Experimental and Numerical Investigations of Effects of Flow Control Devices Upon Flat-Plate Film Cooling Performance.

This study deals with the experimental and numerical studies of the effect of flow control devices (FCDs) on the film cooling performance of a circular cooling hole on a flat plate. Two types of FCDs with different heights are examined in this study, where each of them is mounted to the flat plate upstream of the cooling hole by changing its lateral position with respect to the hole centerline. In order to measure the film effectiveness as well as heat transfer downstream of the cooling hole with upstream FCD, a transient method using a high-resolution infrared camera is adopted. The velocity field downstream of the cooling hole is captured by 3D laser Doppler velocimeter (LDV). Furthermore, the aerodynamic loss associated with the cooling hole with/without FCD is measured by a total pressure probe rake. The experiments are carried out at blowing ratios ranging from 0.5 to 1.0. In addition, numerical simulations are also made to have a better understanding of the flow field. LES approach is employed to solve the flow field and visualize the vortex structure around the cooling hole with FCD. When a taller FCD is mounted to the plate, the film effectiveness tends to increase due to the vortex structure generated by the FCD. As FCD is laterally shifted from the centerline, the film effectiveness increases, while the lift-off of cooling air is also promoted when FCD is put on the center line.

[1]  A. Schulz,et al.  Comparison the Cooling Performance of Cylindrical and Fan-Shaped Cooling Holes With Special Emphasis on the Effect of Internal Coolant Cross-Flow , 2008 .

[2]  R. Abhari,et al.  Aerothermal Performance of Streamwise and Compound Angled Pulsating Film Cooling Jets , 2009 .

[3]  Giuseppe Franchini,et al.  The Effect of an Upstream Ramp on Cylindrical and Fan-Shaped Hole Film Cooling: Part II — Adiabatic Effectiveness Results , 2007 .

[4]  Christian Saumweber,et al.  Free-Stream Effects on the Cooling Performance of Cylindrical and Fan-Shaped Cooling Holes , 2008 .

[5]  Toshihiko Takahashi,et al.  Experimental Study on Effects of Internal Rib and Rear Bump on Film Effectiveness , 2012 .

[6]  K. Funazaki,et al.  Experimental Investigations on Aero-Thermal Interaction of Film Cooling Airs Ejected From Multiple Holes: Shallow Hole Angle , 2012 .

[7]  Giuseppe Franchini,et al.  The Effect of an Upstream Ramp on Cylindrical and Fan-Shaped Hole Film Cooling: Part I — Aerodynamic Results , 2007 .

[8]  Y. W. Kim,et al.  Darryl E. Metzger Memorial Session Paper: A Summary of the Cooled Turbine Blade Tip Heat Transfer and Film Effectiveness Investigations Performed by Dr. D. E. Metzger , 1995 .

[9]  R. J. Goldstein,et al.  Effects of hole geometry and density on three-dimensional film cooling , 1974 .

[10]  Tom Shih,et al.  Increasing adiabatic film-cooling effectiveness by using an upstream ramp , 2007 .

[11]  Srinath V. Ekkad,et al.  Improved film cooling from cylindrical angled holes with triangular tabs: effect of tab orientations , 2003 .

[12]  S. J. Kline,et al.  Describing Uncertainties in Single-Sample Experiments , 1953 .

[13]  M. Kurosaka,et al.  Anti-Kidney Pair of Vortices in Shaped Holes and Their Influence on Film Cooling Effectiveness , 1997 .