In this article , the residual strength of debond composite laminates and their repaired structures under tension and bending load is calculated using finite element analysis method . The influence of the patch parameters on the repair structure , such as the dimension of the patch, the thickness of the patch and the stacking sequence is discussed. The work includes following steps:
1. Bring forward the repair method and repair demand of composite laminates when the honeycomb is debond from the...