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Composite Materials Research Progress

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30<br />

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a)<br />

Jacquemin Frédéric and Fréour Sylvain<br />

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AS4 50_1_1 ΔC m / ΔC I = 2<br />

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composite (CMF) matrix (numerical) fiber (numerical)<br />

matrix (analytical) fiber (analytical)<br />

Figure 4. Local stresses in T300/5208 composite for the inner ply, in the case of a) the uni-directionaly<br />

reinforced composite and b) the [+55°/-55°] S symmetric laminate. CMF stands for Continuum<br />

Mechanics Formalisms.<br />

This work demonstrates the complementarities of continuum mechanics and micromechanical<br />

models for the prediction of a possible damage in composite structures submitted<br />

to hygro-elastic loads.<br />

In the following section, the analytical expressions presented here for the localization of<br />

the macroscopic mechanical states within the plies constituents, will be inversed in order to<br />

achieve the identification of the strength of the constitutive matrix of a composite ply.<br />

5. Identification of the Local Strength of the Constitutive Matrix<br />

of a <strong>Composite</strong> Ply<br />

5.1. Introduction<br />

Damage predictions are important for design and for guiding materials improvement for<br />

engineering applications. <strong>Composite</strong> structures encountered in engineering applications

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