Existing solutions for stress intensity factor and crack mouth opening
displacement of three-point bend specimens are shown to overestimate
these quantities for shallow cracks by up to +/-4.5 percent, because t
hey do not account for the disturbance of the bending stress distribut
ion by the concentrated force at the loading point. This error is far
larger than the accuracy claimed by these solutions (0.2 to 0.5 percen
t). New expressions are therefore developed for stress intensity, crac
k mouth opening displacement and crack mouth open angle of single edge
notched bend specimens loaded in three-point bending. As a reference,
and to show the accuracy of the solutions, also the pure bending situ
ation is treated. Rigorously derived asymptotic solutions are used for
the shallow and deep crack limits, in order to prescribe both the pro
per limit values and gradients to the interpolation functions, of whic
h the intermediate values are derived from refined finite element anal
yses. The crack mouth opening angle solutions are primarily intended t
o facilitate crack mouth opening measurement at other locations then t
he specimen surface, i.e. at an offset from the specimen surface as is
the case when removable knife edges are applied. No solutions of the
crack mouth opening angle of three-point bend specimens were available
until now. For use with unloading compliance crack length measurement
, also an inverse crack mouth opening relation is developed. This also
includes crack mouth opening measurement at an offset from the specim
en surface, which is lacking in presently available expressions of thi
s kind.