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Composite Materials Research Progress

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252<br />

DD, DI<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 />

Maria Pia Cavatorta and Davide Salvatore Paolino<br />

y = 1.1E-01x + 3.2E-01<br />

R 2 = 1.00<br />

1 2 3 4 5<br />

Impact Number<br />

DD DI<br />

Figure 14a. Comparison between DD and DI data in repeated impact tests performed on CE90m_4.00<br />

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

DD, DI<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 />

y = 9.3E-03x + 1.9E-01<br />

R 2 = 0.96<br />

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

Impact Number<br />

DD DI<br />

Figure 14b. Comparison between DD and DI data in repeated impact tests performed on GVP90_12.31<br />

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

Figure 14a reports data for the CE90m_4.00 laminate tested at an impact energy of 98J.<br />

Perforation is achieved at the 5 th impact. As it can be observed, the DD constantly increases<br />

impact after impact to reach a value of about one at the 4 th impact, where laminate penetration<br />

is achieved. DI values increase at a constant rate up to the 3 rd impact to then grow very<br />

rapidly and reach the value of one at laminate perforation. This trend is more evident in<br />

Figure 14b, for which perforation is achieved at the 19 th impact. Up to the 17 th impact, the DI<br />

slowly increases at a constant rate impact after impact. In the last two impacts before

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