Nonlinear Finite Element Eccentric Low-Velocity Impact Analysis of Rectangular Laminated Composite Plates Subjected to In-phase/Anti-phase Biaxial Preloads

All impact analyses performed so far for the composite plates, have treated central impacts. furthermore, investigations on influences of the in-plane biaxial compression, tension, or tension-compression preloads on various responses of the low-velocity impact, especially the indentation, have not been performed so far. in the present research, a finite element formulation is presented for response prediction of a low-velocity eccentric impact between a rigid spherical indenter and a laminated composite rectangular plate with asymmetric lamination scheme. different contact laws are considered for the loading and unloading phases. a parametric study is performed to investigate influence of the specifications of the plates and the indenter, the eccentric value, and the in-plane preloads on the indentation and force time histories. results show that the compressive and tensile in-plane preloads reduce and increase the contact force (and consequently, the indentation values), respectively. therefore, the extensive tensile preloads may lead to higher damages.