The Hertzian static contact law predicts the force-indentation relationship
for impacted composite laminates inaccurately. An innovative solution meth
od has been developed for the impact contact problem by using volumetric di
splacements as control variables and discrete patch loadings as state varia
bles. Impact responses are acquired through modal superposition in terms of
loading distribution rather than conventional displacement fields. A syste
m of governing equations of contact stresses is derived via an energy varia
tional approach, with three-dimensional boundary conditions and interlamina
r continuity taken into account. Using small incremental linearization, the
nonlinear impact contact problem involving discrete pressures and the fina
l contact area is solved by iteration. Three-dimensional displacements and
stresses can be evaluated throughout the laminated plate for dynamic respon
se. (C) 1999 Elsevier Science Ltd. All rights reserved.