FORCED VIBRATION AND LOW-VELOCITY IMPACT OF LAMINATED COMPOSITE PLATES

The layerwise theory of Reddy is used to study the low velocity impact response of laminated plates. Forced-vibration analysis is developed by the modal superposition technique. Six different models are introdu ced for representation of the impact pressure distribution. The first five models, in which the contact area is assumed to be known, result in a nonlinear integral equation similar to the one obtained by Timosh enko in 1913. The resulting nonlinear integral equation is discretised using a time-element scheme. Two different interpolation functions, n amely: (i) Lagrangian and (ii) Hermite, are used to express the impact force. The Hermitian polynomial-based representation, obviously more sophisticated, is introduced to verify the Lagrangian-based representa tion. Due to its modular nature the present numerical technique is pre ferable to the existing numerical methods in the literature. The final loading model, in which the time dependence of the contact area is ta ken into account according to the Hertzian contact law, resulted in a relatively more complicated but more realistic, nonlinear integral equ ation. The analytical developments concerning this model are all new a nd are reported for the first time in this paper. Also a simple, but a ccurate, numerical technique is developed for solving our new nonlinea r integral equation which results in the time-history of the impact fo rce. Our numerical results are first tested with a series of existing example problems. Then a detailed study concerning all the response qu antities, including the in-plane and interlaminar stresses, is carried out for symmetric and antisymmetric cross-ply laminates and important conclusions are reached concerning the usefulness and accuracy of the various plate theories.