Turbine Blade Platform Film Cooling with Typical Stator-Rotor Purge Flow and Discrete-Hole Film Cooling.
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American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
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Effect of a Cutback Squealer and Cavity Depth on Film-Cooling Effectiveness for a Gas Turbine Blade Tip
American Institute of Aeronautics and Astronautics |
American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
American Institute of Aeronautics and Astronautics |
American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
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Aerothermal Impact of Stator-Rim Purge Flow and Rotor-Platform Film Cooling on a Transonic Turbine Stage.
American Society of Mechanical Engineers |
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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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