In this paper, stress-intensity factors and load-line displacements have been calculated for chevron-notched bar and rod-fracture specimens using a three-dimensional finite-element analysis. Both specimens were subject to simulated wedge loading (either uniform applied displacement or uniform applied load). The chevron-notch sides and crack front were assumed to be straight. Crack-length-to-specimen width ratios (a/w) ranged from 0.4 to 0.7. The width-to-thickness ratio (w/B) was 1.45 or 2. The bar specimen had a height-to-width ratio of 0.435 or 0.5. Finite-element models were composed of singularity elements around the crack front and 8-noded isoparametric elements elsewhere. The models had about 11 000 degrees of freedom. Stress-intensity factors were calculated by using a nodal-force method for distribution along the crack front and by using a compliance method for average values. The stress-intensity factors and load-line displacements are presented and compared with experimental solutions from the literature. The stress-intensity factors and load-line displacements were about 2.5 and 5% lower than the reported experimental values, respectively.