# positions[].organizations[].parent[].label
Texas A&M Engineering Experiment Station (TEES)

# overview
My research focuses on thermal Fluid Sciences - heat transfer and cooling in gas turbines, heat transfer enhancement, heat transfer in rotating flows, film cooling in unsteady high turbulent flows, combustor-liner cooling, mini-channel heat transfer, advanced CFD and experimental methods.

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
Fluid Dynamics And Heat Transfer Phenomena In Compressor And Turbine Components Of Gas Turbine Engines

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4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4007 Control Engineering, Mechatronics And Robotics

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4007 Control Engineering, Mechatronics And Robotics

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
Fluid Dynamics And Heat Transfer Phenomena In Compressor And Turbine Components Of Gas Turbine Engines

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# keywords[]
4012 Fluid Mechanics And Thermal Engineering

# awardsAndHonors[].label
ASME K-14 Warren Rohsenow Prize for Best Presentation

# awardsAndHonors[].label
ASME Heat Transfer Division 75th Anniversary Medal

# awardsAndHonors[].label
ASME IGTI Aircraft Engine Technology Award

# awardsAndHonors[].label
ASME IGTI Certificate Award for Valued Service as Chair of the Heat Transfer Committee

# publications[].label
Local heat transfer in a rotating two-pass triangular duct with smooth walls

# publications[].label
Heat Transfer in Rotating Serpentine Coolant Passage With Ribbed Walls at Low Mach Numbers

# publications[].label
INFLUENCE OF SURFACE HEAT-FLUX RATIO ON HEAT-TRANSFER AUGMENTATION IN SQUARE CHANNELS WITH PARALLEL, CROSSED, AND V-SHAPED ANGLED RIBS

# publications[].label
Effect of rib height on heat transfer in a two pass rectangular channel (AR=1:4) with a sharp entrance at high rotation numbers

# publications[].label
INFLUENCE OF COOLANT DENSITY ON TURBINE BLADE FILM-COOLING WITH COMPOUND-ANGLE SHAPED HOLES

# publications[].label
HEAT TRANSFER COEFFICIENTS AND FILM COOLING EFFECTIVENESS OF TRANSONIC TURBINE VANE SUCTION SURFACE USING TSP TECHNIQUE

# publications[].label
Heat transfer in trailing edge, wedge-shaped cooling channels under high rotation numbers

# publications[].label
High Rotation Number Effect on Heat Transfer in a Triangular Channel With 45, Inverted 45, and 90 Ribs

# publications[].label
Heat Transfer in Leading Edge, Triangular Shaped Cooling Channels With Angled Ribs Under High Rotation Numbers

# publications[].label
Gas Turbine Heat Transfer and Cooling Technology

# publications[].label
Heat Transfer in Rotating Multi-Pass Rectangular Smooth Channel with and without a Turning Vane in Hub Region

# publications[].label
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

# publications[].label
Internal cooling near trailing edge of a gas turbine airfoil with cooling airflow through blockages with holes

# publications[].label
Unsteady wake effect on film temperature and effectiveness distributions for a gas turbine blade

# publications[].label
Heat transfer in rotating rectangular cooling channels (AR = 4) with dimples

# publications[].label
HEAT TRANSFER MEASUREMENTS IN ROTATING BLADE-SHAPE SERPENTINE COOLANT PASSAGE WITH RIBBED WALLS AT HIGH REYNOLDS NUMBERS

# publications[].label
Heat Transfer in Square Channels with Wedge-Shaped and Delta-Shaped Turbulence Promoters

# publications[].label
TRANSIENT NUCLEATION AND BUBBLE-GROWTH IN IMMISCIBLE LIQUID COMPOSITES INDUCED BY COUNTERDIFFUSION OF GASES

# publications[].label
Heat Transfer in Rotating, Trailing Edge, Converging Channels With Partial Length Pin-Fins

# publications[].label
Effect of 45-deg Rib Orientations on Heat Transfer in a Rotating Two-Pass Channel With Aspect Ratio from 4:1 to 2:1

# publications[].label
FLAT-PLATE FILM COOLING WITH STEAM INJECTION THROUGH ONE ROW AND 2 ROWS OF INCLINED HOLES

# publications[].label
Film cooling effectiveness on the leading edge region of a rotating turbine blade with two rows of film cooling holes using pressure sensitive paint

# publications[].label
Heat transfer and pressure distributions on a gas turbine blade tip

# publications[].label
HEAT TRANSFER AND FILM COOLING WITH STEAM INJECTION THROUGH AN INCLINED HOLE OVER A FLAT PLATE.

# publications[].label
Upstream Vortex Effect on Turbine Platform Film Cooling with Typical Purge Flow

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Influence of mainstream turbulence on turbine blade platform cooling from simulated swirl purge flow

# publications[].label
Measurements on Augmented Heat Transfer Surfaces Using a Transient Liquid Crystal Technique

# publications[].label
Effect of Rib Spacing on Heat Transfer in a Two Pass Rectangular Channel (AR=2:1) at High Rotation Numbers

# publications[].label
Film-cooling effectiveness on a gas turbine blade tip using pressure-sensitive paint

# publications[].label
Film-cooling effectiveness on a rotating turbine platform using pressure sensitive paint technique

# publications[].label
Heat Transfer in Trailing Edge, Wedge Shaped Cooling Channels with Slot Ejection under High Rotation Numbers

# publications[].label
Effect of upstream wake with vortex on turbine blade platform film cooling with simulated stator-rotor purge flow

# publications[].label
Heat Transfer Coefficient and Film-Cooling Effectiveness on the Squealer Tip of a Gas Turbine Blade

# publications[].label
Heat Transfer and Pressure Loss Measurements in a Turbulated High Aspect Ratio Channel With Large Reynolds Number Flows

# publications[].label
Flat plate film cooling with linear and curved round-to-diffusion shaped slots using PSP measurement technique

# publications[].label
HEAT TRANSFER IN ROTATING MULTI-PASS RECTANGULAR RIBBED CHANNEL WITH AND WITHOUT A TURNING VANE

# publications[].label
Heat Transfer in a Rotating Cooling Channel (AR=2:1) With Rib Turbulators and a Tip Turning Vane

# publications[].label
A Combined Experimental and Numerical Study of the Turbine Blade Tip Film Cooling Effectiveness Under Rotation Condition

# publications[].label
Flow and heat transfer in rotating two-pass rectangular channels (AR=2) by Reynolds stress turbulence model

# publications[].label
Method and apparatus for heating a mold cavity uniformly

# publications[].label
Effect of inlet flow angle on gas turbine blade tip film cooling

# publications[].label
Heat Transfer in Leading Edge, Triangular Shaped Cooling Channels with Angled Ribs under High Rotation Numbers

# publications[].label
Heat-transfer coefficients of a turbine blade-tip and near-tip regions

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
HEAT-TRANSFER AND FRICTION IN RECTANGULAR CHANNELS WITH RIBBED OR RIBBED-GROOVED WALLS

# publications[].label
Turbine blade internal cooling passages with rib turbulators

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
LOCAL HEAT/MASS TRANSFER DISTRIBUTION AROUND SHARP 180 degree TURN IN A SMOOTH SQUARE CHANNEL.

# publications[].label
Effect of film-hole shape on turbine-blade heat-transfer coefficient distribution

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Heat transfer in a two-pass rectangular channel (AR=1 : 4) under high rotation numbers

# publications[].label
Heat Transfer and Friction in Triangular Ducts with Turbulence Promoters

# publications[].label
Prediction of Film Cooling Effectiveness of Steam

# publications[].label
PREDICTION OF FILM COOLING EFFECTIVENESS OF STEAM.

# publications[].label
TURBINE BLADE PLATFORM FILM COOLING WITH SIMULATED SWIRL PURGE FLOW AND SLASHFACE LEAKAGE CONDITIONS

# publications[].label
A numerical study of flow and heat transfer in rotating rectangular channels (AR=4) with 45 deg rib turbulators by Reynolds stress turbulence model

# publications[].label
Forced convective heat transfer in channels with internal longitudinal fins

# publications[].label
Influence of High Mainstream Turbulence on Leading Edge Film Cooling Heat Transfer: Effect of Film Hole Row Location

# publications[].label
Turbulent heat transfer and friction in a square channel with discrete rib turbulators

# publications[].label
Rotation Effect on Jet Impingement Heat Transfer in Smooth Rectangular Channels with Film Coolant Extraction

# publications[].label
Detailed film cooling measurements on a cylindrical model with simulated TBC spallation

# publications[].label
Plasma induced virtual turbine airfoil trailing edge extension

# publications[].label
Effect of a Turning Vane on Heat Transfer in Rotating Multipass Rectangular Smooth Channel

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
EFFECT OF LATERAL FLOW EJECTION ON TURBULENT HEAT TRANSFER IN PIN FIN CHANNELS.

# publications[].label
Heat Transfer Characteristics of Turbulent Flow in a Square Channel With Angled Discrete Ribs

# publications[].label
Turbine rotor with various tip configurations flow and heat transfer prediction

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Turbine Blade Platform Film Cooling With Fan-Shaped Holes Under Simulated Swirl Purge Flow and Slashface Leakage Conditions

# publications[].label
Effect of rib profiles on turbulent channel flow heat transfer

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
EFFECTS OF FIN CONFIGURATION AND ENTRANCE LENGTH ON LOCAL ENDWALL HEAT/MASS TRANSFER IN A PIN FIN CHANNEL.

# publications[].label
HEAT-TRANSFER AND FRICTION IN CHANNELS WITH 2 OPPOSITE RIB-ROUGHENED WALLS

# publications[].label
Upstream Film Cooling on the Contoured Endwall of a Transonic Turbine Vane in an Annular Cascade

# publications[].label
EFFECT OF COOLANT DENSITY ON LEADING EDGE SHOWERHEAD FILM COOLING USING PSP MEASUREMENT TECHNIQUE

# publications[].label
Film cooling effectiveness distribution on a gas turbine blade platform with inclined slot leakage and discrete film hole flows

# publications[].label
Film Cooling for Cylindrical and Fan-Shaped Holes Using Pressure-Sensitive Paint Measurement Technique

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Heat transfer in a smooth rotating multi-passage channel with hub turning vane and trailing-edge slot ejection

# publications[].label
Advanced Cooling in Gas Turbines 2016 Max Jakob Memorial Award Paper

# publications[].label
Film cooling measurements on cylindrical models with simulated thermal barrier coating spallation

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
LOCAL HEAT MASS-TRANSFER DISTRIBUTIONS AROUND SHARP 180 DEG TURNS IN 2-PASS SMOOTH AND RIB-ROUGHENED CHANNELS

# publications[].label
Influence of Channel Orientation on Heat Transfer in a Two-Pass Smooth and Ribbed Rectangular Channel (AR=2:1) Under Large Rotation Numbers

# publications[].label
Film-cooling prediction on turbine blade tip with various film hole configurations

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
LOCAL HEAT TRANSFER AUGMENTATION IN CHANNELS WITH TWO OPPOSITE RIBBED SURFACES

# publications[].label
Effect of Flow Parameter Variations on Full Coverage Film-Cooling Effectiveness for a Gas Turbine Blade

# publications[].label
Surface heating effect on local heat transfer in a rotating two-pass square channel with 60 angled rib turbulators

# publications[].label
Effect of Flow Parameter Variations on Full Coverage Film-Cooling Effectiveness for a Gas Turbine Blade

# publications[].label
Turbine Blade Surface Phantom Cooling from Upstream Nozzle Trailing-Edge Ejection

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Film Cooling Effectiveness Comparison on Full-Scale Turbine Vane Endwalls Using PSP Technique

# publications[].label
Numerical Investigation of the Effect of Purge Flow on Aerodynamic Performance and Film Cooling Effectiveness on a Rotating Turbine with Non-Axisymmetric Endwall Contouring

# publications[].label
Heat Transfer in Two-Pass Rotating Rectangular Channels (AR=1:2 and AR=1:4) With Smooth Walls

# publications[].label
Near-wall second-moment closure for rotating multiple-pass cooling channels

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Unsteady Wake Over a Linear Turbine Blade Cascade With Air and CO2 Film Injection: Part II  Effect on Film Effectiveness and Heat Transfer Distributions

# publications[].label
Heat transfer in rotating rectangular cooling channels (AR=4) with dimples

# publications[].label
Film cooling effectiveness distribution on a gas turbine blade platform with inclined slot leakage and discrete film hole flows

# publications[].label
INFLUENCE OF COOLANT DENSITY ON TURBINE BLADE FILM-COOLING WITH AXIAL SHAPED HOLES

# publications[].label
Effect of Unsteady Wake on Detailed Heat Transfer Coefficient and Film Effectiveness Distributions for a Gas Turbine Blade

# publications[].publisher
American Society of Mechanical Engineers

# publications[].label
Heat transfer in trailing edge, wedge-shaped cooling channels under high rotation numbers

# publications[].label
Recent developments in turbine blade internal cooling.

# publications[].label
Heat Transfer and Friction in Rectangular Convergent and Divergent Channels with Ribs

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Heat Transfer and Friction in Cooling Channels Near Trailing Edges of Turbine Blades

# publications[].label
Heat transfer coefficients on the squealer tip and near squealer tip regions of a gas turbine blade

# publications[].label
Effect of Upstream Step on Flat Plate Film-Cooling Effectiveness Using PSP

# publications[].label
Effects of angled ribs on turbulent heat transfer and friction factors in a rectangular divergent channel

# publications[].label
COMPUTER MODEL FOR GAS TURBINE BLADE COOLING ANALYSIS.

# publications[].label
Detailed Film Cooling Measurements over a Gas Turbine Blade Using a Transient Liquid Crystal Image Technique

# publications[].label
Influence of Cooling Flow Rate Variation on Gas Turbine Blade Temperature Distributions

# publications[].label
AUGMENTED HEAT-TRANSFER IN SQUARE CHANNELS WITH PARALLEL, CROSSED, AND V-SHAPED ANGLED RIBS

# publications[].label
Heat Transfer and Flow on the Squealer Tip of a Gas Turbine Blade

# publications[].label
Film Cooling Effectiveness Distributions on a Turbine Blade Cascade Platform With Stator-Rotor Purge and Discrete Film Hole Flows

# publications[].label
Film-cooling on a gas turbine blade pressure side or suction side with compound angle shaped holes

# publications[].label
Film Cooling Effectiveness Comparison on Full-Scale Turbine Vane Endwalls Using Pressure-Sensitive Paint Technique

# publications[].label
Influence of Surface Heating Condition on Local Heat Transfer in Enclosed Corotating Disks With Axial Throughflow

# publications[].label
Turbulent Flow Heat Transfer and Friction in a Rectangular Channel With Varying Number of Ribbed Walls

# publications[].label
Detailed heat transfer coefficient distributions on a large-scale gas turbine blade tip

# publications[].label
EFFECT OF RIB-ANGLE ORIENTATION ON LOCAL MASS-TRANSFER DISTRIBUTION IN A 3-PASS RIB-ROUGHENED CHANNEL

# publications[].label
Impingement heat transfer on a target plate with film cooling holes

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Unsteady high turbulence effect on turbine blade film cooling heat transfer performance using a transient liquid crystal technique

# publications[].label
FILM COOLING EFFECTIVENESS COMPARISON ON TURBINE VANE ENDWALL WITH CLUSTER CONFIGURATIONS USING PSP MEASUREMENT TECHNIQUE

# publications[].label
Influence of Coolant Density on Turbine Platform Film-Cooling With Stator-Rotor Purge Flow and Compound-Angle Holes

# publications[].label
Turbulent Flow in Circular Tubes with Twisted-Tape Inserts and Axial Interrupted Ribs

# publications[].label
Plasma lifted boundary layer gas turbine engine vane

# publications[].label
Rib spacing effect on heat transfer and pressure loss in a rotating two-pass rectangular channel (AR=1:2) with 45-degree angled ribs

# publications[].label
Jet Impingement Heat Transfer on Pinned Surfaces Using a Transient Liquid Crystal Technique

# publications[].label
Influence of Mainstream Turbulence on Leading Edge Film Cooling Heat Transfer Through Two Rows of Inclined Film Slots

# publications[].label
Effect of Rib-Angle Orientation on Local Mass Transfer Distribution in a Three-Pass Rib-Roughened Channel

# publications[].label
Surface Heating Effect on Local Heat Transfer in an Inclosed Corotating Disks with Axial Throughflow

# publications[].label
Heat Transfer and Thermal Mechanical Stress Distributions in Gas Turbine Blades

# publications[].label
Numerical prediction of film cooling and heat transfer on the leading edge of a rotating blade with two rows holes in a 1-(1)/(2) turbine stage at design and off design conditions

# publications[].label
Airfoil with plasma generator for shielding a boundary layer downstream of a film cooling hole and corresponding operating method

# publications[].label
INFLUENCE OF UNSTEADY WAKE ON HEAT-TRANSFER COEFFICIENT FROM A GAS-TURBINE BLADE

# publications[].label
Effect of Rotation on Heat Transfer in Narrow Rectangular Cooling Channels (AR = 8:1 and 4:1) With Pin-Fins

# publications[].label
HEAT TRANSFER AND PRESSURE DROP MEASUREMENTS FOR A SQUARE CHANNEL WITH 45DEG ROUND EDGED RIBS AT HIGH REYNOLDS NUMBERS

# publications[].label
A PREDICTIVE MODEL FOR PRELIMINARY GAS TURBINE BLADE COOLING ANALYSIS

# publications[].label
EFFECT OF UNEVEN WALL TEMPERATURE ON LOCAL HEAT-TRANSFER IN A ROTATING SQUARE CHANNEL WITH SMOOTH WALLS AND RADIAL OUTWARD FLOW

# publications[].label
INFLUENCE OF COOLANT DENSITY ON TURBINE PLATFORM FILM-COOLING WITH STATOR-ROTOR PURGE FLOW AND COMPOUND-ANGLE HOLES

# publications[].label
Film-Cooling on a Gas Turbine Blade Pressure Side or Suction Side With Compound Angle Shaped Holes

# publications[].label
Heat Transfer in a Rotating, Blade-Shaped Serpentine Cooling Passage With Discrete Ribbed Walls at High Reynolds Numbers

# publications[].label
Heat transfer and friction behaviors in rectangular channels with varying number of ribbed walls

# publications[].label
Film-cooling effectiveness on squealer rim walls and squealer cavity floor of a gas turbine blade tip using pressure sensitive paint

# publications[].label
Plasma boundary layer lifting systems for a gas turbine engine vane and corresponding method for operating a gas turbine engine

# publications[].label
Heat-transfer coefficients of a turbine blade-tip and near-tip regions

# publications[].label
Film Cooling Effectiveness on the Leading Edge of a Rotating Turbine Blade

# publications[].label
Turbulent Flow Heat Transfer and Friction in a Rectangular Channel With Varying Number of Ribbed Walls

# publications[].publisher
American Society of Mechanical Engineers

# publications[].label
Transonic Turbine-Vane Film Cooling with Showerhead Effect Using Pressure-Sensitive Paint Measurement Technique

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
AUGMENTED HEAT-TRANSFER IN RECTANGULAR CHANNELS OF NARROW ASPECT RATIOS WITH RIB TURBULATORS

# publications[].label
INFLUENCE OF UNSTEADY WAKE WITH TRAILING EDGE COOLANT EJECTION ON TURBINE BLADE FILM COOLING

# publications[].label
UNSTEADY WAKE EFFECT ON FILM EFFECTIVENESS AND HEAT-TRANSFER COEFFICIENT FROM A TURBINE BLADE WITH ONE ROW OF AIR AND CO2 FILM INJECTION

# publications[].label
Heat transfer coefficients and film cooling effectiveness on the squealer tip of a gas turbine blade

# publications[].label
Film-Cooling Effectiveness From Shaped Film Cooling Holes for a Gas Turbine Blade

# publications[].label
Pressure drop and mass transfer in two-pass ribbed channels

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Film-Cooling Effectiveness on a Rotating Turbine Platform Using Pressure Sensitive Paint Technique

# publications[].label
Prediction of Flow and Heat Transfer in Rotating Two-Pass Rectangular Channels With 45 Rib Turbulators

# publications[].label
Influence of mainstream turbulence on heat transfer coefficients from a gas turbine blade

# publications[].label
FALLING FILM EVAPORATION AND BOILING IN CIRCUMFERENTIAL AND AXIAL GROOVES ON HORIZONTAL TUBES

# publications[].label
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

# publications[].label
Effect of Squealer Geometry Arrangement on a Gas Turbine Blade Tip                     Heat Transfer

# publications[].label
Heat Transfer and Pressure Drop Correlations for Square Channels With V-Shaped Ribs at High Reynolds Numbers

# publications[].label
Heat Transfer in a Rotating, Two-Pass, Variable Aspect Ratio Cooling Channel With Profiled V-Shaped Ribs

# publications[].label
Influence of High Mainstream Turbulence on Leading Edge Film Cooling Heat Transfer

# publications[].label
FILM COOLING WITH FORWARD AND BACKWARD INJECTION FOR CYLINDRICAL AND FAN-SHAPED HOLES USING PSP MEASUREMENT TECHNIQUE

# publications[].label
Heat transfer coefficients on the squealer tip and near-tip regions of a gas turbine blade with single or double squealer

# publications[].label
Conjugate prediction of leading edge film cooling and heat transfer

# publications[].label
SURFACE HEATING EFFECT ON LOCAL HEAT-TRANSFER IN A ROTATING 2-PASS SQUARE CHANNEL WITH 60-DEG ANGLED RIB TURBULATORS

# publications[].label
Heat transfer in a two-pass rectangular rotating channel with 45-deg angled rib turbulators

# publications[].label
Influence of turbine blade leading edge shape on film cooling with cylindrical holes

# publications[].label
TURBINE BLADE FILM COOLING USING PSP TECHNIQUE

# publications[].publisher
Computers, Materials and Continua (Tech Science Press)

# publications[].label
Film Effectiveness Over a Flat Surface With Air and CO2 Injection Through Compound Angle Holes Using a Transient Liquid Crystal Image Method

# publications[].publisher
American Society of Mechanical Engineers

# publications[].label
Experimental Methods in Heat Transfer and Fluid Mechanics

# publications[].label
LOCAL ENDWALL HEAT/MASS TRANSFER IN A PIN FIN CHANNEL.

# publications[].label
Assessment of steady state PSP, TSP, and IR measurement techniques for flat plate film cooling

# publications[].label
Prediction of turbulent heat transfer in rotating smooth square ducts

# publications[].label
SIMULATION OF TURBULENT HEAT-TRANSFER IN A ROTATING DUCT

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Heat Transfer Coefficient on the Squealer Tip and Near Squealer Tip Regions of a Gas Turbine Blade

# publications[].label
Detailed Film Cooling Measurements on a Cylindrical Leading Edge Model: Effect of Free-Stream Turbulence and Coolant Density

# publications[].label
HEAT-TRANSFER CHARACTERISTICS OF TURBULENT-FLOW IN A SQUARE CHANNEL WITH ANGLED DISCRETE RIBS

# publications[].label
A Combined Numerical and Experimental Study of the Effect of Non-Axisymmetric Contouring on Performance and Film Cooling Behavior of a Rotating Turbine Endwall

# publications[].label
Effect of film hole row location on film effectiveness on a gas turbine blade

# publications[].label
Effect of Unsteady Wake on Full Coverage Film-Cooling Effectiveness for A Gas Turbine Blade

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Detailed heat transfer distributions under an array of orthogonal impinging jets

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
DEVELOPING HEAT-TRANSFER IN RECTANGULAR CHANNELS WITH RIB TURBULATORS

# publications[].label
Augmented Heat Transfer in Turbine Cooling Passages

# publications[].label
Influence of Surface Heating Condition on Local Heat Transfer in a Rotating Square Channel With Smooth Walls and Radial Outward Flow

# publications[].label
Unsteady wake effect on film effectiveness and heat transfer coefficient from a turbine blade with one row of air and CO<inf>2</inf>film injection

# publications[].label
Film-cooling effectiveness on a rotating blade platform

# publications[].label
Full-Scale Turbine Vane Endwall Film-Cooling Effectiveness Distribution Using Pressure-Sensitive Paint Technique

# publications[].label
IMPINGEMENT HEAT TRANSFER FROM JET ARRAYS ON TURBULATED TARGET WALLS AT LARGE REYNOLDS NUMBERS

# publications[].label
Turbine Blade Platform Film Cooling With Simulated Swirl Purge Flow and Slashface Leakage Conditions

# publications[].label
Internal cooling near trailing edge of a gas turbine airfoil with cooling airflow through blockages with holes

# publications[].label
Detailed heat transfer coefficient distributions under an array of impinging jets with coolant extraction

# publications[].label
Heat Transfer Coefficient and Film-Cooling Effectiveness on a Gas Turbine Blade Tip

# publications[].label
Detailed Film Cooling Measurements on a Cylindrical Leading Edge Model: Effect of Free-Stream Turbulence and Coolant Density

# publications[].publisher
American Society of Mechanical Engineers

# publications[].label
High Rotation Number Effects on Heat Transfer in a Rectangular (AR=2:1) Two-Pass Channel

# publications[].label
Flow and heat transfer in a rotating square channel with 45 deg angled ribs by Reynolds stress turbulence model

# publications[].label
Film cooling effectiveness distributions on a turbine blade cascade platform with stator-rotor purge and discrete film hole flows

# publications[].label
Heat transfer enhancement in rectangular channels with axial ribs or porous foam under through flow and impinging jet conditions

# publications[].label
AUGMENTED HEAT-TRANSFER IN TRIANGULAR DUCTS WITH FULL AND PARTIAL RIBBED WALLS

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
EFFECT OF UPSTREAM STEP ON FLAT PLATE FILM COOLING EFFECTIVENESS USING PSP

# publications[].label
Rotation effect on jet impingement heat transfer in smooth rectangular channels with heated target walls and film coolant extraction

# publications[].label
Heat Transfer in a Five-Pass Irregular Channel With and Without Pin Fins

# publications[].label
Influence of Coolant Density on Turbine Blade Platform Film-Cooling

# publications[].label
Unsteady wake over a linear turbine blade cascade with air co film injection: Part I - effect on heat transfer coefficients

# publications[].label
Film Cooling Effectiveness From Two Rows of Compound Angled Cylindrical Holes Using Pressure-Sensitive Paint Technique

# publications[].label
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

# publications[].label
Impingement heat transfer on dimpled surfaces using a transient liquid crystal technique

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Effect of Superposition on Spanwise Film-Cooling Effectiveness Distribution on a Gas Turbine Blade

# publications[].label
Heat transfer coefficients over a flat surface with air and CO2 injection through compound angle holes using a transient liquid crystal image method

# publications[].label
Float transfer and flow on the squealer tip of a gas turbine blade

# publications[].label
Flow and heat-transfer computations in rotating rectangular channels with V-shaped ribs

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
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

# publications[].label
Effectiveness Distributions on Turbine Blade Cascade Platforms through Simulated Stator-Rotor Seals

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Upstream vortex effects on turbine blade platform film cooling with typical stator-rotor purge flow

# publications[].label
Unsteady Wake Over a Linear Turbine Blade Cascade With Air and CO2 Film Injection: Part I  Effect on Heat Transfer Coefficients

# publications[].label
Film cooling effectiveness on the leading edge of a rotating film-cooled blade using pressure sensitive paint

# publications[].label
Flow and Heat Transfer in a Rotating Square Channel With 45 Angled Ribs by Reynolds Stress Turbulence Model

# publications[].label
Computation of Flow and Heat Transfer in Rotating Rectangular Channels (AR = 4) With V-Shaped Ribs by a Reynolds Stress Turbulence Model

# publications[].label
Numerical Simulation of Film Cooling on Rotating Blade Tips within a High-Pressure Turbine

# publications[].label
COMBINED EFFECT OF FREE-STREAM TURBULENCE AND UNSTEADY WAKE ON HEAT-TRANSFER COEFFICIENTS FROM A GAS-TURBINE BLADE

# publications[].label
Heat Transfer in a Rib and Pin Roughened Rotating Multipass Channel With Hub Turning Vane and Trailing-Edge Slot Ejection

# publications[].label
Turbine Platform Cooling and Blade Suction Surface Phantom Cooling From Simulated Swirl Purge Flow

# publications[].label
Numerical Prediction of Film Cooling and Heat Transfer on the Leading Edge of a Rotating Blade in a 1-1/2 Turbine Stage

# publications[].label
INFLUENCE OF HIGH MAINSTREAM TURBULENCE ON LEADING-EDGE HEAT-TRANSFER

# publications[].label
TURBINE VANE ENDWALL FILM COOLING WITH SLASHFACE LEAKAGE AND DISCRETE HOLE CONFIGURATION

# publications[].label
Professor Bengt Sunden on his 70th Birthday

# publications[].label
Effect of unsteady wake with trailing edge coolant ejection on detailed heat transfer coefficient distributions for a gas turbine blade

# publications[].label
INFLUENCE OF JET-GRID TURBULENCE ON FLAT-PLATE TURBULENT BOUNDARY-LAYER FLOW AND HEAT-TRANSFER

# publications[].label
TURBINE PLATFORM COOLING AND BLADE SUCTION SURFACE PHANTOM COOLING FROM SIMULATED SWIRL PURGE FLOW

# publications[].label
Impingement heat transfer measurements under an array of inclined jets

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Heat Transfer in a Two-Pass Rectangular Rotating Channel With 45 Angled Rib Turbulators

# publications[].label
Surface Heating Effect on Local Heat Transfer in a Rotating Two-Pass Square Channel With 60 Angled Rib Turbulators

# publications[].label
Film-Cooling Effectiveness on a Gas Turbine Blade Tip Using Pressure Sensitive Paint

# publications[].label
TURBINE BLADE LEADING EDGE COOLING WITH ONE ROW OF NORMAL OR TANGENTIAL IMPINGING JETS

# publications[].label
LEADING-EDGE FILM-COOLING HEAT-TRANSFER THROUGH ONE ROW OF INCLINED FILM SLOTS AND HOLES INCLUDING MAINSTREAM TURBULENCE EFFECTS

# publications[].label
Numerical Simulation of Flow and Heat Transfer in Rotating Cooling Passage With Turning Vane in Hub Region

# publications[].label
Effect of Squealer Geometry Arrangement on Gas Turbine Blade Tip Heat Transfer

# publications[].label
Influence of Film-Hole Shape and Angle on Showerhead Film Cooling Using PSP Technique

# publications[].label
Heat Transfer Enhancement in a Rectangular Cooling Channel With Airfoil Shaped Fins

# publications[].label
Rotation effect on jet impingement heat transfer in smooth rectangular channels with four heated walls and radially outward cross flow

# publications[].label
LOCAL ENDWALL HEAT/MASS TRANSFER AND PRESSURE DROP IN A PIN FIN CHANNEL WITH LATERAL FLOW EJECTION.

# publications[].label
Turbine Blade Trailing Edge Film Cooling Using PSP Technique

# publications[].label
Computation of flow and heat transfer in two-pass channels with 60 deg ribs

# publications[].label
Unsteady Wake and Coolant Density Effects on Turbine Blade Film Cooling Using Pressure Sensitive Paint Technique

# publications[].label
Influence of Mainstream Turbulence on Leading Edge Film Cooling Heat Transfer Through Two Rows of Inclined Film Slots

# publications[].label
Effect of model orientation and wall heating condition on local heat transfer in a rotating two-pass square channel with rib turbulators

# publications[].label
Heat Transfer Coefficients Over a Flat Surface With Air and CO2 Injection Through Compound Angle Holes Using a Transient Liquid Crystal Image Method

# publications[].label
Heat Transfer in Rotating Multipass Rectangular Ribbed Channel With and Without a Turning Vane

# publications[].label
Airfoil with plasma generator for shielding a boundary layer upstream of a film cooling hole and corresponding operating method

# publications[].label
The benefit of high-conductivity materials in film cooled turbine nozzles

# publications[].label
Computation of Flow and Heat Transfer in Turbine Blade Cooling Passages by Reynolds Stress Turbulence Model (Keynote Paper)

# publications[].label
Heat Transfer Enhancement in Channels With Turbulence Promoters

# publications[].label
Local heat transfer in a rotating two-pass ribbed triangular duct with two model orientations

# publications[].label
UNSTEADY WAKE OVER A LINEAR TURBINE BLADE CASCADE WITH AIR AND CO2 FILM INJECTION .1. EFFECT ON HEAT-TRANSFER COEFFICIENTS

# publications[].label
Local heat transfer in a rotating two-pass triangular duct with smooth walls

# publications[].label
Film temperature and effectiveness measurements on a cylindrical leading edge film cooling model

# publications[].label
Influence of Coolant Density on Turbine Blade Film-Cooling Using Pressure Sensitive Paint Technique

# publications[].label
Rib spacing effect on heat transfer in rotating two-pass ribbed channel (AR=1:2)

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
HEAT TRANSFER AND PRESSURE DROP IN BLADE COOLING CHANNELS WITH TURBULENCE PROMOTERS.

# publications[].label
Film-Cooling Effectiveness on a Rotating Blade Platform

# publications[].label
Computation of flow and heat transfer in rotating rectangular channels (AR=4 : 1) with pin-fins by a Reynolds stress turbulence model

# publications[].label
Pressure Loss Distribution in Three-Pass Rectangular Channels With Rib Turbulators

# publications[].label
Influence of Unsteady Wake With Trailing Edge Coolant Ejection on Turbine Blade Film Cooling

# publications[].label
Heat Transfer in Two-Pass Rotating Rectangular Channels (AR=1:2 and AR=1:4) With 45 Angled Rib Turbulators

# publications[].label
Turbine Vane Endwall Film Cooling With Slashface Leakage and Discrete Hole Configuration

# publications[].label
A transient liquid crystal thermography technique for gas turbine heat transfer measurements

# publications[].label
Effect of unsteady wake on film-cooling effectiveness distribution on a gas turbine blade with compound shaped holes

# publications[].label
Film Cooling Effectiveness of Transonic Turbine Vane Suction Side with Compound-Angle shaped hole configuration

# publications[].label
Internal heat transfer of film-cooled leading edge model with normal and tangential impinging jets

# publications[].label
Numerical Prediction of Film Cooling and Heat Transfer With Different Film-Hole Arrangements on the Plane and Squealer Tip of a Gas Turbine Blade

# publications[].label
Heat Transfer in a Rotating Two-Pass Rectangular Channel Featuring a Converging Tip Turn With Various 45 deg Rib Coverage Designs

# publications[].label
INFLUENCE OF MAINSTREAM TURBULENCE ON HEAT-TRANSFER COEFFICIENTS FROM A GAS-TURBINE BLADE

# publications[].label
Influence of Turbine Blade Leading Edge Profile on Film Cooling With Shaped Holes

# publications[].label
TURBINE BLADE TIP FILM-COOLING AND HEAT TRANSFER MEASUREMENTS AT HIGH BLOWING RATIOS

# publications[].label
Effect of Inlet Flow Angle on Gas Turbine Blade Tip Film Cooling

# publications[].label
A transient liquid crystal image technique for local heat transfer distributions near a sharp 180 turn of a two-pass smooth square channel

# publications[].label
EFFECT OF RIB ANGLE ON LOCAL HEAT MASS-TRANSFER DISTRIBUTION IN A 2-PASS RIB-ROUGHENED CHANNEL

# publications[].label
Full Coverage Film Cooling for a Turbine Blade with Axial Shaped Holes

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Impingement cooling in rotating two-pass rectangular channels

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Effect of Unsteady Wake on Detailed Heat Transfer Coefficient and Film Effectiveness Distributions for a Gas Turbine Blade

# publications[].label
Detailed heat transfer distributions in two-pass smooth and turbulated square channels with bleed holes

# publications[].label
Film-cooling effectiveness on squealer cavity and rim walls of gas-turbine blade tip

# publications[].label
Effect of unsteady wake on detailed heat transfer coefficient and film effectiveness distributions for a gas turbine blade

# publications[].label
Rotation Effect on Jet Impingement Heat Transfer in Smooth Rectangular Channels With Four Heated Walls and Radially Outward Crossflow

# publications[].label
HEAT TRANSFER AND PRESSURE LOSS MEASUREMENTS IN A TURBULATED HIGH ASPECT RATIO CHANNEL WITH LARGE REYNOLDS NUMBER FLOWS

# publications[].label
INFLUENCE OF HIGH MAINSTREAM TURBULENCE ON LEADING-EDGE FILM COOLING HEAT-TRANSFER

# publications[].label
TURBULENT HEAT-TRANSFER AND FRICTION IN A SQUARE CHANNEL WITH DISCRETE RIB TURBULATORS

# publications[].label
Heat transfer coefficient on the squealer tip and near squealer tip regions of a gas turbine blade

# publications[].label
Heat transfer in two-pass rotating rectangular channels (AR=2) with five different orientations of 45 deg V-shaped rib turbulators

# publications[].label
Heat Transfer Measurements in Rotating Blade–Shape Serpentine Coolant Passage With Ribbed Walls at High Reynolds Numbers

# publications[].label
Airfoil with plasma generator on trailing edge and corresponding operating method

# publications[].label
Computation of flow and heat transfer in two-pass channels with 60 deg ribs

# publications[].label
Effect of free-stream turbulence on turbine blade heat transfer and pressure coefficients in low Reynolds number flows

# publications[].label
Heat Transfer in Trailing Edge, Wedge Shaped Cooling Channels With Slot Ejection Under High Rotation Numbers

# publications[].label
Influence of Surface Heat Flux Ratio on Heat Transfer Augmentation in Square Channels With Parallel, Crossed and V-Shaped Angled Ribs

# publications[].label
Effect of Rib Angle on Local Heat/Mass Transfer Distribution in a Two-Pass Rib-Roughened Channel

# publications[].label
HEAT-TRANSFER AND FRICTION CHARACTERISTICS IN RECTANGULAR CHANNELS WITH RIB TURBULATORS

# publications[].label
Effect of Unsteady Wake With Trailing Edge Coolant Ejection on Film Cooling Performance for a Gas Turbine Blade

# publications[].publisher
American Society of Mechanical Engineers

# publications[].label
PIV flow measurements for heat transfer characterization in two-pass square channels with smooth and 90 degrees ribbed walls

# publications[].label
Gas Turbine Heat Transfer and Cooling Technology

# publications[].label
INFLUENCE OF COOLANT DENSITY ON TURBINE BLADE FILM-COOLING USING PRESSURE SENSITIVE PAINT TECHNIQUE

# publications[].label
Film cooling and heat transfer on two cutback trailing edge models with internal perforated blockages

# publications[].label
Local Heat/Mass Transfer Distributions Around Sharp 180 deg Turns in Two-Pass Smooth and Rib-Roughened Channels

# publications[].label
Effect of Coolant Density on Leading Edge Showerhead Film Cooling Using the Pressure Sensitive Paint Measurement Technique

# publications[].label
EFFECT OF RIB SPACING ON HEAT TRANSFER IN A TWO PASS RECTANGULAR CHANNEL (AR=2:1) AT HIGH ROTATION NUMBERS

# publications[].label
Turbine Blade Leading Edge Cooling With One Row of Normal or Tangential Impinging Jets

# publications[].label
Thermal Instability in Liquid Droplets on a Heated Surface

# publications[].label
TURBINE BLADE SURFACE PHANTOM COOLING FROM UPSTREAM NOZZLE TRAILING EDGE EJECTION

# publications[].label
Effect of Unsteady Wake With Trailing Edge Coolant Ejection on Film Cooling Performance for a Gas Turbine Blade

# publications[].label
FULL-SCALE TURBINE VANE END-WALL FILM-COOLING EFFECTIVENESS DISTRIBUTION USING PSP TECHNIQUE

# publications[].label
LOCAL HEAT-TRANSFER IN ENCLOSED CO-ROTATING DISKS WITH AXIAL THROUGHFLOW

# publications[].label
Turbine Vane Endwall Film Cooling From Cross-Row Configuration With Simulated Upstream Leakage Flow

# publications[].label
Jet-impingement heat transfer in rotating channels with staggered extraction flow

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Impingement cooling in rotating two-pass rectangular channels with ribbed walls

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Effect of rib-angle orientation on local mass transfer distribution in a three-pass rib-roughened channel

# publications[].label
Swirl Impinging Cooling on an Airfoil Leading Edge Model at Large Reynolds Number

# publications[].label
High rotation number effect on heat transfer in a trailing edge channel with tapered ribs

# publications[].label
Turbulent flow and heat transfer in rotating different aspect ratio channels

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
INFLUENCE OF SHOCK WAVE ON TURBINE VANE SUCTION SIDE FILM COOLING WITH COMPOUND-ANGLE SHAPED HOLES

# publications[].label
Impingement Heat Transfer From Jet Arrays on Turbulated Target Walls at Large Reynolds Numbers

# publications[].label
Airfoil with plasma generator at leading edge for vortex reduction and corresponding operating method

# publications[].label
Unsteady Wake Effect on Film Temperature and Effectiveness Distributions for a Gas Turbine Blade

# publications[].label
Conjugate heat transfer in channels with internal longitudinal fins

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Heat Transfer Coefficients on the Squealer Tip and Near Tip Regions of a Gas Turbine Blade With Single or Double Squealer

# publications[].label
Experimental Investigation of the Effect of Purge Flow on Film Cooling Effectiveness on a Rotating Turbine With Nonaxisymmetric End Wall Contouring

# publications[].label
UNSTEADY WAKE OVER A LINEAR TURBINE BLADE CASCADE WITH AIR AND CO2 FILM INJECTION .2. EFFECT ON FILM EFFECTIVENESS AND HEAT-TRANSFER DISTRIBUTIONS

# publications[].label
Gas Turbine Heat Transfer and Cooling Technology

# publications[].label
Experimental and Computational Film Cooling with Backward Injection for Cylindrical and Fan-Shaped Holes

# publications[].label
APPLICATION OF ADIABATIC FILM COOLING EFFECTIVENESS TO NON-ADIABATIC BLADE COOLING DESIGN.

# publications[].label
Rotation effect on jet impingement heat transfer in smooth rectangular channels with heated target walls and radially outward cross flow

# publications[].label
SURFACE HEAT TRANSFER VISUALIZATION ON A MODEL GAS TURBINE BLADE USING A TRANSIENT LIQUID CRYSTAL IMAGE TECHNIQUE

# publications[].label
Turbulent flow heat transfer and friction in a rectangular channel with varying numbers of ribbed walls

# publications[].label
Heat Transfer in Rotating Rectangular Channels (AR = 4:1) With V-Shaped and Angled Rib Turbulators With and Without Gaps

# publications[].label
INFLUENCE OF SURFACE HEATING CONDITION ON LOCAL HEAT-TRANSFER IN A ROTATING SQUARE CHANNEL WITH SMOOTH WALLS AND RADIAL OUTWARD FLOW

# publications[].label
Overall effectiveness of film-cooled leading edge model with normal and tangential impinging jets

# publications[].label
Residual stresses in 3LPO external pipeline coatings - Disbondment and cracking

# publications[].label
Heat transfer prediction of rotating rectangular channels using Reynolds stress model

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Heat Transfer, Pressure Drop, and Mass Flow Rate in Pin Fin Channels With Long and Short Trailing Edge Ejection Holes

# publications[].label
Full-coverage film cooling for a turbine blade with axial-shaped holes

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Prediction of flow and heat transfer in rotating two-pass rectangular channels with 45-deg rib turbulators

# publications[].label
Local heat transfer in rotating smooth and ribbed two-pass square channels with three channel orientations

# publications[].label
Turbine Blade Platform Film Cooling With Fan-Shaped Holes Under Simulated Swirl Purge Flow and Slashface Leakage Conditions

# publications[].label
HEAT TRANSFER IN TRAILING EDGE WEDGE-SHAPED PIN-FIN CHANNELS WITH SLOT EJECTION UNDER HIGH ROTATION NUMBERS

# publications[].label
EFFECT OF RIB SPACING ON HEAT TRANSFER IN A TWO-PASS RECTANGULAR CHANNEL (AR=1:4) WITH A SHARP ENTRANCE AT HIGH ROTATION NUMBERS

# publications[].label
Effect of unsteady wake with trailing edge coolant ejection on film cooling performance for a gas turbine blade

# publications[].label
MEASUREMENT OF HEAT TRANSFER AND PRESSURE DROP IN RECTANGULAR CHANNELS WITH TURBULENCE PROMOTERS.

# publications[].label
Heat transfer in two-pass rotating rectangular channels (AR=2:1) with discrete ribs

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Local heat transfer coefficient and film effectiveness distributions on a cylindrical leading edge model using a transient liquid crystal image method

# publications[].label
AUGMENTED HEAT-TRANSFER IN A PIN FIN CHANNEL WITH SHORT OR LONG EJECTION HOLES

# publications[].label
Heat Transfer and Pressure Distributions on A Gas Turbine Vane End-Wall

# publications[].label
On flow separation with adverse rotational buoyancy

# publications[].label
Structural Foam Surface Finishes are Practically Perfect Now

# publications[].label
Influence of entrance geometry on heat transfer in rotating rectangular cooling channels (AR=4:1) with angled ribs

# publications[].label
Local endwall heat/mass-transfer distributions in pin fin channels

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Gas Turbine Heat Transfer and Cooling Technology, Second Edition

# publications[].label
Experimental Investigation of the Effect of Purge Flow on Film Cooling Effectiveness on a Rotating Turbine with Non-Axisymmetric Endwall Contouring

# publications[].label
Turbine Blade Platform Film Cooling with Typical Stator-Rotor Purge Flow and Discrete-Hole Film Cooling

# publications[].label
Numerical study of film cooled rotor leading edge with tip clearance in 1-1/2 turbine stage

# publications[].label
Surface Heating Effect on Local Heat Transfer in an Enclosed CoRotating Disks with Axial Throughflow

# publications[].label
A REVIEW OF HOLE GEOMETRY AND COOLANT DENSITY EFFECT ON FILM COOLING

# publications[].publisher
Computers, Materials and Continua (Tech Science Press)

# publications[].label
Buoyancy effects on heat transfer in five different aspect-ratio rectangular channels with smooth walls and 45-degree ribbed walls

# publications[].label
Heat Transfer, Pressure Drop, and Mass Flow Rate in Pin Fin Channels With Long and Short Trailing Edge Ejection Holes

# publications[].label
Heat transfer in two-pass rotating rectangular channels (AR=2) with parallel and crossed 45 V-shaped rib turbulators

# publications[].label
HEAT TRANSFER AND FRICTION IN SQUARE DUCTS WITH TWO OPPOSITE RIB-ROUGHENED WALLS.

# publications[].label
Heat transfer in two-pass rotating rectangular channels (AR=1:2 and AR=1:4) with 45 deg angled rib turbulators

# publications[].label
Heat transfer in rotating rectangular cooling channels (AR=4) with angled ribs

# publications[].label
Computation of Discrete-Hole Film Cooling by a Near-Wall Second-Moment Turbulence Closure

# publications[].label
Recent Development in Turbine Blade Film Cooling

# publications[].label
Computation of flow and heat transfer in rotating two-pass rectangular channels (AR=1 : 1, 1 : 2, and 1 : 4) with smooth walls by a Reynolds stress turbulence model

# publications[].label
Assessment of a near-wall second-moment closure for rotating multiple-pass cooling channels

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
An investigation of heat transfer and friction for rib-roughened surfaces

# publications[].label
A Combined Experimental and Numerical Study of the Turbine Blade Tip Film Cooling Effectiveness under Rotation Condition

# publications[].label
LOCAL HEAT TRANSFER COEFFICIENT AND FILM EFFECTIVENESS DISTRIBUTIONS ON A CYLINDRICAL LEADING EDGE MODEL USING A TRANSIENT LIQUID CRYSTAL IMAGE METHOD

# publications[].label
Prediction of turbulent flow and heat transfer in rotating square and rectangular smooth channels

# publications[].label
Effect of Film-Hole Shape on Turbine-Blade Heat-Transfer Coefficient Distribution

# publications[].label
Rib-Spacing Effect on Heat Transfer in Rectangular Channels at High Rotation Numbers

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
TURBULENT HEAT-TRANSFER AND FRICTION IN PIN FIN CHANNELS WITH LATERAL FLOW EJECTION

# publications[].label
Detailed heat transfer distributions in two-pass square channels with rib turbulators

# publications[].label
A Numerical Study of Flow and Heat Transfer in Rotating Rectangular Channels (AR=4) With 45 Rib Turbulators by Reynolds Stress Turbulence Model

# publications[].label
Detailed heat transfer distributions in two-pass square channels with rib turbulators and bleed holes

# publications[].label
Heat transfer distributions on a cylinder with simulated thermal barrier coating spallation

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
A Computer Model for Gas Turbine Blade Cooling Analysis

# publications[].label
Influence of Channel Orientation on Heat Transfer in a Two-Pass Smooth and Ribbed Rectangular Channel (AR=2:1) Under Large Rotation Numbers

# publications[].label
Turbine Vane Endwall Film Cooling Comparison From Five Film-Hole Design Patterns and Three Upstream Injection Angles

# publications[].label
Numerical Prediction of Flow and Heat Transfer in a Two-pass Square Channel with 90 Ribs

# publications[].label
MEASUREMENT AND MODELLING OF BLADE TIP COOLING IN GAS TURBINES

# publications[].label
A Predictive Model for Preliminary Gas Turbine Blade Cooling Analysis

# publications[].label
Rotation Effect on Jet Impingement Heat Transfer in Smooth Rectangular Channels With Four Heated Walls and Film Coolant Extraction

# publications[].label
HIGH-PERFORMANCE HEAT-TRANSFER DUCTS WITH PARALLEL BROKEN AND V-SHAPED BROKEN RIBS

# publications[].label
HEAT TRANSFER ENHANCEMENT FOR TURBINE BLADE INTERNAL COOLING

# publications[].label
Effect of a cutback squealer and cavity depth on film-cooling effectiveness on a gas turbine blade tip

# publications[].label
Heat transfer in rotating rectangular channels with V-shaped and angled ribs

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Visualization of Flow Patterns in Plastic Injection Molds

# publications[].label
The New Thermal Cycling Process for Structural Foam Smooth Surface

# publications[].label
Airfoil leading edge end wall vortex reducing plasma

# publications[].label
WALL HEATING EFFECT ON LOCAL HEAT-TRANSFER IN A ROTATING 2-PASS SQUARE CHANNEL WITH 90-DEGREES RIB TURBULATORS

# publications[].label
HEAT-TRANSFER ENHANCEMENT IN CHANNELS WITH TURBULENCE PROMOTERS

# publications[].label
UNEVEN WALL TEMPERATURE EFFECT ON LOCAL HEAT-TRANSFER IN A ROTATING 2-PASS SQUARE CHANNEL WITH SMOOTH WALLS

# publications[].label
Effect of model orientation on local heat transfer in a rotating two-pass smooth triangular duct

# publications[].label
Effect of non-traditional rib-profiles on heat transfer and friction in turbulent channel flows

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Effect of a cutback squealer and cavity depth on film-cooling effectiveness on a gas turbine blade tip

# publications[].label
Film cooling on a gas turbine blade pressure side or suction side with axial shaped holes

# publications[].label
Local Heat Transfer in Channels with Pin Fins Via the Naphthalene Sublimation Technique

# publications[].label
Numerical study of a rotating blade platform with film cooling from cavity purge flow in a 1-% turbine stage

# publications[].label
Heat transfer performance comparisons of five different rectangular channels with parallel angled ribs

# publications[].label
Influence of high mainstream turbulence on leading edge film cooling heat transfer

# publications[].label
INFLUENCE OF COOLANT DENSITY ON TURBINE BLADE PLATFORM FILM-COOLING

# publications[].label
Influence of surface heating condition on local heat transfer in enclosed corotating disks with axial throughflow

# publications[].label
Measurements of wall heat (mass) transfer for flow through blockages with round and square holes in a wide rectangular channel

# publications[].label
Turbine Blade Platform Film Cooling With Typical Stator-Rotor Purge Flow and Discrete-Hole Film Cooling

# publications[].label
Influence of Mainstream Turbulence on Leading Edge Film Cooling Heat Transfer Through Two Rows of Inclined Film Slots

# publications[].label
Heat Transfer Through Falling Film Evaporation and Boiling on Horizontal Tubes

# publications[].label
A REVIEW OF HOLE GEOMETRY AND COOLANT DENSITY EFFECT ON FILM COOLING

# publications[].label
Transonic Turbine Vane Suction Side Film Cooling With Showerhead Effect Using PSP Measurement Technique

# publications[].label
Turbulent Heat Transfer Enhancement and Surface Heating Effect in Square Channels with Wavy, and Twisted Tape Inserts with Interrupted Ribs

# publications[].label
Effect of Film Injection Location on Local Heat Transfer Coefficient on a Gas Turbine Blade

# publications[].label
Influence of surface heat flux ratio on heat transfer augmentation in square channels with parallel, crossed, and V-shaped angled ribs

# publications[].label
HIGH ROTATION NUMBER EFFECTS ON HEAT TRANSFER IN A RECTANGULAR (AR=2:1) TWO PASS CHANNEL

# publications[].label
Thermal instability in spherical liquid shells induced by surface tension

# publications[].label
Thermal performance of angled, V-shaped, and W-shaped rib turbulators in rotating rectangular cooling channels (AR=4:1)

# publications[].label
TURBINE BLADE LEADING EDGE IMPINGEMENT COOLING FROM NORMAL OR TANGENTIAL JETS WITH CROSSFLOW EFFECT

# publications[].publisher
Computers, Materials and Continua (Tech Science Press)

# publications[].label
Reynolds number effect on leading edge film effectiveness and heat transfer coefficient

# publications[].label
Experimental heat transfer in a rotating triangular duct: Effect of model orientation

# publications[].label
Heat Transfer in Rotating Rectangular Cooling Channels (AR=4) With Dimples

# publications[].label
Heat Transfer and Flow Predictions in a Rotating Square Duct with Coriolis-Modified Turbulence Models

# publications[].label
Rotational buoyancy effects on heat transfer in five different aspect-ratio rectangular channels with smooth walls and 45 degree ribbed walls

# publications[].label
MAINSTREAM TURBULENCE EFFECT ON FILM EFFECTIVENESS AND HEAT-TRANSFER COEFFICIENT OF A GAS-TURBINE BLADE WITH AIR AND CO2 FILM INJECTION

# publications[].label
Film effectiveness over a flat surface with air and CO2 injection through compound angle holes using a transient liquid crystal image method

# publications[].label
Heat Transfer and Pressure Drop Correlations for Square Channels With 45 Deg Ribs at High Reynolds Numbers

# publications[].label
Effect of film-hole shape on turbine-blade film-cooling performance

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Heat Transfer in Trailing-Edge Channels with Slot Ejection Under High Rotation Numbers

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Computation of heat transfer in rotating two-pass square channels by a second-moment closure model

# publications[].label
Rotation effect on jet impingement heat transfer in smooth rectangular channels with four heated walls and radially outward crossflow

# publications[].label
Computation of Flow and Heat Transfer in Two-Pass Rotating Rectangular Channels (AR=1:1, AR=1:2, AR=1:4) With 45-deg. Angled Ribs by Reynolds Stress Turbulence Model

# publications[].label
Numerical prediction of turbulent heat transfer in a rotating square duct with variable rotational buoyancy effects

# publications[].label
Heat transfer in a two-pass rectangular channel (AR=1 : 4) under high rotation numbers

# publications[].label
Effectiveness distributions on turbine-blade cascade platforms through simulated stator-rotor seals

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Heat transfer coefficients and film-cooling effectiveness on a gas turbine blade tip

# publications[].label
Heat Transfer in Two-Pass Rotating Rectangular Channels (AR=2:1) With Discrete V-Shaped and Discrete Angled Rib Turbulators

# publications[].label
High Rotation Number Effect on Heat Transfer in a Triangular Channel With 45 deg, Inverted 45 deg, and 90 deg Ribs

# publications[].label
Unsteady Wake Over a Linear Turbine Blade Cascade With Air and CO2 Film Injection: Part II  Effect on Film Effectiveness and Heat Transfer Distributions

# publications[].publisher
American Society of Mechanical Engineers

# publications[].label
Effect of unsteady wake with trailing edge coolant ejection on detailed heat transfer coefficient distributions for a gas turbine blade

# publications[].label
Heat Transfer in Rotating Serpentine Coolant Passage with Ribbed Walls at Low Mach Numbers

# publications[].label
Film-cooling prediction on rotor blade leading edge in 1-1/2 turbine stage

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Effect of rotation on heat transfer in rectangular channels with pin fins

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Effects of rim location, rim height, and tip clearance on the tip and near tip region heat transfer of a gas turbine blade

# publications[].label
Heat Transfer and Pressure Drop Measurements for a Square Channel With 45 deg Round-Edged Ribs at High Reynolds Numbers

# publications[].label
Flow and Heat Transfer Prediction On Turbine Rotor Blade with Various Tip Configurations

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Influence of Coolant Density on Turbine Blade Film-Cooling With Axial and Compound Shaped Holes

# publications[].label
Detailed Heat Transfer Coefficient Measurements on a Scaled Realistic Turbine Blade Internal Cooling System

# publications[].label
Transonic Turbine Vane Endwall Film Cooling Using the Pressure-Sensitive Paint Measurement Technique

# publications[].label
Augmented Heat Transfer in Square Channels with Wedge-Shaped and Delta-Shaped Turbulence Promoters

# publications[].label
Detailed film cooling measurements over a gas turbine blade using a transient liquid crystal image technique

# publications[].label
Effect of jet grid turbulence on turbulent boundary layer heat transfer

# publications[].label
Influence of high mainstream turbulence on leading edge heat transfer

# publications[].label
INFLUENCE OF HIGH MAINSTREAM TURBULENCE ON LEADING-EDGE FILM COOLING HEAT-TRANSFER - EFFECT OF FILM HOLE SPACING

# publications[].label
THE APPLICATION OF ADIABATIC FILM COOLING EFFECTIVENESS TO NON-ADIABATIC BLADE COOLING DESIGN

# publications[].label
Prediction of Turbulent Flow and Heat Transfer in Rotating Square and Rectangular Smooth Channels

# publications[].label
Influence of high mainstream turbulence on leading edge film cooling heat transfer: effect of film hole spacing

# publications[].label
INFLUENCE OF CONCURRENT STEAM SHEAR VELOCITY ON FALLING FILM EVAPORATION AND BOILING ON A HORIZONTAL TUBE.

# publications[].label
Numerical Simulation of Flow and Heat Transfer in Rotating Cooling Passage with Turning Vane in Hub Region

# publications[].label
Film cooling effectiveness for three-row compound angle hole design on flat plate using PSP technique

# publications[].label
Heat Transfer in Rotating, Trailing-Edge, Converging Channels With Smooth Walls and Pin-Fins

# publications[].label
HEAT TRANSFER IN A RIB AND PIN ROUGHENED ROTATING MULTI-PASS CHANNEL WITH HUB TURNING VANE AND TRAILING-EDGE SLOT EJECTION

# publications[].label
Film Effectiveness Over a Flat Surface With Air and CO2 Injection Through Compound Angle Holes Using a Transient Liquid Crystal Image Method

# publications[].label
Effect of rotation on heat transfer in two-pass square channels with five different orientations of 45 degrees angled rib turbulators

# publications[].label
Assessment of steady state PSP and transient IR measurement techniques for leading edge film cooling

# publications[].label
Turbine blade cooling studies at Texas A&M University: 1980-2004

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Effect of rotation on leading edge region film cooling of a gas turbine blade with three rows of film cooling holes

# publications[].label
Effect of Upstream Wake With Vortex on Turbine Blade Platform Film Cooling With Simulated Stator-Rotor Purge Flow

# publications[].label
Computation of flow and heat transfer in rotating rectangular channels (AR=4 : 1) with pin-fins by a Reynolds stress turbulence model

# publications[].label
Local heat transfer in a rotating two-pass triangular duct with smooth walls

# publications[].label
Turbine vane endwall film cooling from mid-chord or downstream rows and upstream coolant injection

# publications[].label
EFFECTS OF FIN CONFIGURATION AND ENTRANCE LENGTH ON LOCAL ENDWALL HEAT/MASS TRANSFER IN A PIN FIN CHANNEL.

# publications[].label
Thermal Performance of Angled, V-Shaped, and W-Shaped Rib Turbulators in Rotating Rectangular Cooling Channels (AR = 4:1)

# publications[].label
UNSTEADY WAKE AND COOLANT DENSITY EFFECTS ON TURBINE BLADE FILM COOLING USING PSP TECHNIQUE

# publications[].label
Heat Transfer Characteristics of Turbulent Flow in a Square Channel With Angled Discrete Ribs

# publications[].publisher
American Society of Mechanical Engineers

# publications[].label
Heat Transfer and Friction Characteristics of Turbulent Flow in Circular Tubes with Twisted-Tape Inserts and Axial Interrupted Ribs

# publications[].label
Influence of Rotation on Heat Transfer from a Two-Pass Channel with Periodically Placed Turbulence and Secondary Flow Promoters

# publications[].label
Heat transfer inside and downstream of cavities using transient liquid crystal method

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
Computation of Flow and Heat Transfer in Rotating Two-Pass Square Channels by a Reynolds Stress Model

# publications[].label
Detailed film cooling measurements on a cylindrical leading edge model: Effect of free-stream turbulence and coolant density

# publications[].label
Film Cooling With Steam Injection Through Three Staggered Rows of Inclined Holes Over a Straight Airfoil

# publications[].label
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

# publications[].label
Heat Transfer and Pressure Drop Measurements in a High Aspect Ratio Channel With Circular Pins and Strip Fins

# publications[].label
Jet impingement cooling in rotating two-pass rectangular channels with smooth walls

# publications[].publisher
American Institute of Aeronautics and Astronautics (AIAA)

# publications[].label
HEAT TRANSFER ENHANCEMENT FOR TURBINE BLADE INTERNAL COOLING

# publications[].label
Turbine Vane Endwall Film Cooling Study From Axial-Row Configuration With Simulated Upstream Leakage Flow

# publications[].label
Influence of Coolant Density on Turbine Blade Film-Cooling Using Pressure Sensitive Paint Technique

# streetAddress
Texas A&M University; Mechanical Engineering; 3123 TAMU

# organizations[]
Texas A&M Engineering Experiment Station (TEES)

# schools[]
Texas A&M Engineering Experiment Station (TEES)

# etdChairOf[].label
Liu, Yao-Hsien (2005-08). Effect of rib spacing on heat transfer and friction in a rotating two-pass rectangular (AR=1:2) channel. Master's Thesis.

# etdChairOf[].label
Ahn, Jaeyong (2005-12). Film cooling effectiveness measurements on rotating and non-rotating turbine components. Doctoral Dissertation.

# etdChairOf[].label
Liu, Yao-Hsien (2008-12). Heat transfer in leading and trailing edge cooling channels of the gas turbine blade under high rotation numbers. Doctoral Dissertation.

# etdChairOf[].label
Liu, Kuo-Chun (2010-01). Blowing Ratio Effects on Film Cooling Effectiveness. Master's Thesis.

# etdChairOf[].label
Lei, Jiang 1980- (2011-08). Heat Transfer in Rectangular Channels (AR=2:1) of the Gas Turbine Blade at High Rotation Numbers. Doctoral Dissertation.

# etdChairOf[].label
Ullah, Izhar (2018-07). Flat Plate Film Cooling with Linear and Curved Round-to-Diffusion Shaped Slots Using PSP Measurement Technique. Master's Thesis.

# etdChairOf[].label
Chu, Hung-Chieh 1979- (2012-11). Numerical Simulation of Flow and Heat Transfer in Internal Multi-Pass Cooling Channel within Gas Turbine Blade. Master's Thesis.

# etdChairOf[].label
Lu, Kun (2014-12). Numerical Investigations of Flow and Film Cooling with Endwall Contouring and Blade Tip Ejection under Rotating Turbine Conditions. Doctoral Dissertation.

# etdChairOf[].label
Li, Shiou-Jiuan (2012-12). Experimental Investigation of Film Cooling Effectiveness on Gas Turbine Blades. Doctoral Dissertation.

# etdChairOf[].label
Choi, Jungho (2004-12). An experimental investigation of turbine blade heat transfer and turbine blade trailing edge cooling. Doctoral Dissertation.

# etdChairOf[].label
Lee, Jiyeon (2015-09). The Effect of Mainstream Turbulence on Turbine Blade Platform Cooling with Simulated Swirl Purge Flow. Master's Thesis.

# etdChairOf[].label
Varvel, Trent Alan (2004-12). Shaped hole effects on film cooling effectiveness and a comparison of multiple effectiveness measurement techniques. Master's Thesis.

# etdChairOf[].label
Narzary, Diganta P. (2010-10). Experimental Study of Gas Turbine Blade Film Cooling and Heat Transfer. Doctoral Dissertation.

# etdChairOf[].label
Zhang, Mingjie (2018-11). Experimental and Numerical Investigation of Turbine Blade Leading Edge Heat Transfer with Jet Impingement and Film Cooling. Doctoral Dissertation.

# etdChairOf[].label
Fu, Wen-Lung (2005-05). Aspect ratio effect on heat transfer in rotating two-pass rectangular channels with smooth walls and ribbed walls. Doctoral Dissertation.

# etdChairOf[].label
Alkhamis, Nawaf Yahya (2010-10). Heat Transfer and Pressure Drop Measurement for Square Channels with V-shape Ribs at High Reynolds Numbers. Master's Thesis.

# etdChairOf[].label
Chen, Andrew F (2013-12). Film Cooling with Forward and Backward Injection for Cylindrical and Fan-shaped Holes Using PSP Measurement Technique. Master's Thesis.

# etdChairOf[].label
Chen, Andrew F (2018-04). Turbine Platform Film Cooling Effectiveness and Rotational Effect on Internal Cooling Passages with a Converging Tip Turn. Doctoral Dissertation.

# etdChairOf[].label
Yang, Shangfeng (2014-12). Turbine Vane Film Cooling and Internal Rotating Coolant Passage Heat Transfer. Doctoral Dissertation.

# etdChairOf[].label
Blake, Sarah Anne (2007-05). Turbine blade platform film cooling with simulated stator-rotor purge flow with varied seal width and upstream wake with vortex. Master's Thesis.

# etdChairOf[].label
Chowdhury, MD Nafiz Hossain Khan (2017-05). Measurements and Assessment of Adiabatic Film Cooling Performance on a Gas Turbine Vane Endwall Using PSP Technique. Doctoral Dissertation.

# etdChairOf[].label
Wang, Nian (2018-12). Turbine Blade Internal Heat Transfer and Film Cooling Studies. Doctoral Dissertation.

# etdChairOf[].label
Bashir, Muhammad Hassan (2016-07). Film Cooling Effectiveness for Three Row Compound Hole Design on Flat Plate Using PSP Technique. Master's Thesis.

# etdChairOf[].label
Su, Guoguang (2005-12). Numerical simulation of flow and heat transfer of internal cooling passage in gas turbine blade. Doctoral Dissertation.

# etdChairOf[].label
Zirakzadeh, Hootan (2014-08). Numerical Investigation of Temperature Distribution on a High Pressure Gas Turbine Blade. Master's Thesis.

# etdChairOf[].label
Rezasoltani, Mohsen (2015-12). Experimental Investigations of Flow and Film Cooling with Endwall Contouring and Blade Tip Ejection under Rotating Turbine Conditions. Doctoral Dissertation.