Film-Cooling Effectiveness on Squealer Rim Walls and Squealer Cavity Floor of a Gas Turbine Blade Tip Using Pressure Sensitive Paint.
類似資料:
American Society of Mechanical Engineers |
7
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 |
8
テクニカルペーパー
Effect of Flow Parameter Variations on Full Coverage Film-Cooling Effectiveness for a Gas Turbine Blade.
American Society of Mechanical Engineers |
3
テクニカルペーパー
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 |
10
テクニカルペーパー
Film Cooling Effectiveness on the Leading Edge of a Rotating Film-Cooled Blade Using Pressure Sensitive Paint.
American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
American Institute of Aeronautics and Astronautics |
American Society of Mechanical Engineers |
12
テクニカルペーパー
Film Cooling Effectiveness on a Rotating Turbine Platform Using Pressure Sensitive Paint Technique.
American Society of Mechanical Engineers |