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 | AVESİS

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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

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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

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