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Composite Materials Research Progress

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Damage Variables in Impact Testing of <strong>Composite</strong> Laminates 247<br />

Interestingly, up to Pn the DI increases linearly with the impact energy to then grow quite<br />

abruptly over the range of the penetration process. A linear relationship also exists between<br />

the DD data and the impact energy; however, the DD data can not be used beyond penetration<br />

as (by definition) the DD stays at the value of one over the entire range of the penetration<br />

process.<br />

DI<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 />

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 />

GVP90_12.31 GE90s_8.00<br />

GE90m_8.00 GE45_4.50<br />

GE90s_4.00 GE90m_4.00<br />

CE60_1.75 CE90_1.55<br />

CE60_0.85 CE90_0.75<br />

CE60_0.40 CE90_0.35<br />

0.0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0<br />

E i/P n<br />

Figure 6. DI values plotted against non-dimensional impact energy E i/P n<br />

y = 0.68x + 0.28<br />

R 2 = 0.96<br />

y = 0.52x - 0.14<br />

R 2 = 0.99<br />

0.0 0.2 0.4 0.6 0.8 1.0 1.2 1.4 1.6 1.8 2.0<br />

E i/P n<br />

DD DI<br />

Figure 7. Comparison between DD and DI values for impact tests on glass/epoxy 6.25 mm thick<br />

laminates. Impact data taken from reference [17].

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