Composite Materials Research Progress
Composite Materials Research Progress
Composite Materials Research Progress
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Damage Variables in Impact Testing of <strong>Composite</strong> Laminates 253<br />
perforation, the increase is on the contrary very rapid. Differently from the DuI which keeps<br />
to a constant low level up to a few impacts before perforation (Figure 12), the DI allows to<br />
monitor the initial phase of steady damage accumulation helping foreseen perforation. The<br />
initial slow decrease of DD values from the first to the second impact is followed by a<br />
constant phase up to the 17 th impact, after which the DD increases rapidly and reaches a value<br />
of one at perforation. Likewise the DuI, DD data are not very sensitive for predicting laminate<br />
perforation as, apart from the last 2-3 impacts, the constant phase of Figure 14b does not<br />
differ from the asymptotic trends of Figures 13a and 13b, where no perforation is achieved.<br />
Also, DD values at the first impact are about the same, regardless of the level of impact<br />
energy.<br />
Conclusion<br />
Impact test data obtained on different laminates are used to compare damage variables which<br />
have been proposed in the literature over the years. To this aim, definition of the two energy<br />
contributions used to compute the DuI has been extended to analyze impact tests with<br />
rebound.<br />
In single impact tests performed at different impact energies, data for Fpeak and DuI point<br />
out the existence of an impact energy threshold at about 40-50% Pn, below which the energy<br />
absorption mechanism is mainly matrix cracking. Graphs of Fpeak vs. impact energy show a<br />
bi-linear trend with a change in slope around the energy threshold; while values of the DuI are<br />
almost null below the energy threshold to then increase quite abruptly up to penetration.<br />
Interestingly, the energy threshold is about the same for all the laminates analyzed in the<br />
study, whose thickness varies from tenths to tens of millimeters. DI data increase<br />
monotonically for increasing impact energies and show very limited scattering up to the<br />
energy threshold. DD values and data in the Master Curve give no indications on the laminate<br />
damage tolerance; rather, they provide a measure of the absorption capability of the laminate.<br />
Results show that thicker laminates are characterized by a higher efficiency of energy<br />
absorption.<br />
Main advantage of the DI variable is the possibility to distinguish between the<br />
penetration and perforation energy thresholds. The distinction is essential when dealing with<br />
thick laminates, for which the impact energy that causes laminate perforation can by far<br />
exceed the penetration energy. In the range of the penetration process, the DI effectively<br />
monitors the impactor moving deeper and deeper into the laminate.<br />
Also in case of repeated impact tests, the DI provides important pieces of information.<br />
For impact energies that cause no laminate perforation within test duration, the DI stays at a<br />
constant low value throughout the test, owing to a negligible damage accumulation besides<br />
initial laminate indentation. For impact energies that cause perforation, the DI shows an initial<br />
phase of linear growth with the number of impacts, owing to a steady accumulation of<br />
damage. A few impacts before perforation, the DI starts raising quite abruptly, helping<br />
foreseeing laminate failure.<br />
Results for Fpeak show that it maintains a constant value when perforation is not achieved<br />
while it decreases rapidly otherwise. However, graphs of Fpeak versus impact number do not<br />
signal any change in the rate of damage accumulation. DuI values are almost null throughout<br />
the test when no perforation occurs. Low and constant values also characterize tests at higher