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    Cooling the Tip of a Turbine Blade Using Pressure Side Holes—Part II: Heat Transfer Measurements 

    Source: Journal of Turbomachinery:;2005:;volume( 127 ):;issue: 002:;page 278
    Author(s): J. R. Christophel; F. J. Cunha; K. A. Thole
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The clearance gap between a turbine blade tip and its associated shroud allows leakage flow across the tip from the pressure side to the suction side of the blade. Understanding how this ...
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    Cooling the Tip of a Turbine Blade Using Pressure Side Holes—Part I: Adiabatic Effectiveness Measurements 

    Source: Journal of Turbomachinery:;2005:;volume( 127 ):;issue: 002:;page 270
    Author(s): J. R. Christophel; F. J. Cunha; K. A. Thole
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Durability of turbine blade tips has been and continues to be challenging, particularly since increasing turbine inlet temperatures is the driver for improving turbine engine performance. As a ...
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    Measured Adiabatic Effectiveness and Heat Transfer for Blowing From the Tip of a Turbine Blade 

    Source: Journal of Turbomachinery:;2005:;volume( 127 ):;issue: 002:;page 251
    Author(s): J. R. Christophel; F. J. Cunha; E. Couch; K. A. Thole
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The clearance gap between the tip of a turbine blade and the shroud has an inherent leakage flow from the pressure side to the suction side of the blade. This leakage flow of combustion ...
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