NASA ROTOR 37 CFD CODE Validation Glenn-HT Code

In order to advance the goals of Aeronautics Programs at NASA, it is necessary to continuously improve the computational tools used for research and design at NASA. One such code is the Glenn-HT code which is used at NASA Glenn Research Center for turbomachinery computations and in particular for turbine heat transfer computations. For this exercise, a data set measuring various quantities of interest in compressor flows is used. The results presented here are in good agreement with this data. Most of the measures of performance are well within the measurement uncertainties and the exit profiles of interest agree with the experimental measurements.