Single-Hole Film Cooling on a Turbine-Blade Leading-Edge Model

@inproceedings{Mishra2007SingleHoleFC,
  title={Single-Hole Film Cooling on a Turbine-Blade Leading-Edge Model},
  author={Suman Mishra and Rohan Wanchoo and U. Ghia and K. Ghia},
  year={2007}
}
The present study numerically investigates the effectiveness of film cooling on a turbine blade leading-edge model through a single-hole coolant exit. The model used in this study has the same dimensions as that of an experimental investigation done earlier by Ekkad et al [1]. The cylindrical model, a half cylinder and a flat after-body attached to it, well represents the leading edge of a turbine blade. The half-cylinder is 88.9 mm in diameter with a length of 364 mm. The flat after-body is… Expand
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