Flexural failure of a unidirectional aramid SVM/epoxy composite was st
udied using two-point loading of half-ring specimens. Failure originat
ed near the compressive side of the specimen where several intersectin
g shear yield bands, similar to slip bands in metals, were observed. T
he angle between the yield bands and the loading direction was 45 +/-
2 degrees. The thickness of the yield bands grew proportionally to the
shear displacement of their opposite sides. The yield stress of the S
VM fibres in bending was equal to 500 MPa, which is close to the fibre
strength in pure axial compression of 400-450 MPa. The maximum failur
e stress of the composite in bending, 530 MPa, was approximately twice
as high as the strength of the composite under pure axial compression
(260-280 MPa). In bending the composite is elastic in the tensile par
t of the beam whilst the other, compressed, part is elastic-plastic.