JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME - Texas A&M University (TAMU) Scholar

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Heat Transfer in Rotating, Trailing Edge, Converging Channels With Full- and Partial-Height Strip-Fins. 144:1-32. 2022
Heat Transfer in a Rotating, Blade-Shaped, Two-Pass Cooling Channel With a Variable Aspect Ratio. 144. 2022
Heat Transfer and Pressure Loss in a Two-Pass, Rectangular Channel Featuring a Reduced Cross-Sectional Area After the 180-Deg Tip Turn With Different Turning Vane Configurations. 143. 2021
Heat Transfer in a Rotating, Two-Pass, Variable Aspect Ratio Cooling Channel With Profiled V-Shaped Ribs. 143. 2021
Heat Transfer in Rotating, Trailing-Edge, Converging Channels With Smooth Walls and Pin-Fins. 143. 2021
Heat Transfer in Rotating, Trailing Edge, Converging Channels With Partial Length Pin-Fins. 143. 2021
Upstream Film Cooling on the Contoured Endwall of a Transonic Turbine Vane in an Annular Cascade. 143. 2021
Transonic Turbine Vane Endwall Film Cooling Using the Pressure-Sensitive Paint Measurement Technique. 142. 2020
Effect of 45-deg Rib Orientations on Heat Transfer in a Rotating Two-Pass Channel With Aspect Ratio from 4:1 to 2:1. 142. 2020
Heat Transfer in a Rotating Two-Pass Rectangular Channel Featuring Reduced Cross-Sectional Area After Tip Turn (Aspect Ratio = 4:1 to 2:1) With Profiled 60 deg Angled Ribs. 141:1-40. 2019
Effect of Density Ratio on Film-Cooling Effectiveness Distribution and Its Uniformity for Several Hole Geometries on a Flat Plate. 141. 2019
Interaction of Flow and Film-Cooling Effectiveness Between Double-Jet Film-Cooling Holes With Various Spanwise Distances. 140. 2018
Film Cooling Effectiveness Comparison on Full-Scale Turbine Vane Endwalls Using Pressure-Sensitive Paint Technique. 140. 2018
Turbine Blade Platform Film Cooling With Fan-Shaped Holes Under Simulated Swirl Purge Flow and Slashface Leakage Conditions. 140:011006. 2018
A Predictive Model for Preliminary Gas Turbine Blade Cooling Analysis. 139:091010. 2017
Turbine Vane Endwall Film Cooling With Slashface Leakage and Discrete Hole Configuration. 139:061003. 2017
Combined Effects of Freestream Pressure Gradient and Density Ratio on the Film Cooling Effectiveness of Round and Shaped Holes on a Flat Plate. 139:041003. 2017
Turbine Blade Platform Film Cooling With Simulated Swirl Purge Flow and Slashface Leakage Conditions. 139:031012. 2017
Turbine Platform Cooling and Blade Suction Surface Phantom Cooling From Simulated Swirl Purge Flow. 138:081004. 2016
Full-Scale Turbine Vane Endwall Film-Cooling Effectiveness Distribution Using Pressure-Sensitive Paint Technique. 138:051002. 2016
A Combined Experimental and Numerical Study of the Turbine Blade Tip Film Cooling Effectiveness Under Rotation Condition. 137:051009. 2015
Experimental Investigation of the Effect of Purge Flow on Film Cooling Effectiveness on a Rotating Turbine With Nonaxisymmetric End Wall Contouring. 136:091009. 2014
Heat Transfer Measurements in Rotating BladeShape Serpentine Coolant Passage With Ribbed Walls at High Reynolds Numbers. 136:091004. 2014
Effect of Coolant Density on Leading Edge Showerhead Film Cooling Using the Pressure Sensitive Paint Measurement Technique. 136:051011. 2014
Endwall Contouring Using Continuous Diffusion: A New Method and its Application to a Three-Stage High Pressure Turbine. 136. 2014
Endwall Contouring Using Continuous Diffusion: A New Method and its Application to a Three-Stage High Pressure Turbine. 136:011006-797. 2014
On the Reliability of RANS and URANS Numerical Results for High-Pressure Turbine Simulations: A Benchmark Experimental and Numerical Study on Performance and Interstage Flow Behavior of High-Pressure Turbines at Design and Off-Design Conditions Using Two Different Turbine Designs. 135:061012. 2013
Impingement Heat Transfer Enhancement on a Cylindrical, Leading Edge Model With Varying Jet Temperatures. 135:031021. 2013
Heat Transfer Enhancement in a Rectangular (AR = 3:1) Channel With V-Shaped Dimples. 135:011028. 2013
Influence of Unsteady Wake With Trailing Edge Coolant Ejection on Turbine Blade Film Cooling. 134:061026-445. 2012
Turbulent Convection From Deterministic Roughness Distributions With Varying Thermal Conductivities. 134:051030. 2012
Influence of Coolant Density on Turbine Blade Film-Cooling Using Pressure Sensitive Paint Technique. 134:031006-509. 2012
Effects of Inlet Temperature Uniformity and Nonuniformity on the Tip Leakage Flow and Rotor Blade Tip and Casing Heat Transfer Characteristics. 134:021001. 2012
Effect of Flow Parameter Variations on Full Coverage Film-Cooling Effectiveness for a Gas Turbine Blade. 134:011004. 2012
Influence of Channel Orientation on Heat Transfer in a Two-Pass Smooth and Ribbed Rectangular Channel (AR=2:1) Under Large Rotation Numbers. 134:011022. 2012
Effect of Density Ratio on Flat Plate Film Cooling With Shaped Holes Using PSP. 133:041011. 2011
Effect of Freestream Turbulence Intensity on Film Cooling Jet Structure and Surface Effectiveness Using PIV and PSP. 133:041023. 2011
Effect of Upstream Step on Flat Plate Film-Cooling Effectiveness Using PSP. 133:041024. 2011
Heat Transfer and Pressure Drop Measurements for a Square Channel With 45 deg Round-Edged Ribs at High Reynolds Numbers. 133:031019. 2011
High Rotation Number Effects on Heat Transfer in a Rectangular (AR=2:1) Two-Pass Channel. 133:021001. 2011
Film-Cooling Effectiveness on a Rotating Turbine Platform Using Pressure Sensitive Paint Technique. 132:041001-13. 2010
INFLUENCE OF COOLANT DENSITY ON TURBINE BLADE FILM-COOLING USING PRESSURE SENSITIVE PAINT TECHNIQUE. 134:1529-1540. 2010
Heat Transfer in Leading Edge, Triangular Shaped Cooling Channels With Angled Ribs Under High Rotation Numbers. 131:041017-12. 2009
Prediction of Film Cooling and Heat Transfer on a Rotating Blade Platform With Stator-Rotor Purge and Discrete Film-Hole Flows in a 1-12 Turbine Stage. 131:041003-12. 2009
Turbine Blade Platform Film Cooling With Typical Stator-Rotor Purge Flow and Discrete-Hole Film Cooling. 131:041004-11. 2009
Effect of Inlet Flow Angle on Gas Turbine Blade Tip Film Cooling. 131:031005. 2009
Effect of Upstream Wake With Vortex on Turbine Blade Platform Film Cooling With Simulated Stator-Rotor Purge Flow. 131:021017. 2009
Experimental Investigation of the Clocking Effect in a 1.5-Stage Axial TurbinePart I: Time-Averaged Results. 131:021003. 2009
Experimental Investigation of the Clocking Effect in a 1.5-Stage Axial TurbinePart II: Unsteady Results and Boundary Layer Behavior. 131:021004. 2009
Film-Cooling Effectiveness on a Rotating Blade Platform. 131:011014. 2009
Film-Cooling on a Gas Turbine Blade Pressure Side or Suction Side With Compound Angle Shaped Holes. 131:011019. 2009
Effect of a cutback squealer and cavity depth on film-cooling effectiveness on a gas turbine blade tip. 130. 2008
Effect of Reynolds Number and Periodic Unsteady Wake Flow Condition on Boundary Layer Development, Separation, and Intermittency Behavior Along the Suction Surface of a Low Pressure Turbine Blade. 129:92-107. 2007
Dynamic Characteristics of the Diverging Taper Honeycomb-Stator Seal. 128:717-724. 2006
Experimental Study of the Effect of Periodic Unsteady Wake Flow on Boundary Layer Development, Separation, and Reattachment Along the Surface of a Low Pressure Turbine Blade. 126:663-676. 2004
Thermal Performance of Angled, V-Shaped, and W-Shaped Rib Turbulators in Rotating Rectangular Cooling Channels (AR=4:1). 126:604-614. 2004
Heat transfer in rotating rectangular cooling channels (AR = 4) with dimples. 125:555-563. 2003
Experimental and Theoretical Comparison of Two Swirl Brake Designs. 123:353-358. 2001
Effect of Unsteady Wake With Trailing Edge Coolant Ejection on Film Cooling Performance for a Gas Turbine Blade. 121:448-455. 1999
Modeling Unsteady Boundary Layer Transition on a Curved Plate Under Periodic Unsteady Flow Conditions: Aerodynamic and Heat Transfer Investigations. 121:88-97. 1999
Detailed Film Cooling Measurements on a Cylindrical Leading Edge Model: Effect of Free-Stream Turbulence and Coolant Density. 120:799-807. 1998
Effect of Unsteady Wake on Detailed Heat Transfer Coefficient and Film Effectiveness Distributions for a Gas Turbine Blade. 120:808-817. 1998
Rotation Effect on Jet Impingement Heat Transfer in Smooth Rectangular Channels With Four Heated Walls and Radially Outward Crossflow. 120:79-85. 1998
Combined Effect of Grid Turbulence and Unsteady Wake on Film Effectiveness and Heat Transfer Coefficient of a Gas Turbine Blade With Air and CO2 Film Injection. 119:594-600. 1997
Film Effectiveness Over a Flat Surface With Air and CO2 Injection Through Compound Angle Holes Using a Transient Liquid Crystal Image Method. 119:587-593. 1997
Development of Two-Dimensional Wakes Within Curved Channels: Theoretical Framework and Experimental Investigation. 118:506-518. 1996
Local Heat Transfer in a Rotating Two-Pass Triangular Duct With Smooth Walls. 118:435-443. 1996
Surface Heating Effect on Local Heat Transfer in a Rotating Two-Pass Square Channel With 60 deg Angled Rib Turbulators. 117:272-280. 1995
Unsteady Wake Over a Linear Turbine Blade Cascade With Air and CO2 Film Injection: Part IIEffect on Film Effectiveness and Heat Transfer Distributions. 116:730-737. 1994
Influence of Surface Heating Condition on Local Heat Transfer in a Rotating Square Channel With Smooth Walls and Radial Outward Flow. 116:149-158. 1994
Influence of High Mainstream Turbulence on Leading Edge Film Cooling Heat Transfer. 114:707-715. 1992
Influence of High Mainstream Turbulence on Leading Edge Film Cooling Heat Transfer: Effect of Film Hole Row Location. 114:716-723. 1992
Influence of Mainstream Turbulence on Leading Edge Film Cooling Heat Transfer Through Two Rows of Inclined Film Slots. 114:724-733. 1992
Influence of surface heat flux ratio on heat transfer augmentation in square channels with parallel, crossed, and V-shaped angled ribs. 114:872-880. 1992
Turbulent Heat Transfer and Friction in a Square Channel With Discrete Rib Turbulators. 113:360-366. 1991
Pressure Loss Distribution in Three-Pass Rectangular Channels With Rib Turbulators. 111:515-521. 1989
Heat Transfer, Pressure Drop, and Mass Flow Rate in Pin Fin Channels With Long and Short Trailing Edge Ejection Holes. 111:116-123. 1989
Effect of Rib Angle on Local Heat/Mass Transfer Distribution in a Two-Pass Rib-Roughened Channel. 110:233-241. 1988
Effect of Rib Angle on Local Heat/Mass Transfer Distribution in a Two-Pass Rib-Roughened Channel. 110:233-241. 1988
Flat-Plate Film Cooling With Steam Injection Through One Row and Two Rows of Inclined Holes. 108:137-144. 1986
Film Cooling Effectiveness Distributions on a Turbine Blade Cascade Platform With Stator-Rotor Purge and Discrete Film Hole Flows 2008
Internal Cooling Near Trailing Edge of a Gas Turbine Airfoil With Cooling Airflow Through Blockages With Holes 2008
Effect of a Cutback Squealer and Cavity Depth on Film-Cooling Effectiveness on a Gas Turbine Blade Tip 2008
Heat Transfer in Two-Pass Rotating Rectangular Channels (AR=1:2 and AR=1:4) With 45 Deg Angled Rib Turbulators 2005
Heat Transfer Coefficients and Film Cooling Effectiveness on the Squealer Tip of a Gas Turbine Blade 2003
Heat Transfer Coefficients on the Squealer Tip and Near-Tip Regions of a Gas Turbine Blade With Single or Double Squealer 2003
Heat Transfer in Rotating Rectangular Cooling Channels AR=4 With Dimples 2003
Heat Transfer in a Two-Pass Rectangular Rotating Channel With 45-deg Angled Rib Turbulators 2002
Prediction of Flow and Heat Transfer in Rotating Two-Pass Rectangular Channels With 45-deg Rib Turbulators 2002
Flow and Heat Transfer in a Rotating Square Channel With 45 deg Angled Ribs by Reynolds Stress Turbulence Model 2001
Heat Transfer and Flow on the Squealer Tip of a Gas Turbine Blade 2000
Heat Transfer and Pressure Distributions on a Gas Turbine Blade Tip 2000
Unsteady Wake Effect on Film Temperature and Effectiveness Distributions for a Gas Turbine Blade 2000
Heat Transfer Coefficients Over a Flat Surface With Air and CO2 Injection Through Compound Angle Holes Using a Transient Liquid Crystal Image Method 1997
Turbulent Flow Heat Transfer and Friction in a Rectangular Channel With Varying Numbers of Ribbed Walls 1997
Development of Two-Dimensional Wakes Within Curved Channels: Theoretical Framework and Experimental Investigation 1996
Rotation Effect on Jet Impingement Heat Transfer in Smooth Rectangular Channels With Four Heated Walls and Radially Outward Cross Flow 1996
Unsteady Wake Over a Linear Turbine Blade Cascade With Air and CO2 Film Injection: Part IEffect on Heat Transfer Coefficients 1994
Effect of Trailing-Edge Ejection on Local Heat (Mass) Transfer in Pin Fin Cooling Channels in Turbine Blades 1994
Influence of Mainstream Turbulence on Leading Edge Film Cooling Heat Transfer Through Two Rows of Inclined Film Slots 1992
Influence of Surface Heat Flux Ratio on Heat Transfer Augmentation in Square Channels With Parallel, Crossed, and V-Shaped Angled Ribs 1992
Heat Transfer Characteristics of Turbulent Flow in a Square Channel With Angled Discrete Ribs 1991
Effect of Rib-Angle Orientation on Local Mass Transfer Distribution in a Three-Pass Rib-Roughened Channel 1991
Heat Transfer, Pressure Drop, and Mass Flow Rate in Pin Fin Channels With Long and Short Trailing Edge Ejection Holes 1989

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