Film cooling effectiveness distribution of cylindrical hole injections at different locations on a vane endwall

[1]  Je-Chin Han,et al.  Effect of Upstream Wake With Vortex on Turbine Blade Platform Film Cooling With Simulated Stator-Rotor Purge Flow , 2009 .

[2]  A. E. Forest,et al.  Aerodynamic Investigation of Endwall Film-Cooling in an Axial Turbine Cascade Part I: Experimental Investigation , 1999 .

[3]  Howard P. Hodson,et al.  AERODYNAMIC ASPECTS OF ENDWALL FILM-COOLING , 1997 .

[4]  H. Hodson,et al.  Distribution of Film-Cooling Effectiveness on a Turbine Endwall Measured Using the Ammonia and Diazo Technique , 1995 .

[5]  Kenichiro Takeishi,et al.  Effect of Endwall Film Cooling Upstream of an Airfoil/Endwall Junction to Suppress the Formation of Horseshoe Vortex in a Symmetric Airfoil , 2013 .

[6]  L. M. Russell,et al.  Experimental determination of stator endwall heat transfer , 1990 .

[7]  A. Lefebvre,et al.  GAS TURBINE COMBUSTION—Alternative Fuels and Emissions , 2010 .

[8]  H. Hodson,et al.  Heat Transfer Committee Best Paper of 1995 Award: Distribution of Film-Cooling Effectiveness on a Turbine Endwall Measured Using the Ammonia and Diazo Technique , 1996 .

[9]  Thomas Povey,et al.  Experimental and CFD Studies of NGV Endwall Cooling , 2013 .

[10]  Je-Chin Han,et al.  Film Cooling Effectiveness Distributions on a Turbine Blade Cascade Platform With Stator-Rotor Purge and Discrete Film Hole Flows , 2008 .

[11]  G. Barigozzi,et al.  Fan-Shaped Hole Effects on the Aero-Thermal Performance of a Film Cooled Endwall , 2005 .

[12]  Karen A. Thole,et al.  Adiabatic Effectiveness Measurements of Endwall Film-Cooling for a First Stage Vane , 2004 .

[13]  Terrence W. Simon,et al.  Effects of Slot Bleed Injection Over a Contoured Endwall on Nozzle Guide Vane Cooling Performance: Part I — Flow Field Measurements , 2000 .

[14]  Luzeng J. Zhang,et al.  The Effects of Vane Showerhead Injection Angle and Film Compound Angle on Nozzle Endwall Cooling (Phantom Cooling) , 2015 .

[15]  Daniel G. Knost.  Predictions and Measurements of Film-Cooling on the Endwall of a First Stage Vane , 2003 .

[16]  Yang Zhang,et al.  Turbine Endwall Film Cooling With Pressure Side Radial Holes , 2013 .

[17]  Magnus Jonsson,et al.  Experimental and Numerical Study of the Thermal Performance of a Film Cooled Turbine Platform , 2009 .

[18]  Sunao Aoki,et al.  An Experimental Study of Heat Transfer and Film Cooling on Low Aspect Ratio Turbine Nozzles , 1990 .

[19]  Ikuo Okada,et al.  Development of Key Technologies for the Next Generation Gas Turbine , 2007 .

[20]  Bruno Facchini,et al.  Performance Improvement of a Heavy Duty GT: Adiabatic Effectiveness Measurements on First Stage Vanes in Representative Engine Conditions , 2014 .

[21]  Akhilesh P. Rallabandi,et al.  TURBINE BLADE FILM COOLING USING PSP TECHNIQUE , 2010 .

[22]  Sanjay M. Correa,et al.  Power generation and aeropropulsion gas turbines: From combustion science to combustion technology , 1998 .

[23]  Luzeng J. Zhang,et al.  Turbine Nozzle Endwall Film Cooling Study Using Pressure-Sensitive Paint , 2001 .

[24]  R. E. Gaugler,et al.  COMPARISON OF VISUALIZED TURBINE ENDWALL SECONDARY FLOWS AND MEASUREU HEAT TRAW ER PATTERNS , 2010 .

[25]  L. Langston,et al.  Three-Dimensional Flow Within a Turbine Cascade Passage , 1977 .

[26]  Bruno Facchini,et al.  Comparison between PSP and TLC steady state techniques for adiabatic effectiveness measurement on a multiperforated plate , 2013 .

[27]  M. F. Blair,et al.  An Experimental Study of Endwall and Airfoil Surface Heat Transfer in a Large Scale Turbine Blade Cascade , 1980 .

[28]  Howard P. Hodson,et al.  The Design of an Improved Endwall Film-Cooling Configuration , 1999 .

[29]  Karen A. Thole,et al.  Influence of flow injection angle on a leading-edge horseshoe vortex , 2012 .

[30]  Hugh W. Coleman,et al.  Experimentation and Uncertainty Analysis for Engineers , 1989 .