Kahveci, H. S. Et Al. 2011. 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. ASME Turbo Expo 2011, Volume 5: Heat Transfer, Parts A and B , (Vancouver, Canada), 1735-1744.

Kahveci, H. S., Haldeman, C., Mathıson, R., & Dunn, M., (2011). 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 . ASME Turbo Expo 2011, Volume 5: Heat Transfer, Parts A and B (pp.1735-1744). Vancouver, Canada

Kahveci, HARİKA Et Al. "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," ASME Turbo Expo 2011, Volume 5: Heat Transfer, Parts A and B, Vancouver, Canada, 2011

Kahveci, HARİKA S. Et Al. "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." ASME Turbo Expo 2011, Volume 5: Heat Transfer, Parts A and B , Vancouver, Canada, pp.1735-1744, 2011

Kahveci, H. S. Et Al. (2011) . "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." ASME Turbo Expo 2011, Volume 5: Heat Transfer, Parts A and B , Vancouver, Canada, pp.1735-1744.

@conferencepaper{conferencepaper, author={HARİKA SENEM KAHVECİ Et Al. }, title={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}, congress name={ASME Turbo Expo 2011, Volume 5: Heat Transfer, Parts A and B}, city={Vancouver}, country={Canada}, year={2011}, pages={1735-1744} }