1. Date of download: 10/18/2017
Copyright © ASME. All rights reserved.
From: Film-Cooling on a Gas Turbine Blade Pressure Side or Suction Side With Compound Angle Shaped Holes
J. Turbomach. 2008;131(1): doi: /
Figure Legend:
Schematic of the cascade with film-cooled blade

2. Date of download: 10/18/2017
Copyright © ASME. All rights reserved.
From: Film-Cooling on a Gas Turbine Blade Pressure Side or Suction Side With Compound Angle Shaped Holes
J. Turbomach. 2008;131(1): doi: /
Figure Legend:
Film-cooled blades with compound angle laidback fan-shaped holes

3. Date of download: 10/18/2017
Copyright © ASME. All rights reserved.
From: Film-Cooling on a Gas Turbine Blade Pressure Side or Suction Side With Compound Angle Shaped Holes
J. Turbomach. 2008;131(1): doi: /
Figure Legend:
Wake rod phase locations and conceptual view of wake effect on the test blade

4. Date of download: 10/18/2017
Copyright © ASME. All rights reserved.
From: Film-Cooling on a Gas Turbine Blade Pressure Side or Suction Side With Compound Angle Shaped Holes
J. Turbomach. 2008;131(1): doi: /
Figure Legend:
Optical component setup

5. Date of download: 10/18/2017
Copyright © ASME. All rights reserved.
From: Film-Cooling on a Gas Turbine Blade Pressure Side or Suction Side With Compound Angle Shaped Holes
J. Turbomach. 2008;131(1): doi: /
Figure Legend:
Mach number distribution for the case of no wake

6. Date of download: 10/18/2017
Copyright © ASME. All rights reserved.
From: Film-Cooling on a Gas Turbine Blade Pressure Side or Suction Side With Compound Angle Shaped Holes
J. Turbomach. 2008;131(1): doi: /
Figure Legend:
Mach number distribution under the influence of upstream wake rods

7. Date of download: 10/18/2017
Copyright © ASME. All rights reserved.
From: Film-Cooling on a Gas Turbine Blade Pressure Side or Suction Side With Compound Angle Shaped Holes
J. Turbomach. 2008;131(1): doi: /
Figure Legend:
Film-cooling effectiveness distribution for the PS coolant ejection at wake rod phase 0%

8. Date of download: 10/18/2017
Copyright © ASME. All rights reserved.
From: Film-Cooling on a Gas Turbine Blade Pressure Side or Suction Side With Compound Angle Shaped Holes
J. Turbomach. 2008;131(1): doi: /
Figure Legend:
Film-cooling effectiveness distribution for the SS coolant ejection at wake rod phase 25%