An efficient two-node curved axisymmetric shell element is proposed. The el
ement with three degrees of freedom per node accounts for the transverse sh
ear flexibility and rotary inertia. The strain components are defined in a
curvilinear co-ordinate frame. The variation of normal displacement (w) alo
ng the meridian is represented by a cubic polynomial. The relevant constitu
tive relations and the differential equations of equilibrium in the meridio
nal plane of the shell are used to derive the polynomial field for the tang
ential displacement (u) and section rotation (theta). This results in inter
dependent polynomials for the held variables w, u and theta, whose coeffici
ents are coupled by generalized degrees of freedom and geometric and materi
al properties of the element. These coupled polynomials lead to consistentl
y vanishing coefficients for the membrane and transverse shear strain field
s even in the limit of extreme thinness, without producing any spurious con
straints. Thus the element is devoid of membrane and shear locking in thin
limit of inextensible and shearless bending, respectively. Full Gaussian in
tegration rules are employed for evaluating stiffness marix, consistent loa
d vector and consistent mass matrix. Numerical results are presented for ax
isymmetric deep/shallow shells having curved/straight meridional geometries
for static and free vibration analyses. The accuracy and convergence chara
cteristics of this CO element are superior to other elements of the same cl
ass. The performance of the element demonstrates its applicability over a w
ide range of axisymmetric shell configurations. Copyright (C) 1999 John Wil
ey & Sons, Ltd.