This research deals with the oblique impact contact of a simply supported l
aminated plate by a rigid impactor, in which the moving boundary problem is
composed of an undetermined contact area and undetermined contact stresses
distribution with anisotropic friction. By using the three-dimensional the
ory of laminated plates and shells, an innovative solution method is introd
uced for the governing equations of contact stresses via the energy variati
on and contact mechanics approach. Volumetric displacements and discrete pa
tch loadings are considered as control variables and state variables, respe
ctively. Three-dimensional boundary conditions with contact surface anisotr
opic friction, interlaminar continuity of layer displacements, and transver
se stresses are included. Impact responses are acquired through modal super
position in terms of the loading distribution rather than conventional disp
lacement fields. Using small incremental linearization, the non-linear obli
que impact contact problem (involving discrete pressures and the final cont
act area) is solved by iteration. Three-dimensional dynamic displacements a
nd stresses can be evaluated throughout the laminated plate. (C) 1999 Elsev
ier Science Ltd. All rights reserved.