A new stiffened plate element for stability analysis of laminated stiffened
plates has been presented. The basic plate element is a combination of All
man's plane stress triangular element and a Discrete Kirchhoff-Mindlin plat
e bending element. The element includes transverse shear effects. The model
accommodates any number of arbitrarily oriented stiffeners within the plat
e element and eliminates constraints on the mesh division of the plate. The
element has no problem associated with shear locking - a phenomenon usuall
y encountered in isoparametric elements. The stability analysis of laminate
d stiffened plates has been carried out under different loading conditions
with the present element. (C) 1999 Elsevier Science Ltd. All rights reserve
d.