The formulation of a 3D composite element and its use in a mixed-mode fract
ure mechanics example is presented. This element, like a conventional 3D fi
nite element, has three degrees of freedom per node although, like a plate
element, the strains are defined in the local directions of the mid-plane s
urface. The stress-strain property matrix of this element was modified to d
ecouple the stresses in the local mid-plane and the strains normal to this
plane thus preventing the element from being too stiff in bending. A main a
dvantage of this formulation is the ability to model a laminate with a sing
le 3D element. The motivation behind this work was to improve the computati
onal efficiency associated with the calculation of strain energy release ra
tes in laminated structures. A comparison of mixed-mode results using diffe
rent elements of an in-house finite element package are presented. Good agr
eement was achieved between the results obtained using the new element and
coventional higher-order elements. (C) 1999 Elsevier Science Ltd. All right
s reserved.