A 2-noded curved composite beam element with three degrees of freedom per n
ode is proposed for the analysis of laminated beam structures. The formulat
ion accounts for flexural, extensional and transverse shear loadings in the
plane of the curved beam. The transverse shear flexibility based on first-
order shear deformation theory is incorporated. A cubic polynomial is assum
ed for the transverse displacement w. The field interpolations for the long
itudinal displacement u and section rotation theta are derived using the el
emental equilibrium equations. The procedure leads to field interpolations
that are coupled by means of coefficients, which are functions of geometric
al and material properties of the element. The efficacy of these coupled po
lynomial fields in improving the accuracy and convergence characteristics o
f the proposed element has been demonstrated by a series of numerical examp
les. The lay-up sequence does not affect the accuracy of the element, unlik
e the conventional 2-noded elements, which make use of independent field in
terpolations. The element does not exhibit membrane and shear locking. The
test problems prove the versatility of the element for the analysis of curv
ed and straight laminated beams. (C) 2000 Elsevier Science Ltd. All rights
reserved.