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Composite Materials Research Progress

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D<br />

Damage Evaluation and Residual Strength Prediction of CFRP Laminates … 191<br />

1.0<br />

0.9<br />

0.8<br />

0.7<br />

0.6<br />

0.5<br />

0.4<br />

0.3<br />

0.2<br />

0.1<br />

0.0<br />

0.000 0.002 0.004 0.006 0.008 0.010 0.012 0.014<br />

Strain<br />

Figure 20. Damage for QI3 laminate types.<br />

Case study 2: materials and method<br />

Eighteen graphite/epoxy composite square laminate plates 250x250 mm 2 were studied.<br />

Their thickness was 1.6 mm. They have been made in autoclave from pre-pregs by stacking<br />

eight unidirectional plies with quasi-isotropic orientations [0,90,45,-45]s.<br />

The specimens were placed in a circular clamping fixture with an internal diameter of<br />

200 mm and they were loaded at the centre: an hemispherical hardened steel ball with a radius<br />

of 7 mm was indented in the top centre point of the laminate by means of a servo-hydraulic<br />

Instron 8033 testing machine controlled by an MTS Teststar II system and equipped by a<br />

25kN load cell.<br />

The specimens were loaded monotonically out-of-plane in control of displacement and<br />

the head speed was 0.05 mm/s.<br />

The tests were stopped at three different damage levels, one (Low) corresponding to the<br />

load value of 2 kN, the second (Medium) corresponding to the first load drop in the loaddisplacement<br />

curve and the third (High) to the complete perforation of the plate.<br />

During the test, the AE has been monitored by a Physical Acoustic Corporation (PAC)<br />

PCI-DSP4 device with four transducers PAC R15 setting up the amplitude threshold at 40 dB.<br />

In figure 21a it is possible to see the fixture system equipped with AE piezoelectric<br />

sensors and in figure 21b the complete experimental setup.<br />

After each quasi-static test, the damaged plate was sliced by a diamond saw to obtain<br />

tensile specimens with the same geometry suggested by ASTM D 5766 for open hole testing<br />

of CFRP, a width of 40 mm and a length of 250 mm. The indented zone was in the centre of<br />

these tensile specimens and the whole damaged zone was included in the specimen width.<br />

The damaged zones size was previously identified by means of the localization tool of the<br />

AE system as it is shown in figure 22 for the High damage level.<br />

QI3

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