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. 2017 Oct 11;473(2206):20170538. doi: 10.1098/rspa.2017.0538

Figure 8.

Figure 8.

Compressive stress distributions in helicoidal structures at different fibre–matrix modulus ratios of 0.2, 1 and 10. Scale bar (a) for contours at ratios of 0.2 and 1 and scale bar (b) for contours at a modulus ratio of 10. The top planes are contours of interlayer matrices, while the bottom planes are contours of rotated fibres. (Online version in colour.)