JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME
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Overview
publication venue for
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HEAT TRANSFER IN A ROTATING TWO-PASS RECTANGULAR CHANNEL FEATURING REDUCED CROSS-SECTIONAL AREA AFTER TIP TURN (AR=4:1 to 2:1) WITH PROFILED 60 DEG ANGLED RIBS.
141:1-40.
2019
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Effect of Density Ratio on Film-Cooling Effectiveness Distribution and Its Uniformity for Several Hole Geometries on A Flat Plate.
141.
2019
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Interaction of Flow and Film-Cooling Effectiveness between Double-Jet Film-Cooling Holes with Various Spanwise Distances.
140.
2018
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Film Cooling Effectiveness Comparison on Full-Scale Turbine Vane Endwalls Using PSP Technique.
140.
2017
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Turbine Blade Platform Film Cooling With Fan-Shaped Holes Under Simulated Swirl Purge Flow and Slashface Leakage Conditions.
140:011006.
2017
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A Predictive Model for Preliminary Gas Turbine Blade Cooling Analysis.
139:091010.
2017
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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
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Turbine Vane Endwall Film Cooling With Slashface Leakage and Discrete Hole Configuration.
139:061003.
2017
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Turbine Blade Platform Film Cooling With Simulated Swirl Purge Flow and Slashface Leakage Conditions.
139:031012.
2016
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Turbine Platform Cooling and Blade Suction Surface Phantom Cooling From Simulated Swirl Purge Flow.
138:081004.
2016
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Full-Scale Turbine Vane Endwall Film-Cooling Effectiveness Distribution Using Pressure-Sensitive Paint Technique.
138:051002.
2016
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A Combined Experimental and Numerical Study of the Turbine Blade Tip Film Cooling Effectiveness Under Rotation Condition.
137:051009.
2015
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Experimental Investigation of the Effect of Purge Flow on Film Cooling Effectiveness on a Rotating Turbine With Nonaxisymmetric End Wall Contouring.
136:091009.
2014
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Heat Transfer Measurements in Rotating Blade–Shape Serpentine Coolant Passage With Ribbed Walls at High Reynolds Numbers.
136:091004.
2014
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Endwall Contouring Using Continuous Diffusion: A New Method and its Application to a Three-Stage High Pressure Turbine.
136.
2014
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Endwall Contouring Using Continuous Diffusion: A New Method and its Application to a Three-Stage High Pressure Turbine.
136:011006-797.
2014
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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
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Effect of Coolant Density on Leading Edge Showerhead Film Cooling Using the Pressure Sensitive Paint Measurement Technique.
136:051011.
2013
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Impingement Heat Transfer Enhancement on a Cylindrical, Leading Edge Model With Varying Jet Temperatures.
135:031021.
2013
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Heat Transfer Enhancement in a Rectangular (AR = 3:1) Channel With V-Shaped Dimples.
135:011028.
2013
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Influence of Unsteady Wake With Trailing Edge Coolant Ejection on Turbine Blade Film Cooling.
134:061026-445.
2012
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Turbulent Convection From Deterministic Roughness Distributions With Varying Thermal Conductivities.
134:051030.
2012
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Effect of Density Ratio on Flat Plate Film Cooling With Shaped Holes Using PSP.
133:041011.
2011
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Effect of Freestream Turbulence Intensity on Film Cooling Jet Structure and Surface Effectiveness Using PIV and PSP.
133:041023.
2011
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Influence of Coolant Density on Turbine Blade Film-Cooling Using Pressure Sensitive Paint Technique.
134:031006-509.
2011
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Effects of Inlet Temperature Uniformity and Nonuniformity on the Tip Leakage Flow and Rotor Blade Tip and Casing Heat Transfer Characteristics.
134:021001.
2011
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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.
2011
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Effect of Flow Parameter Variations on Full Coverage Film-Cooling Effectiveness for a Gas Turbine Blade.
134:011004.
2011
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Effect of Upstream Step on Flat Plate Film-Cooling Effectiveness Using PSP.
133:041024.
2011
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Heat Transfer and Pressure Drop Measurements for a Square Channel With 45 deg Round-Edged Ribs at High Reynolds Numbers.
133:031019.
2010
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High Rotation Number Effects on Heat Transfer in a Rectangular (AR=2:1) Two-Pass Channel.
133:021001.
2010
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INFLUENCE OF COOLANT DENSITY ON TURBINE BLADE FILM-COOLING USING PRESSURE SENSITIVE PAINT TECHNIQUE.
134:1529-1540.
2010
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Film-Cooling Effectiveness on a Rotating Turbine Platform Using Pressure Sensitive Paint Technique.
132:041001-13.
2010
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Heat Transfer in Leading Edge, Triangular Shaped Cooling Channels With Angled Ribs Under High Rotation Numbers.
131:041017-12.
2009
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Turbine Blade Platform Film Cooling With Typical Stator-Rotor Purge Flow and Discrete-Hole Film Cooling.
131:041004-11.
2009
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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
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Effect of Inlet Flow Angle on Gas Turbine Blade Tip Film Cooling.
131:031005.
2009
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Experimental Investigation of the Clocking Effect in a 1.5-Stage Axial Turbine—Part I: Time-Averaged Results.
131:021003.
2009
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Experimental Investigation of the Clocking Effect in a 1.5-Stage Axial Turbine—Part II: Unsteady Results and Boundary Layer Behavior.
131:021004.
2009
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Effect of Upstream Wake With Vortex on Turbine Blade Platform Film Cooling With Simulated Stator-Rotor Purge Flow.
131:021017.
2009
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Film-Cooling on a Gas Turbine Blade Pressure Side or Suction Side With Compound Angle Shaped Holes.
131:011019.
2008
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Film-Cooling Effectiveness on a Rotating Blade Platform.
131:011014.
2008
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Effect of a cutback squealer and cavity depth on film-cooling effectiveness on a gas turbine blade tip.
130.
2008
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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
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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
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Dynamic Characteristics of the Diverging Taper Honeycomb-Stator Seal.
128:717-724.
2004
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Heat transfer in rotating rectangular cooling channels (AR = 4) with dimples.
125:555-563.
2003
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Experimental and Theoretical Comparison of Two Swirl Brake Designs.
123:353-358.
2000
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Effect of Unsteady Wake With Trailing Edge Coolant Ejection on Film Cooling Performance for a Gas Turbine Blade.
121:448-455.
1999
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Modeling Unsteady Boundary Layer Transition on a Curved Plate Under Periodic Unsteady Flow Conditions: Aerodynamic and Heat Transfer Investigations.
121:88-97.
1999
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Detailed Film Cooling Measurements on a Cylindrical Leading Edge Model: Effect of Free-Stream Turbulence and Coolant Density.
120:799-807.
1998
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Effect of Unsteady Wake on Detailed Heat Transfer Coefficient and Film Effectiveness Distributions for a Gas Turbine Blade.
120:808-817.
1998
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Rotation effect on jet impingement heat transfer in smooth rectangular channels with four heated walls and radially outward crossflow.
120:79-85.
1998
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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
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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
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Local Heat Transfer in a Rotating Two-Pass Triangular Duct With Smooth Walls.
118:435-443.
1996
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Development of two-dimensional wakes within curved channels: Theoretical framework and experimental investigation.
118:506-518.
1996
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Surface Heating Effect on Local Heat Transfer in a Rotating Two-Pass Square Channel With 60 deg Angled Rib Turbulators.
117:272-280.
1995
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Unsteady Wake Over a Linear Turbine Blade Cascade With Air and CO2 Film Injection: Part II—Effect on Film Effectiveness and Heat Transfer Distributions.
116:730-737.
1994
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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
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Influence of High Mainstream Turbulence on Leading Edge Film Cooling Heat Transfer.
114:707-715.
1992
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Influence of High Mainstream Turbulence on Leading Edge Film Cooling Heat Transfer: Effect of Film Hole Row Location.
114:716-723.
1992
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Influence of mainstream turbulence on leading edge film cooling heat transfer through two rows of inclined film slots.
114:724-733.
1992
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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
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Turbulent Heat Transfer and Friction in a Square Channel With Discrete Rib Turbulators.
113:360-366.
1991
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Pressure Loss Distribution in Three-Pass Rectangular Channels With Rib Turbulators.
111:515-521.
1989
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Heat transfer, pressure drop, and iass flow rate in pin fin channels with long and short trailing edge ejection holes.
111:116-123.
1989
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Effect of Rib Angle on Local Heat/Mass Transfer Distribution in a Two-Pass Rib-Roughened Channel.
110:233-241.
1988
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Effect of rib angle on local heat/mass transfer distribution in a two-pass rib-roughened channel.
110:233-241.
1988
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Flat-Plate Film Cooling With Steam Injection Through One Row and Two Rows of Inclined Holes.
108:137-144.
1986
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Film Cooling Effectiveness Distributions on a Turbine Blade Cascade Platform With Stator-Rotor Purge and Discrete Film Hole Flows
2008
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Internal Cooling Near Trailing Edge of a Gas Turbine Airfoil With Cooling Airflow Through Blockages With Holes
2008
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Effect of a Cutback Squealer and Cavity Depth on Film-Cooling Effectiveness on a Gas Turbine Blade Tip
2008
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Heat Transfer in Two-Pass Rotating Rectangular Channels (AR=1:2 and AR=1:4) With 45 Deg Angled Rib Turbulators
2005
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Thermal Performance of Angled, V-Shaped, and W-Shaped Rib Turbulators in Rotating Rectangular Cooling Channels (AR=4:1)
2004
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Heat Transfer Coefficients and Film Cooling Effectiveness on the Squealer Tip of a Gas Turbine Blade
2003
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Heat Transfer Coefficients on the Squealer Tip and Near-Tip Regions of a Gas Turbine Blade With Single or Double Squealer
2003
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Heat Transfer in Rotating Rectangular Cooling Channels (AR=4) With Dimples
2003
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Heat Transfer in a Two-Pass Rectangular Rotating Channel With 45-deg Angled Rib Turbulators
2002
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Prediction of Flow and Heat Transfer in Rotating Two-Pass Rectangular Channels With 45-deg Rib Turbulators
2002
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Flow and Heat Transfer in a Rotating Square Channel With 45 deg Angled Ribs by Reynolds Stress Turbulence Model
2000
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Heat Transfer and Flow on the Squealer Tip of a Gas Turbine Blade
2000
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Heat Transfer and Pressure Distributions on a Gas Turbine Blade Tip
2000
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Unsteady Wake Effect on Film Temperature and Effectiveness Distributions for a Gas Turbine Blade
1999
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Rotation Effect on Jet Impingement Heat Transfer in Smooth Rectangular Channels With Four Heated Walls and Radially Outward Crossflow
1998
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Heat Transfer Coefficients Over a Flat Surface With Air and CO2 Injection Through Compound Angle Holes Using a Transient Liquid Crystal Image Method
1997
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Turbulent Flow Heat Transfer and Friction in a Rectangular Channel With Varying Numbers of Ribbed Walls
1997
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Development of Two-Dimensional Wakes Within Curved Channels: Theoretical Framework and Experimental Investigation
1996
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Unsteady Wake Over a Linear Turbine Blade Cascade With Air and CO2 Film Injection: Part I—Effect on Heat Transfer Coefficients
1994
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Effect of Trailing-Edge Ejection on Local Heat (Mass) Transfer in Pin Fin Cooling Channels in Turbine Blades
1994
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Influence of Mainstream Turbulence on Leading Edge Film Cooling Heat Transfer Through Two Rows of Inclined Film Slots
1992
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Influence of Surface Heat Flux Ratio on Heat Transfer Augmentation in Square Channels With Parallel, Crossed, and V-Shaped Angled Ribs
1992
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Heat Transfer Characteristics of Turbulent Flow in a Square Channel With Angled Discrete Ribs
1991
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Effect of Rib-Angle Orientation on Local Mass Transfer Distribution in a Three-Pass Rib-Roughened Channel
1991
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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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