SUMMARY
Delamination is the separation of layers which are fortified together in composite cover. It is a typical harm in fiber strengthened composite overlays, normally avoided outer view. On account of bowing burdens delamination as a rule prompts critical loss of twisting firmness and quality. Accordingly, it is essential to distinguish the nearness of delamination at a beginning time on the grounds that early harm discovery assumes a critical part to ensure security and unwavering quality of in-benefit structures. The delamination causes diminishment of solidness and in this manner the modular frequencies likewise change. In this work modular investigation is utilized to decide the delamination in the composite structure. This is finished by making a four-layer multi directional overlay of E-Glass/Epoxy in ANSYS 15.0. A parametric report is led by changing length of the delamination in the center layer by shifting limit conditions. The outcomes got from the numerical displaying is approved with the outcomes acquired from the explanatory demonstrating in view of the transverse vibration of the composite shaft for the settled free, basic, settled limit conditions.Harmonic analysis is done to observe the resonating and anti-resonating peaks for the intact composite beam and delaminated composite beam with fixed-free, simple-simple, fixed-fixed boundary condition. Amplitude values of the beam also obtained from this harmonic analysis by varying the length of the delamination for the beams with different boundary conditions