Journal of Turbomachinery Journal

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Overview

publication venue for

• Film Cooling Comparison of Full-Scale Turbine Vanes Using the Pressure Sensitive Paint Technique.  145. 2023
• Characterization of an Apparatus to Study Solid Deposit Formation in Lubricating Oils at High Temperatures.  145. 2023
• Heat Transfer in Rotating, Trailing Edge, Converging Channels With Full- and Partial-Height Strip-Fins.  144. 2022
• Thermal Performance of Double-Sided, Partial Height Strip Fin Arrays in a High Aspect Ratio, Rectangular Channel.  144. 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
• 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
• 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 Blade–Shape 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
• Impingement Heat Transfer Enhancement on a Cylindrical, Leading Edge Model With Varying Jet Temperatures.  135:031021. 2013
• 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
• Effects of Inlet Temperature Uniformity and Nonuniformity on the Tip Leakage Flow and Rotor Blade Tip and Casing Heat Transfer Characteristics.  134:021001. 2012
• ENDWALL CONTOURING USING CONTINIOUS DIFFUSION, A BREAKTHROUGH METHOD AND ITS APPLICATION TO A THREE-STAGE HIGH PRESSURE TURBINE.  136:787-797. 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
• 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
• 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
• Film-Cooling Effectiveness on a Rotating Blade Platform.  131:011014. 2009
• Effect of a cutback squealer and cavity depth on film-cooling effectiveness on a gas turbine blade tip.  130. 2008
• 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
• 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
• 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
• 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

Identity

International Standard Serial Number (ISSN)

• 0889-504X