Heat Transfer for the Film Cooled Vane of a 1 1 2 Stage High Pressure Transonic Turbine Part II Effect of Cooling Variation on the Vane Airfoil and Inner Endwall


Kahveci H. S. , Haldeman C., Mathıson R., Dunn M.

ASME Turbo Expo 2011, Volume 5: Heat Transfer, Parts A and B, Vancouver, Canada, 6 - 10 June 2011, vol.5, pp.1735-1744 identifier

  • Publication Type: Conference Paper / Full Text
  • Volume: 5
  • Doi Number: 10.1115/gt2011-46573
  • City: Vancouver
  • Country: Canada
  • Page Numbers: pp.1735-1744