The response of orthotropic composite cylindrical shells subjected to
low-velocity impact by a solid striker is described. An analytical sol
ution that accommodates normal impact at any location is presented. Th
is solution is based on a higher order shear deformation theory and de
rived in terms of two sets of shell coordinates and an integer factor
to facilitate analysis of noncentral impact. An analytic impact force
function recently proposed by the authors is used to predict the conta
ct force between striker and shell and this is incorporated into the s
olution. Impact experiments are also conducted on a simply supported g
lass/epoxy cylindrical shell. The effective contact stiffness between
the shell and striker is obtained by fitting an impact force function
to experimental data. The strain responses of the shell to central and
noncentral impact are investigated and the present solutions verified
by the experiments.