This article deals with the transient response of a stiffened composite pla
te subjected to low velocity impact. An approximate solution for the predic
tion of plate response to low velocity impact is presented. This solution i
ncludes the combined action of the plate and stiffeners as well as the effe
cts of the contact and transverse shear deformation. A finite element (FE)
approach is also proposed. In the FE approach, an impact force function bas
ed on Hertz contact law is linked into a commercial FE code, which facilita
tes the study of a more realistic model. Results predicted by the present s
olution for a simplified stiffened plate are compared with those by the FE
approach for a realistic stiffened plate. Effects of the stiffener spacing
and thickness, anisotropic material properties, impact mass and contact sti
ffness on the impact response are also examined. (C) 1999 Elsevier Science
Ltd. All rights reserved.