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
  • Middle East Technical University Affiliated: No