The numerical analysis is a very important work in the process of design on how composites resist the damage from bird impact.The paper analyzed and tested numerically the initial damage

stress and strain of every layer of laminates from bird impact using instantaneous non-linear FEM.It also analyzed how the changes of ply stacking sequence

parameter of laminates and birds affect the absorbing energy of laminates.The results of this paper provide a basis for further research on composite structures resisting bird impact.