Influence of material thickness on the response of carbon-fabric/epoxy panels to low velocity impact

Low velocity impact tests were carried out on carbon-fabric/epoxy laminates of different thicknesses, by means of a hemispherical impactor. The force and absorbed energy at the point of delamination initiation, the maximum fo rce and related energy, and penetration energy were evaluated. From the exp erimental results, all these quantities, except the energy for delamination initiation, followed the same trend, increasing to the power of approximat ely 1.5 with increasing plate thickness. For what concerns the force at del amination initiation, it is shown that its trend agrees with the assumption of a Hertzian contact law, coupled with the hypothesis that only the shear stress is responsible for delamination. It is also demonstrated that the f orce/displacement curves recorded for the different thicknesses sensibly su perpose with each other when the forces are scaled to the power 1.5 and the displacements are held unchanged. This explains the observed dependence of the maximum force, energy at maximum force, and penetration energy on the thickness. Finally, the energy at delamination initiation is calculated by an analytical model, assuming that the total energy is shared in two parts, one of which is stored in flexure, and the other in the material volume cl ose to the contact zone. (C) 1999 Elsevier Science Ltd. All rights reserved .