presents a spatial Timoshenko beam element with a total Lagrangia
n formulation. The element is based an curvature interpolation that is inde
pendent of the rigid-body motion of the beam element and simplifies the for
mulation. The section response is derived from plane section kinematics. A
two-node beam element with constant curvature is relatively simple to formu
late and exhibits excellent numerical convergence. The formulation is exten
ded to N-node elements with polynomial curvature interpolation. Models with
moderate discretization yield results of sufficient accuracy with a small
number of iterations at each load step. Generalized second-order stress res
ultants are identified and the section response takes into account non-line
ar material behaviour. Green-Lagrange strains are expressed in terms of sec
tion curvature and shear distortion, whose first and second variations are
functions of node displacements and rotations. A symmetric tangent stiffnes
s matrix is derived by consistent linearization and an iterative accelerati
on method is used to improve numerical convergence for hyperelastic materia
ls. The comparison of analytical results with numerical simulations in the
literature demonstrates the consistency, accuracy and superior numerical pe
rformance of the proposed element. Copyright (C) 2001 John Wiley & Sons, Lt
d.