Effect of Unsteady Wake on Film-Cooling Effectiveness Distribution on a Gas Turbine Blade with Compound Shaped Holes.
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American Society of Mechanical Engineers |
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Effect of Flow Parameter Variations on Full Coverage Film-Cooling Effectiveness for a Gas Turbine Blade.
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 |
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Turbine Blade Platform Film Cooling with Typical Stator-Rotor Purge Flow and Discrete-Hole Film Cooling.
American Society of Mechanical Engineers |
American Institute of Aeronautics and Astronautics |
American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
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テクニカルペーパー
Effect of Unsteady Wake on Full Coverage Film-Cooling Effectiveness for A Gas Turbine Blade
American Institute of Aeronautics and Astronautics |
American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
12
テクニカルペーパー
Unsteady wake effect on film temperature and effectiveness distributions for a gas turbine blade
The American Society of Mechanical Engineers |