A quadrilateral plane element for analysis of spatial structures is of
ten formulated by combining a plane stress (membrane) element with two
translational inplane degrees of freedom at each comer to a plate ben
ding element with two rotational degrees of freedom and one translatio
nal (normal to the plane of element) at each comer. An additional rota
tional degree of freedom normal to the plane of the element and a fict
itious torsional spring are added at each comer. This brings the total
comer nodal degrees of freedom to three rotations and three translati
ons and makes the element usable for general spatial structures. A qua
drilateral hybrid stress element with two translational and one rotati
onal degrees of freedom at each comer is presented in this paper. When
used as the membrane constituent of a shell element, the rotational d
egree of freedom provides factual torsional stiffness. The element mat
rices are derived by minimization of a functional consisting of displa
cement and stress fields. Allman's displacement field is used with sev
en stress modes. The element passes the patch test and is invariant to
orientation of axes and node numbering. Results of commonly employed
benchmark tests are presented to show that the element is accurate and
robust.