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Cooling the Tip of a Turbine Blade Using Pressure Side Holes—Part II: Heat Transfer Measurements
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 ...
Cooling the Tip of a Turbine Blade Using Pressure Side Holes—Part I: Adiabatic Effectiveness Measurements
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 ...
Measured Adiabatic Effectiveness and Heat Transfer for Blowing From the Tip of a Turbine Blade
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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