This study evaluates the ability of available turbulence models in the commercial software FLUENT to predict film cooling effectiveness for a single row of short (L/D = 2.91) . film cooling holes fed by a narrow plenum (H /D = 1). The results are compared to experimental data obtained by the present investigators. The study concentrates on the near-hole region for the geometry being studied experimentally by the present investigators. The results of the study indicate that the use of wall functions to predict film cooling effectiveness in the near-hole region is inappropriate due to the boundary layer separation in that region. Also, the ability of the Reynolds Stress turbulence model to better predict spanwise spreading of the jet indicates the need for anisotropic turbulnce model capabilities to better predict film cooling effectiveness.
CITATION STYLE
Hale, C. A., Ramadhyani, S., & Plesniak, M. W. (1999). Film cooling effectiveness predictions for short holes fed by a narrow plenum. In Proceedings of the ASME Turbo Expo (Vol. 3). American Society of Mechanical Engineers (ASME). https://doi.org/10.1115/99-GT-162
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