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):011019-011019-11. doi:10.1115/1.2813012 Figure Legend: Schematic of the cascade with film-cooled blade
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):011019-011019-11. doi:10.1115/1.2813012 Figure Legend: Film-cooled blades with compound angle laidback fan-shaped holes
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):011019-011019-11. doi:10.1115/1.2813012 Figure Legend: Wake rod phase locations and conceptual view of wake effect on the test blade
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):011019-011019-11. doi:10.1115/1.2813012 Figure Legend: Optical component setup
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):011019-011019-11. doi:10.1115/1.2813012 Figure Legend: Mach number distribution for the case of no wake
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):011019-011019-11. doi:10.1115/1.2813012 Figure Legend: Mach number distribution under the influence of upstream wake rods
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):011019-011019-11. doi:10.1115/1.2813012 Figure Legend: Film-cooling effectiveness distribution for the PS coolant ejection at wake rod phase 0%
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):011019-011019-11. doi:10.1115/1.2813012 Figure Legend: Film-cooling effectiveness distribution for the SS coolant ejection at wake rod phase 25%