Figure 3 | Scientific Reports

Figure 3

From: On the thermal shock resistance and mechanical properties of novel unidirectional UHTCMCs for extreme environments

Figure 3

(a) Lateral view of failed composite under flexural loading with longitudinal Cf orientation (0°). (b) Fracture surface of failed composite under flexural loading with transverse Cf orientation (90°). The possible fracture origin is highlighted by the circle. (c) Respective load-displacement curves of 4 point flexural strength for three different bars for each orientation. The adsorbed energy for each bar is reported.

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