Numerical Study of a Rotating Blade Platform with Cooling From Cavity Purge Flow in a 1-1/2 Turbine Stage.
類似資料:
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 |
American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
10
テクニカルペーパー
Flow and Heat Transfer Prediction On Turbine Rotor Blade with Various Tip Configurations
American Institute of Aeronautics and Astronautics |
American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
6
テクニカルペーパー
Turbine Blade Platform Film Cooling with Typical Stator-Rotor Purge Flow and Discrete-Hole Film Cooling.
American Society of Mechanical Engineers |
American Society of Mechanical Engineers |