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    Film Cooling Performance of a Turbine Vane Suction Side: The Showerhead Effect on Film Cooling Hole Placement for Cylindrical and Fan Shaped Holes 

    Source: Journal of Turbomachinery:;2015:;volume( 137 ):;issue: 009:;page 91005
    Author(s): Najafabadi, Hossein Nadali; Karlsson, Matts; Kinell, Mats; Utriainen, Esa
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this paper, the transient IRthermography method is used to investigate the effect of showerhead cooling on the filmcooling performance of the suction side of a turbine guide vane working under enginerepresentative ...
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    Shower Head and Trailing Edge Cooling Influence on Transonic Vane Aero Performance 

    Source: Journal of Turbomachinery:;2014:;volume( 136 ):;issue: 011:;page 111001
    Author(s): Saha, Ranjan; Fridh, Jens; Fransson, Torsten H.; Mamaev, Boris I.; Annerfeldt, Mats; Utriainen, Esa
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An experimental investigation on a cooled nozzle guide vane (NGV) has been conducted in an annular sector to quantify aerodynamic influences of shower head (SH) and trailing edge (TE) cooling. The investigated vane is a ...
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    Experimental Study on Pressure Losses in Circular Orifices for the Application in Internal Cooling Systems 

    Source: Journal of Turbomachinery:;2015:;volume( 137 ):;issue: 003:;page 31005
    Author(s): Binder, Christian; Kinell, Mats; Utriainen, Esa; Eriksson, Daniel; Bahador, Mehdi; Kneer, Johannes; Bauer, Hans
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The cooling air flow in a gas turbine is governed by the flow through its internal passages and controlled by restrictors such as circular orifices. If the cooling air flow is incorrectly controlled, the durability and ...
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