High-Resolution Film Cooling Effectiveness Comparison of Axial and Compound Angle Holes on the Suction Side of a Turbine Vane
Journal of turbomachinery ; 129 , 2
2007
Aufsatz (Zeitschrift)
Englisch
Film-Cooling on a Gas Turbine Blade Pressure Side or Suction Side With Compound Angle Shaped Holes
Online Contents | 2009
|Deposition Near Film Cooling Holes on a High Pressure Turbine Vane
Online Contents | 2012
|