Virtual testing of large composite structure requires multi-scale analysis techniques due to the involved high computational challenges. Global/local modeling is a possible solution in which the size of the local region is a key-aspect to approximate the solution with accuracy and efficiency; however no defined solution for the initial prediction for the size of the local region exists. In this study, wave propagation based analytical approach is proposed for an impacted laminated structure to estimate the size of the local region. Stress wave formulation and damping along the different directions of laminate can describe the shape and area of the local region. The speed for shear and flexural waves is determined along the fiber orientations and their damping characteristics are studied. Wave propagation is dependent on the mechanics of selected materials along with laminate layup and can be different in different directions, defining different shapes of the local region. The analytical approach is formulated and implemented using MATLAB code. It can figure out the distance traveled by the flexural wave front in the in-plane directions of the laminated structure. A validation is performed from three examples for the contact force and damaged area predictions. Then the study is extended for a 3D leading edge of a wing under bird striking for finding the dynamic response. The prediction is compared with the experimental results obtained in our Lab. It is shown that the current approach can not only reduce the computational effort by predicting the contact force and damaged area for high as well low speed impact scenarios, but with satisfied accuracy and efficiency. The approach can be a base for defining the size of the local area in the Global/Local modeling methodology for large composite structures. The technique can also be employed to find out the shape of the affected and damaged area in the composite structure by implementing the methodology at different angles from the impact center.
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