Available expressions for load-line compliance and crack-mouth opening compliance expressions for standard three-point bend specimens (span over width ratio = 4) are assessed. It is concluded that none of the available expressions are able to reproduce the source data (boundary collocation results and theoretical limits for relative crack depths equal to 0 and 1) for the entire range of relative crack depth. New expressions for example are proposed and the accuracy of each is indicated. A by-product of the new expression for load-line compliance is a new, fully compatible stress intensity expression that is, consistent with the load line compliance expression as known from theoretical considerations. Also inverse expressions are presented which predicting the crack length from compliance. To improve the accuracy of such inverse expressions, a correction that results in a considerable error reduction is presented. NOMENCLATURE a = crack length B = specimen thickness C = load line compliance ( = A / P ) C, = load-line compliance of the uncracked specimen (= A J P ) C, = crack-mouth opening compliance ( = A m / P ) C,, = load-line compliance due to the presence of the crack only (= C -C,) E = modulus of elasticity E ' = effective modulus of elasticity [=E for plane stress, E/(l -v2) for plane strain] K = stress intensity factor (mode I) P = load S = specimen span W = specimen width a = relative crack depth ( = a / W ) 6,, =' transfer function used for inverse load-line compliance expressions 6 , = transfer function used for inverse crack-mouth opening compliance expressions A = load-line displacement Acr = load-line displacement due to the presence of the crack Anc = load-line displacement of uncracked specimen Acr = crack-mouth opening displacement v = Poisson's ratio