Film Cooling Effectiveness Distribution on a Gas Turbine Blade Platform with Inclined Slot Leakage and Discrete Film Hole Flows.
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American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
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Effectiveness Distributions on Turbine Blade Cascade Platforms through Simulated Stator-Rotor Seals
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Turbine Blade Platform Film Cooling with Typical Stator-Rotor Purge Flow and Discrete-Hole Film Cooling.
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Effect of Flow Parameter Variations on Full Coverage Film-Cooling Effectiveness for a Gas Turbine Blade.
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Numerical Study of a Rotating Blade Platform with Cooling From Cavity Purge Flow in a 1-1/2 Turbine Stage.
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