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Composite Materials Research Progress

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176<br />

Giangiacomo Minak and Andrea Zucchelli<br />

the corresponding experimental values, while in table 3 the ultimate strain and stress values<br />

are reported.<br />

Table 2. Theoretical calculation and experimental measure of Elastic modulus of each<br />

laminate type<br />

Ex (MPa)<br />

Theoretical Experimental<br />

ID M.V. M.V. S.D.<br />

UD 197000 190000 16000<br />

AP 23000 22000 3000<br />

QI1 75000 74000 6000<br />

QI2 75000 76000 3000<br />

QI3 77000 78000 3000<br />

Table 3. Ultimate strain and stress values of tested laminates<br />

Ultimate Strain Ultimate Stress (MPa)<br />

ID M.V. S.D. M.V. S.D.<br />

UD 0.019 0.001 2157 104<br />

AP 0.084 0.008 62 7<br />

QI1 0.012 0.002 571 35<br />

QI2 0.010 0.001 600 44<br />

QI3 0.012 0.001 322 19<br />

The main acoustic parameters that have been considered are: counts per AE event and AE<br />

event energy (Ea). Both parameters have been related by means of double entry diagram with<br />

the stress-strain behaviour. In the following figures 6-10 examples of these diagrams, one for<br />

each type of laminate, are reported.

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