In previous years, significant progresses have been made in understanding failure mechanisms of composite materials such as delamination and fiber–-matrix breakage. Delaminations, which can arise during the manufacturing process or as a consequence of impacts from foreign objects, are probably the most investigated mode of failure in composite laminates. However, others damages such as matrix cracks, fiber–-matrix debonding, and fiber fractures can also appear in composite structures under service conditions. These different damage mechanisms are able to interact with each other and lead to a considerable reduction in stiffness and strength of local critical areas and consequently to the reduction of the load-carrying capability of the entire composite structure. These interactions can have a relevant role in particular for delaminated composite plates under compression. In this chapter, integrated numerical methodologies, considering simultaneously the presence of different damage mechanisms in composites, are presented.

Detailed Methodologies for Integrated Delamination Growth and Fiber-Matrix Damage Progression Simulation

Raimondo, Antonio
2015-01-01

Abstract

In previous years, significant progresses have been made in understanding failure mechanisms of composite materials such as delamination and fiber–-matrix breakage. Delaminations, which can arise during the manufacturing process or as a consequence of impacts from foreign objects, are probably the most investigated mode of failure in composite laminates. However, others damages such as matrix cracks, fiber–-matrix debonding, and fiber fractures can also appear in composite structures under service conditions. These different damage mechanisms are able to interact with each other and lead to a considerable reduction in stiffness and strength of local critical areas and consequently to the reduction of the load-carrying capability of the entire composite structure. These interactions can have a relevant role in particular for delaminated composite plates under compression. In this chapter, integrated numerical methodologies, considering simultaneously the presence of different damage mechanisms in composites, are presented.
2015
Damage Growth in Aerospace Composites
9783319040035
9783319040042
Energy Release Rate
Growth Initiation
Plane Displacement
Progressive Damage
Stiffened Panel
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11311/1290833
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