The failure of transversely loaded unidirectional CFRP has been investigate
d by the use of mechanical and thermo-mechanical test methods and finite-el
ement analysis. The case considered here is characterized by a high interfa
cial strength between fiber and matrix, so that matrix failure governs the
fracture process of the composite. On the basis of the experimental results
, the parabolic and other failure criteria were applied to the FE calculati
ons. The failure dependence of the resin on the actual stress state could b
e described. Furthermore, the influence of thermal residual stresses on the
initial matrix failure has been investigated, and the actual stiffnesses a
nd thermal expansion changes of the epoxy resins and the composites as a fu
nction of temperature have been determined experimentally. The results of t
he mechanical and thermo-mechanical tests performed on the pure resins and
on the composites were incorporated into a finite-element analysis and comp
ared with the transverse tensile properties of the composite laminates. In
the FE analysis, the local fiber-volume fraction was varied over a wide ran
ge in order to investigate its influence on the thermal residual stresses a
nd transverse composite strength. The results could explain the low strain
to failure of transverse laminates under tensile loading. (C) 2000 Elsevier
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