Influence of a Favorable Streamwise Pressure Gradient on Laminar Film Cooling at Mach 2 . 67

@inproceedings{Keller2011InfluenceOA,
  title={Influence of a Favorable Streamwise Pressure Gradient on Laminar Film Cooling at Mach 2 . 67},
  author={Michael Keller and Markus J. Kloker},
  year={2011}
}
Direct numerical simulations are used to investigate the me thod of film cooling in a laminar flat-plate Mach-2.67 boundary layer. Air is employed as mean-flow and coolant ga s and is introduced into the boundary layer through one row of holes by means of a modeled b lowing approach. The e ffects of a favorable streamwise pressure gradient are investigated… CONTINUE READING