TY - GEN
T1 - Study of low velocity impact damage in CFRP laminates using 3D computed tomography
AU - Demerath, B. M.
AU - Zhupanska, O. I.
N1 - Publisher Copyright:
Copyright © 2015 by DEStech Publications, Inc. and American Society for Composites. All rights reserved.
PY - 2015
Y1 - 2015
N2 - In this work low velocity impact damage in IM7/977-3 carbon fiber reinforced polymer (CFRP) composites has been investigated using 3D computed tomography (CT). 32-ply IM7/977-3 symmetric cross-ply composites were impacted at different impact energy levels and with different impactors (flat-ended cylindrical and hemispherical) using an Instron 8200 Dynatup drop-weight impact machine. Impact energy was chosen to produce slight damage, which was characterized by the small crack on the front, impacted side and small visible delamination on the back, nonimpacted side of the specimens, and barely visible damage, which was characterized by slight indentation on the impacted side, but no visible delamination on the back side of the specimens. The difference in the impact energy to produce these types of damage was about 30%. Internal impact damage was assessed using ZEISS METROTOM 1500 CT scanning system. CT images were reconstructed using VGStudio MAX. To determine the extent of the damage zone, impacted 6 in by 6 in composite specimens were scanned first. As the relatively large specimen size did not allow for detailed evaluation of damage (internal cracks and delaminations were not visible), smaller 45 mm by 45 mm specimens, with enclosed impact damage zones, were cut out and analyzed. The CT imaging results showed that volume of the impact damage zone had a positive correlation with impact energy, maximum load and maximum deflection, but that relationship was generally weak. Absence of noticeable correlation between damage volume and impact energy was unexpected as the difference in the impact energy was up to 30%.
AB - In this work low velocity impact damage in IM7/977-3 carbon fiber reinforced polymer (CFRP) composites has been investigated using 3D computed tomography (CT). 32-ply IM7/977-3 symmetric cross-ply composites were impacted at different impact energy levels and with different impactors (flat-ended cylindrical and hemispherical) using an Instron 8200 Dynatup drop-weight impact machine. Impact energy was chosen to produce slight damage, which was characterized by the small crack on the front, impacted side and small visible delamination on the back, nonimpacted side of the specimens, and barely visible damage, which was characterized by slight indentation on the impacted side, but no visible delamination on the back side of the specimens. The difference in the impact energy to produce these types of damage was about 30%. Internal impact damage was assessed using ZEISS METROTOM 1500 CT scanning system. CT images were reconstructed using VGStudio MAX. To determine the extent of the damage zone, impacted 6 in by 6 in composite specimens were scanned first. As the relatively large specimen size did not allow for detailed evaluation of damage (internal cracks and delaminations were not visible), smaller 45 mm by 45 mm specimens, with enclosed impact damage zones, were cut out and analyzed. The CT imaging results showed that volume of the impact damage zone had a positive correlation with impact energy, maximum load and maximum deflection, but that relationship was generally weak. Absence of noticeable correlation between damage volume and impact energy was unexpected as the difference in the impact energy was up to 30%.
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M3 - Conference contribution
AN - SCOPUS:84966460649
T3 - Proceedings of the American Society for Composites - 30th Technical Conference, ACS 2015
BT - Proceedings of the American Society for Composites - 30th Technical Conference, ACS 2015
A2 - Xiao, Xinran
A2 - Liu, Dahsin
A2 - Loos, Alfred
PB - DEStech Publications
T2 - 30th Annual Technical Conference of the American Society for Composites, ASC 2015
Y2 - 28 September 2015 through 30 September 2015
ER -