Journal of Turbomachinery - Texas A&M University (TAMU) Scholar

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Thermal Performance of Double-Sided, Partial Height Strip Fin Arrays in a High Aspect Ratio, Rectangular Channel. 144. 2022
Heat Transfer in Rotating, Trailing Edge, Converging Channels With Full- and Partial-Height Strip-Fins. 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 Partial Length Pin-Fins. 143. 2021
Heat Transfer in Rotating, Trailing-Edge, Converging Channels With Smooth Walls and Pin-Fins. 143. 2021
Upstream Film Cooling on the Contoured Endwall of a Transonic Turbine Vane in an Annular Cascade. 143. 2021
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
Transonic Turbine Vane Endwall Film Cooling Using the Pressure-Sensitive Paint Measurement Technique. 142. 2020
Effect of Density Ratio on Film-Cooling Effectiveness Distribution and Its Uniformity for Several Hole Geometries on a Flat Plate. 141. 2019
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
Film Cooling Effectiveness Comparison on Full-Scale Turbine Vane Endwalls Using Pressure-Sensitive Paint Technique. 140. 2018
Interaction of Flow and Film Cooling Effectiveness Between Double-Jet Film-Cooling Holes With Various Spanwise Distances. 140. 2018
Turbine Blade Platform Film Cooling With Fan-Shaped Holes Under Simulated Swirl Purge Flow and Slashface Leakage Conditions. 140:011006. 2018
Turbine Blade Platform Film Cooling With Simulated Swirl Purge Flow and Slashface Leakage Conditions. 139:031012. 2017
A Predictive Model for Preliminary Gas Turbine Blade Cooling Analysis. 139:091010. 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 Vane Endwall Film Cooling With Slashface Leakage and Discrete Hole Configuration. 139:061003. 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
Effect of Coolant Density on Leading Edge Showerhead Film Cooling Using the Pressure Sensitive Paint Measurement Technique. 136:051011. 2014
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 Blade-Shape Serpentine Coolant Passage With Ribbed Walls at High Reynolds Numbers. 136:091004. 2014
Endwall Contouring Using Continuous Diffusion: A New Method and its Application to a Three-Stage High Pressure Turbine. 136. 2014
Heat Transfer Enhancement in a Rectangular (AR=3:1) Channel With V-Shaped Dimples. 135:011028. 2013
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
ENDWALL CONTOURING USING CONTINIOUS DIFFUSION, A BREAKTHROUGH METHOD AND ITS APPLICATION TO A THREE-STAGE HIGH PRESSURE TURBINE. 136:787-797. 2012
INFLUENCE OF UNSTEADY WAKE WITH TRAILING EDGE COOLANT EJECTION ON TURBINE BLADE FILM COOLING. 134:435-445. 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
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 Flow Parameter Variations on Full Coverage Film-Cooling Effectiveness for a Gas Turbine Blade. 134:011004. 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
Heat Transfer and Pressure Drop Measurements for a Square Channel With 45 deg Round-Edged Ribs at High Reynolds Numbers. 133:031019. 2011
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
High Rotation Number Effects on Heat Transfer in a Rectangular (AR=2:1) Two-Pass Channel. 133:021001. 2011
Effect of Upstream Step on Flat Plate Film-Cooling Effectiveness Using PSP. 133:041024. 2011
INFLUENCE OF COOLANT DENSITY ON TURBINE BLADE FILM-COOLING USING PRESSURE SENSITIVE PAINT TECHNIQUE. 134:1529-1540. 2010
Film-Cooling Effectiveness on a Rotating Turbine Platform Using Pressure Sensitive Paint Technique. 132:041001-13. 2010
Film-Cooling on a Gas Turbine Blade Pressure Side or Suction Side With Compound Angle Shaped Holes. 131:011019. 2009
Film-Cooling Effectiveness on a Rotating Blade Platform. 131:011014. 2009
Heat Transfer in Leading Edge, Triangular Shaped Cooling Channels With Angled Ribs Under High Rotation Numbers. 131:041017-12. 2009
Turbine Blade Platform Film Cooling With Typical Stator-Rotor Purge Flow and Discrete-Hole Film Cooling. 131:041004-11. 2009
Prediction of Film Cooling and Heat Transfer on a Rotating Blade Platform With Stator-Rotor Purge and Discrete Film-Hole Flows in a 1-1/2 Turbine Stage. 131:041003-12. 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
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 2-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 .2. EFFECT 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 2-PASS RIB-ROUGHENED CHANNEL. 110:233-241. 1988
FLAT-PLATE FILM COOLING WITH STEAM INJECTION THROUGH ONE ROW AND 2 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
Effect of a cutback squealer and cavity depth on film-cooling effectiveness on a gas turbine blade tip 2008
Internal cooling near trailing edge of a gas turbine airfoil with cooling airflow through blockages with holes 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
Float 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
Rotation effect on jet impingement heat transfer in smooth rectangular channels with four heated walls and radially outward crossflow 1998
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
UNSTEADY WAKE OVER A LINEAR TURBINE BLADE CASCADE WITH AIR AND CO2 FILM INJECTION .1. EFFECT 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 SURFACE HEAT-FLUX RATIO ON HEAT-TRANSFER AUGMENTATION IN SQUARE CHANNELS WITH PARALLEL, CROSSED, AND V-SHAPED ANGLED RIBS 1992
Influence of Mainstream Turbulence on Leading Edge Film Cooling Heat Transfer Through Two Rows of Inclined Film Slots 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 3-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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