Adiabatic Wall Effectiveness Measurements of Film-Cooling Holes With Expanded Exits
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[1] D. Bogard,et al. Film-cooling effectiveness downstream of a single row of holes with variable density ratio , 1990 .
[2] Y. Makki,et al. An experimental study of film cooling from diffused trapezoidal shaped holes , 1986 .
[3] C. Liess,et al. Experimental Investigation of Film Cooling With Ejection From a Row of Holes for the Application to Gas Turbine Blades , 1975 .
[4] Achmed Schulz,et al. TRANSONIC FILM-COOLING INVESTIGATIONS:EFFECTS OF HOLE SHAPES AND ORIENTATIONS , 1996 .
[5] B. R. Haller,et al. Aerodynamic Loss Penalty Produced by Film Cooling Transonic Turbine Blades , 1984 .
[6] Achmed Schulz,et al. Effect of a Crossflow at the Entrance to a Film-Cooling Hole , 1997 .
[7] E. E. Zukoski,et al. A Study of the Interaction of Gaseous Jets from Transverse Slots with Supersonic External Flows , 1968 .
[8] R. J. Goldstein,et al. Effects of hole geometry and density on three-dimensional film cooling , 1974 .
[9] Achmed Schulz,et al. In Situ Calibration for Quantitative Infrared Thermography , 1996 .
[10] David G. Bogard,et al. Film Cooling With Compound Angle Holes: Heat Transfer , 1994 .
[11] D. Lampard,et al. Effect of Crossflows on the Discharge Coefficient of Film Cooling Holes , 1983 .
[12] Achmed Schulz,et al. Flowfield Measurements for Film-Cooling Holes With Expanded Exits , 1998 .
[13] D. Bogard,et al. Film Cooling With Compound Angle Holes: Adiabatic Effectiveness , 1994 .
[14] David G. Bogard,et al. Effects of Surface Roughness on Film Cooling , 1996 .
[15] D. Lampard,et al. The Discharge Coefficient of Flared Film Cooling Holes , 1995 .