ABSTRACT
In the present paper, investigation of the optimal angle for the holes on the leading edge of a gas turbine blade was carried out considering different blowing ratios in order to assess the local film cooling effectiveness. First, the suitability of different eddy viscosity models compared to experimental results was validated to predict local and average film cooling effectiveness. Computations were performed employing the self-developed object-oriented C++ programming in OpenFOAM CFD package. The realisable k–ε model predicted more accurate results compared to RNG k–ε and standard k–ε models for the average film cooling effectiveness since this model has a variable Cμ which causes sensitivity of this model to the mean flow and turbulence. The results obtained for the average film cooling effectiveness versus the different blowing ratios in the realisable k–ε model for holes oriented 20°, 25°, 30° and 35° showed that the holes at an angle of 25° have better performance in comparison to the other angles.
Subscript
inilnetaveaverage tturbulentxstram-wise direction yvertical direction zlateral direction ∞cross-flowccoolant
Disclosure statement
No potential conflict of interest was reported by the authors.
Additional information
Notes on contributors
Akbar Mohammadi-Ahmar
Akbar Mohammadi-Ahmar is a PhD candidate in Mechanical Engineering at the University of Tehran. His research interests are numerical modeling, CFD analysis, renewable energy and turbulence modeling.Ali Solati is a PhD candidate in Mechanical Engineering at the University of Tehran. His research interests are numerical modeling, laser material processing, renewable energy and CFD analysis. Jalal Ghasemi is an assistant professor in Mechanical Engineering at the University of Zanjan. His research interests are numerical modeling, CFD analysis and heat transfer.