Part II of this article presents results of a combined computational/e
xperimental investigation into the effects of stator-rotor interaction
on the heat transfer distributions on the vane and blade of a transon
ic turbine stage. The predictions were obtained using a two-dimensiona
l unsteady Navier-Stokes code described in Part I of this article. and
the measurements were acquired in a short-duration shock tunnel facil
ity. Twenty miniature thin-film heat flux button gauges were mounted a
t the midspan of the vane and blade, and contoured inserts containing
many thin-film gauges were used on the blade leading edge to spatially
resolve the heat transfer rates in that high-gradient region. A grid
refinement study was performed with steady noninteractive solutions to
ascertain the minimum grid size needed to obtain grid-independent sol
utions. Predicted time-averaged and phase-resolved heat transfer rates
are compared with measurements on the vane and blade.