Composite materials are widely used in aeronautical, marine and automotive industries, because of their excellent mechanical properties, low density and ease of manufacture. However, composite laminates are susceptible to delaminations,...
moreComposite materials are widely used in aeronautical, marine and automotive industries, because of their excellent mechanical properties, low density and ease of manufacture. However, composite laminates are susceptible to delaminations, which may not be visible externally, but can substantially affect the performance of the structure. The final objective of this research is to develop a Structural Health Monitoring (SHM) system based on vibration monitoring, to detect, locate and assess delamination damage in laminated composite structures. Towards this end, finite element modelling is employed to simulate the dynamic response of composite laminates (beams and plates) with delamination and extract their vibration parameters. According to the reported theoretical models, we built two finite element (FE) models using Ansys, one free and the other constrained. Modal analysis is applied to the free FE model to extract eigen frequencies while transient analysis is used to get natural frequencies from theconstrained model where contact elements haven't been ignored as in the former. The natural frequencies extracted from the current numerical simulations are compared with previous theoretical, numerical and experimental results as well as from our experimental modal analysis conducted on composite beams with delaminations.