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. 2015 Mar 6;373(2036):20130157. doi: 10.1098/rsta.2013.0157

Figure 10.

Figure 10.

Fibre bridging stresses for the SiC fibres bridging a fatigue crack in a Ti–6Al–4V/35% SiC long-fibre composite holding the crack shut at Kmax (filled symbols, continuous lines) and propping it open at Kmin (open symbols, dashed curves). The far-field thermal contraction mismatch residual stresses in the fibres are represented by the horizontal dashed line. (After [50].) (Online version in colour.)