Numerical Prediction of Film Cooling and Heat Transfer on the Leading Edge of a Rotating Blade with Two Rows Holes in a 1-1/2 Turbine Stage at Design and Off Design Conditions.
類似資料:
American Society of Mechanical Engineers |
The American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
The American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
10
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Flow and Heat Transfer Prediction On Turbine Rotor Blade with Various Tip Configurations
American Institute of Aeronautics and Astronautics |
5
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Numerical Study of a Rotating Blade Platform with Cooling From Cavity Purge Flow in a 1-1/2 Turbine Stage.
American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
12
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Convective Heat Transfer Through Film Cooling Holes of a Gas Turbine Blade Leading Edge.
American Society of Mechanical Engineers |