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. 2018 Feb 16;18(2):609. doi: 10.3390/s18020609

Figure 24.

Figure 24

SMArt multifunctional laminate: time history of the temperature difference variation between damaged and undamaged part (4 plies CFRP in cross-ply stacking sequence, single damage) (a); phase profile of two different damage sites (16 plies, cross-ply stacking sequence, multi-damage) (b), with permission from [34].