Goals For Next Reporting Period

1) Conduct Phase III experiments with non-zero pressure gradients.

2) Prepare all required parts and instrumentation for Phase IV testing in the AFRL Turbine Research Facility.

3) Extend the validation of the discrete-element roughness model for heat transfer capability (Stanton number) using the results of Phase II and Phase III.


During the past six months, two documents have been generated (one by AFIT and one by MSU) which give a comprehensive summary of the experimental and computational results to date. Rather than attempt to "resummarize" these reports, they are attached and constitute the full progress report for this period.

Real Surface Effects on Turbine Heat Transfer and Aerodynamic Performance

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