The principles of stereoscopic particle image velocimetry (PIV), including
distortion compensation, were applied to the turbulent flow in a vessel sti
rred by a Rushton turbine. An angular offset configuration was used and til
t-axis lens mounts were incorporated in order to satisfy the Scheimpflug co
ndition, significantly reducing the ordinarily large depth of field require
ments of such configurations. A distortion compensation procedure, or in si
tu calibration, was utilized in place of the ray tracing, or mechanical reg
istration, used in previous studies. The calibration procedure was validate
d using two tests, one a rigid translation of a speckle target, the other t
he viscous flow between two concentric cylinders. The results of the tests
suggest the success with which the distortion compensation procedure may be
applied to real fluid flows. Phase-locked instantaneous data were ensemble
averaged and interpolated in order to obtain mean 3-D velocity fields on a
cylindrical shell enclosing the turbine blade. From these fields, the tip
vortex pairs and the radial jet documented in previous studies of mixer flo
ws were easily identified.