Vibration-based Structural Health Monitoring is a method to assess damage in structures, working in the principle that variations on the stiffness, mass or energy dissipation properties of the structure will alter its dynamic response. Composite laminate and sandwich structures are more often used in aircraft components. Composite damage features peculiar mechanisms, the most relevant being layer delamination in laminates, skin debounding in sandwich constructions and composite penetration. Delamination and debounding may be internal to the structure and not visible externally render difficult their assessment. These damage mechanisms will change the dynamic response of the structure that may be used to identify damage.
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