Multirow Film Cooling Performances of a High Lift Blade and Vane

[1]  Karen A. Thole,et al.  A film-cooling correlation for shaped holes on a flat-plate surface , 2011 .

[2]  Achmed Schulz,et al.  Flowfield Measurements for Film-Cooling Holes With Expanded Exits , 1998 .

[3]  Ching-Pang Lee,et al.  Heat Transfer and Film Cooling Effectiveness in a Linear Airfoil Cascade , 1995 .

[4]  Tony Arts,et al.  Experimental heat transfer investigation around the film-cooled leading edge of a high-pressure gas turbine rotor blade , 1985 .

[5]  Achmed Schulz,et al.  Interactions of Film Cooling Rows: Effects of Hole Geometry and Row Spacing on the Cooling Performance Downstream of the Second Row of Holes , 2003 .

[6]  W. Colban,et al.  Experimental and Computational Comparisons of Fan-Shaped Film Cooling on a Turbine Vane Surface , 2007 .

[7]  N. V. Nirmalan,et al.  An experimental study of turbine vane heat transfer with leading edge and downstream film cooling , 1990 .

[8]  A. Bölcs,et al.  Investigation of Detailed Film Cooling Effectiveness and Heat Transfer Distributions on a Gas Turbine Airfoil , 1999 .

[9]  Robert J. Moffat,et al.  Describing the Uncertainties in Experimental Results , 1988 .

[10]  Phil Ligrani,et al.  Film Cooling From Shaped Holes , 2000 .

[11]  Achmed Schulz,et al.  Heat Transfer Coefficient Measurements of Film-Cooling Holes With Expanded Exits , 1998 .

[12]  Christian Saumweber,et al.  Interaction of film cooling rows: Effects of hole geometry and row spacing on the cooling performance downstream of the second row of holes , 2004 .

[13]  Achmed Schulz,et al.  Assessment of Various Film-Cooling Configurations Including Shaped and Compound Angle Holes Based on Large-Scale Experiments , 2003 .

[14]  P. Ligrani,et al.  Transonic Film Cooling Effectiveness from Shaped Holes on a Simulated Turbine Airfoil , 2002 .

[15]  Richard J Goldstein,et al.  Film cooling on a gas turbine blade near the end wall , 1985 .