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

# overview
Lesley M. Wright is associate professor and Jana and Quentin A. Baker '78 faculty fellow at Texas A&M University. Prior to joining Texas A&M, she was a member of the mechanical engineering faculty at Baylor University for ten years. She earned a BS in engineering in 2001 at Arkansas State University and an MS and a PhD in mechanical engineering at Texas A&M University in 2003 and 2006, respectively. Currently she is investigating enhanced convective cooling technology, including heat transfer enhancement for gas turbine cooling applications. This experimental research has led to the development of innovative cooling technology for both turbine blade film cooling and internal heat transfer enhancement. In addition, Dr. Wright continues to investigate the effect of rotation on the thermal performance of rotor blade cooling passages. Her research interests have also led to the development of novel experimental methods for the acquisition of detailed surface and flow measurements in highly turbulent flows. She has co-authored the book Experimental Methods in Heat Transfer and Fluid Mechanics and over 100 refereed journal and conference papers. She is a fellow of ASME.

# 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[]
Networking And Information Technology R&d (nitrd)

# 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[]
Turbine Blade And Measurement Advancements

# 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[]
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[]
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

# educationAndTraining[].organization.label
Texas A&M University - (College Station, Texas, United States)

# educationAndTraining[].organization.label
Texas A&M University - (College Station, Texas, United States)

# educationAndTraining[].organization.label
Arkansas State University - (Jonesboro, Arkansas, United States)

# educationAndTraining[].field
Engineering with Professional Concentration in Mechanical Engineering

# awardsAndHonors[].label
Journal of Heat Transfer Outstanding Reviewer

# awardsAndHonors[].label
Society of Automotive Engineers Faculty Advisor

# awardsAndHonors[].label
North Texas Section Young Engineer of the Year

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

# publications[].label
TURNING REGION HEAT TRANSFER IN FIVE, STATIONARY AND ROTATING, MULTI-PASS CHANNELS WITH VARIOUS ASPECT RATIOS

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

# 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
REVIEW OF PLATFORM COOLING TECHNOLOGY FOR HIGH PRESSURE TURBINE BLADES

# publications[].label
MEASUREMENT OF DETAILED HEAT TRANSFER COEFFICIENT AND FILM COOLING EFFECTIVENESS DISTRIBUTIONS USING PSP AND TSP

# publications[].label
Effect of Flow Acceleration on Mainstream-to-Coolant Flow Interaction for Round and Shaped Film Cooling Holes

# publications[].label
Interaction of Flow and Film Cooling Effectiveness Between Double-Jet Film-Cooling Holes With Various Spanwise Distances

# publications[].label
Film Cooling Effectiveness Distributions on a Flat Plate With a Double Hole Geometry Using PSP

# publications[].label
APPLICATION OF S-PIV FOR INVESTIGATION OF ROUND AND SHAPED FILM COOLING HOLES AT HIGH DENSITY RATIOS

# publications[].label
Evaluation of Wavy-Trailing-Edge Film Cooling Versus Pressure Side Cutback Cooling

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

# publications[].label
Heat Transfer in a Rotating, Blade-Shaped, Two-Pass Cooling Channel With Various 45-Deg Rib Turbulators and a Tip Turning Vane

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

# publications[].label
ANALYSIS OF FILM COOLING EFFECTIVENESS ON A GAS TURBINE BLADE WITH AN UNSTEADY WAKE USING FAST RESPONSE PRESSURE SENSITIVE PAINT

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

# publications[].label
Interaction of Flow and Film-Cooling Effectiveness Between Double-Jet Film-Cooling Holes With Various Spanwise Distances

# publications[].label
Influence of Coolant Density on Turbine Blade Tip Film Cooling at Transonic Cascade Flow Conditions Using the Pressure-Sensitive Paint Technique

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

# publications[].label
LEADING EDGE JET IMPINGEMENT UNDER HIGH ROTATION NUMBERS

# publications[].label
Effect of Dimple Depth on Heat Transfer Enhancement in a Rectangular Channel (AR = 3:1) with Hemispherical Dimples

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

# publications[].label
Effect of Freestream Turbulence Intensity on Film Cooling Jet Structure and Surface Effectiveness Using PIV and PSP

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

# publications[].label
Effects of Blowing and Density Ratios on Unsteady Film Cooling Effectiveness Using Fast-Response Pressure-Sensitive Paint

# publications[].label
ASSESSMENT OF A DOUBLE HOLE FILM COOLING GEOMETRY USING S-PIV AND PSP

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

# 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
Thermal Characterization of a Turbulent Free Jet With Planar Laser-Induced Fluorescence

# publications[].label
Temperature Field Reconstruction of Surfaces Heated Through Radiative Heat Transfer Using Convolutional Neural Networks

# 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
FILM COOLING EFFECTIVENESS DISTRIBUTIONS ON A FLAT PLATE WITH A DOUBLE HOLE GEOMETRY USING PSP

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

# publications[].label
Experimental investigation of turbine blade platform film cooling and rotational effect on trailing edge internal cooling

# publications[].label
Parametric Study and Correlation of Racetrack Shaped Jets for Leading Edge Impingement

# publications[].label
TPIV Experimental Investigation of Film Coolant-to-Mainstream Interaction From Shaped Cooling Holes With Various Inlet Geometries

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

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

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

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

# publications[].label
COMPARISON OF STAGGERED AND IN-LINE V-SHAPED DIMPLE ARRAYS USING S-PIV

# publications[].label
Effect of Coolant Ejection in Rectangular and Trapezoidal Trailing Edge Cooling Passages

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

# publications[].label
Impingement Heat Transfer on a Cylindrical, Concave Surface With Varying Jet Geometries

# 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
Assessment of Binary Pressure Sensitive Paint for Temperature and Heat Transfer Coefficient Measurement of Leading Edge Film Cooling

# publications[].label
HEAT TRANSFER ENHANCEMENT IN A RECTANGULAR (AR=3:1) CHANNEL WITH V-SHAPED DIMPLES

# publications[].label
NUMERICAL STUDY ON COOLING CHARACTERISTICS OF DOUBLE-ROW CYLINDRICAL HOLES ON UPSTREAM ENDWALL

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

# publications[].label
Periodic Unsteady Flow Aerodynamics and Heat Transfer: Studies on a Curved Surface, Combined Part I and II

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

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

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

# publications[].label
Effect of Strip-Fin Height On Jet Impingement Heat Transfer in a Rectangular Channel At Two Jet-to-target Surface Spacings

# publications[].label
Effects of Jet-to-Target Surface Spacing and Pin-Fin Height on Jet Impingement Heat Transfer in a Rectangular Channel

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

# publications[].label
Influence of Entrance Geometry on Heat Transfer in Narrow Rectangular Cooling Channels (AR = 4:1) With Angled Ribs

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

# 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
Film Cooling Comparison of Full-Scale Turbine Vanes Using the Pressure Sensitive Paint Technique

# publications[].label
TPIV Experimental Investigation of Film Coolant-to-Mainstream Interaction From Shaped Cooling Holes With Various Inlet Geometries

# publications[].label
Heat Transfer in Rotating, Trailing Edge, Converging Channels With Full- and Partial-Height Strip-Fins

# publications[].label
Thermal Performance of Double-Sided, Partial Height Strip Fin Arrays in a High Aspect Ratio, Rectangular Channel

# publications[].label
Effect of Density Ratio on Film-Cooling Effectiveness Distribution and its Uniformity for Several Hole Geometries on a Flat Plate

# publications[].label
Heat Transfer in Rotating, Trailing Edge, Converging Channels With Full and Partial Height Strip-Fins

# publications[].label
IMPINGEMENT HEAT TRANSFER ENHANCEMENT ON A CYLINDRICAL, LEADING EDGE MODEL WITH VARYING JET TEMPERATURES

# publications[].label
Effect of Density Ratio on Flat Plate Film Cooling With Shaped Holes Using PSP

# publications[].label
Impingement Heat Transfer Enhancement on a Cylindrical, Leading Edge Model With Varying Jet Temperatures

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

# publications[].label
Thermal Performance of Double-Sided, Partial Height Strip Fin Arrays in a High Aspect Ratio, Rectangular Channel

# publications[].label
Comparisons of Overall Performance Among Double-Jet Film Cooling Holes, Cylinder Holes, and Fan-Shaped Holes

# publications[].label
EXPERIMENTAL INVESTIGATION OF HEAT TRANSFER IN A LEADING EDGE, TWO-PASS SERPENTINE PASSAGE AT HIGH ROTATION NUMBERS

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

# publications[].label
Pressure-fed mechanism to compensate for motions and dynamic characteristics of compliant nanopositioning stages

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

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

# publications[].label
Assessment of Binary Pressure-Sensitive Paint for Temperature and Heat Transfer Coefficient Measurement of Leading-Edge Film Cooling

# publications[].label
Heat Transfer and Pressure Loss Correlations for Leading Edge, Jet Impingement Using Racetrack-Shaped Jets With Filleted Edges

# publications[].label
Effect of Strip-Fin Height on Jet Impingement Heat Transfer in a Rectangular Channel With Two Jet-to-Target Surface Spacings

# publications[].label
W-Shaped Rib Pitch Effect on Jet Impingement Heat Transfer in Rectangular Channel

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

# publications[].label
Optimized Film Cooling Flow on a Contoured Endwall Within a Transonic Annular Cascade

# publications[].label
Thermal Characterization of a Turbulent Free Jet with Planar Laser Induced Fluorescence (PLIF)

# publications[].label
Heat Transfer and Pressure Loss in a Two-Pass, Rectangular Channel Featuring a Reduced Cross-Sectional Area After the 180-Degree Tip Turn With Different Turning Vane Configurations

# publications[].label
Heat transfer in two-pass rotating rectangular channels (AR=1:2 and AR=1:4) with smooth walls

# 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
COMBINED EFFECTS OF JET PLATE THICKNESS AND FILLET RADIUS ON LEADING EDGE JET IMPINGEMENT WITH ROUND AND RACETRACK SHAPED JETS

# publications[].label
Heat Transfer and Friction in a Rectangular Channel With Varying Numbers of Walls Roughened With 90-Deg Transverse or 45-Deg V-Shaped Ribs

# publications[].label
Full Coverage Film Cooling Performance for Combustor Cooling Manufactured Using DMLS

# publications[].label
EFFECT OF FREESTREAM TURBULENCE INTENSITY ON FILM COOLING JET STRUCTURE AND SURFACE EFFECTIVENESS USING PIV AND PSP

# publications[].label
TURBULENT CONVECTION FROM DETERMINISTIC ROUGHNESS DISTRIBUTIONS WITH VARYING THERMAL CONDUCTIVITIES

# 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 in Two-Pass Rotating Rectangular Channels (AR=2:1) With Discrete V-Shaped and Discrete Angled Rib Turbulators

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

# 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
Combined Effects of Freestream Pressure Gradient and Density Ratio on the Film Cooling Effectiveness of Round and Shaped Holes on a Flat Plate

# publications[].label
Heat Transfer in a Rotating, Blade-Shaped, Two-Pass Cooling Channel With Various 45 Deg Rib Turbulators and a Tip Turning Vane

# publications[].label
Effects of Streamwise Distance and Density Ratio on Film-Cooling Effectiveness for Double-Jet Film-Cooling on a Flat Plate

# publications[].label
IMPINGEMENT HEAT TRANSFER ON A CYLINDRICAL, CONCAVE SURFACE WITH VARYING JET GEOMETRIES

# publications[].label
Jet Impingement Heat Transfer in a Rectangular Channel With Smooth and Pinned Target Walls

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

# publications[].label
LEADING EDGE IMPINGEMENT WITH RACETRACK SHAPED JETS AND VARYING INLET SUPPLY CONDITIONS

# publications[].label
Turbulent Convection From Deterministic Roughness Distributions With Varying Thermal Conductivities

# publications[].label
Thermal Characterization of a Turbulent Free Jet With Planar Laser Induced Fluorescence (PLIF)

# publications[].label
EFFECT OF IMPINGEMENT SUPPLY CONDITION ON LEADING EDGE HEAT TRANSFER WITH ROUNDED IMPINGING JETS

# publications[].label
Heat Transfer and Pressure Loss Correlations for Leading Edge, Jet Impingement Using Racetrack-Shaped Jets With Filleted Edges

# publications[].label
EFFECTS OF STREAMWISE DISTANCE AND DENSITY RATIO ON FILM-COOLING EFFECTIVENESS FOR DOUBLE-JET FILM-COOLING ON A FLAT PLATE

# publications[].label
Analysis of upstream, double-row, cylindrical holes on primary and secondary effects of endwall flow and film cooling

# publications[].label
Heat Transfer and Flow Field Characteristics of Variable Aspect Ratio, Serpentine Passages

# publications[].label
Experimental Evaluation of a Wavy Trailing Edge Cooling Design as an Alternative to Pressure Side Cutback Cooling

# publications[].label
Thermal Development of an Impinging Jet Using Planar Laser Induced Fluorescence (PLIF)

# publications[].label
Heat Transfer in a Rotating Blade-Shaped Two-Pass Channel with a Turning Vane

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

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

# publications[].label
An experimental investigation on streamwise distance and density ratio effects on double-jet film-cooling

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

# publications[].label
EXPERIMENTAL INVESTIGATION OF LEADING EDGE IMPINGEMENT UNDER HIGH ROTATION NUMBERS WITH RACETRACK SHAPED JETS

# publications[].label
Effect of Turbulator Width and Spacing on the Thermal Performance of Angled Ribs in a Rectangular Channel (AR=3:1)

# publications[].label
Effect of the number of ribbed walls on the thermal performance in rectangular channels with 45-deg parallel or criss-cross ribs

# publications[].label
EFFECT OF DENSITY RATIO ON FLAT PLATE FILM COOLING WITH SHAPED HOLES USING PSP

# publications[].label
Cavity Ring-Down Absorption of O2 in Air as a Temperature Sensor for an Open and a Cryogenic Optical Cavity.

# publications[].label
Effect of Inlet Geometry on Film-Cooling Effectiveness from Shaped Holes

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

# publications[].label
Development of an experimental technique for high temperature impingement studies

# publications[].label
Optimized Film Cooling Flow on a Contoured Endwall Within a Transonic Annular Cascade

# publications[].label
Combined Effects of Freestream Pressure Gradient and Density Ratio on the Film Cooling Effectiveness of Round and Shaped Holes on a Flat Plate

# publications[].label
Coupling of Volumetric Flowfield and Surface Effectiveness Measurements for Flat-Plate Film Cooling With Cylindrical Holes Using Tomographic Particle Image Velocimetry and Pressure-Sensitive Paint

# 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
Heat Transfer in a Rotating, Blade-Shaped, Two-Pass Cooling Channel With a Variable Aspect Ratio

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

# publications[].label
Upstream and Passage Endwall Film Cooling of a Transonic Turbine Vane

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

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

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

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

# publications[].label
Turning Region Heat Transfer in Five, Stationary and Rotating, Multi-Pass Channels With Various Aspect Ratios

# 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
EFFECT OF INLET GEOMETRY ON FLAT PLATE, FILM COOLING EFFECTIVENESS FROM SHAPED HOLES

# publications[].label
Effect of Density Ratio on Film-Cooling Effectiveness Distribution and Its Uniformity for Several Hole Geometries on a Flat Plate

# publications[].label
Influence of Coolant Density on Turbine Blade Film Cooling at Transonic Cascade Flow Conditions Using the Pressure Sensitive Paint Technique

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

# publications[].label
COMPUTATIONAL INVESTIGATION OF JET IMPINGEMENT ON TURBINE BLADE LEADING EDGE COOLING WITH ENGINE-LIKE TEMPERATURES

# publications[].label
Leading Edge Jet Impingement Under High Rotation Numbers

# publications[].label
Heat Transfer in a Rotating, Blade-Shaped, Two-Pass Cooling Channel With Various 45-Deg Rib Orientations

# publications[].label
PIV Investigation of the Effect of Freestream Turbulence Intensity on Film Cooling From Fanshaped Holes

# publications[].label
IDENTIFICATION AND QUANTIFICATION OF RESIDUAL STRAINS DURING CURING OF CARBON FIBER EPOXY LAMINATES

# publications[].label
Effect of the Coolant Ejection in Rectangular and Trapezoidal Trailing-Edge Cooling Passages

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

# publications[].label
Heat Transfer Enhancement in a Rectangular (AR=3:1) Channel With V-Shaped Dimples

# publications[].label
The effect of periodic unsteady flow on aerodynamics and heat transfer on a curved surface

# publications[].label
Ply INVESTIGATION OF THE EFFECT OF FREESTREAM TURBULENCE INTENSITY ON FILM COOLING FROM FANSHAPED HOLES

# publications[].label
Heat Transfer Coefficients and Film Cooling Effectiveness on the Endwall of a Transonic Turbine Vane Measured With the Reference Luminophore of Binary Pressure-Sensitive Paint

# publications[].label
Film-Cooling Performance Comparison of Blade Tips With a Trailing Edge, Pressure Side Cutback, or a Suction Side Squealer in a Transonic Linear Cascade

# 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 ENHANCEMENT FOR TURBINE BLADE INTERNAL COOLING

# publications[].label
Evaluation of Additively Manufactured Heat Exchanger Tubes Using Experimental and Conjugate Heat Transfer Analysis

# publications[].label
Influence of Hole Inlet Geometry on the Film Cooling Effectiveness from Shaped Film Cooling Holes

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

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

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