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Composite Materials Research Progress

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F peak [kN]<br />

16<br />

14<br />

12<br />

10<br />

8<br />

6<br />

4<br />

2<br />

0<br />

Damage Variables in Impact Testing of <strong>Composite</strong> Laminates 249<br />

1 4 7 10 13 16 19 22 25 28 31 34 37 40<br />

Impact Number<br />

GVP90_12.31<br />

CE90m_4.00<br />

Figure 9. Values of peak force in repeated impact tests performed on GVP90_12.31 and CE90m_4.00<br />

laminates. Impact energy: 25 J.<br />

F peak [kN]<br />

30<br />

25<br />

20<br />

15<br />

10<br />

5<br />

0<br />

1 3 5 7 9 11 13 15 17 19<br />

Impact Number<br />

GVP90_12.31<br />

CE90m_4.00<br />

Figure 10. Values of peak force in repeated impact tests performed on GVP90_12.31 and CE90m_4.00<br />

laminates. Impact energy: 98 J.<br />

Figures 11-12 report data in terms of the DuI. As in Figure 5, for impact tests with<br />

rebound, contribution of Einitiation and Epropagation is calculated according to the definition<br />

illustrated in Figure 4b. Figure 11 shows that for impact energies that cause no perforation,<br />

the DuI is very low and constant throughout the test, signaling no significant damage

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