Journal of Turbomachinery-Transactions of the Asme

Article	Citations
Evaluation of Cooling Requirements for Rotating Detonation Combustors	30
Quantitative Evaluation and Optimization of Feeding-Back Previous Cycles Information for Computational Fluid Dynamics Periodic Convergence	27
On the Divergence Mechanisms Analysis of a Vibrating Blade Subjected to Repetitive Rubs With an Abradable Coating	23
Rotating Instabilities in Shrouded Low Pressure Turbine at Design and Off-Design Conditions	22
On the Use of Pressure-Sensitive Paint to Determine the Rim Sealing Effectiveness	21
Effect of the Key Geometry and Flow Parameters on Discharge Coefficient of Laidback Fan-Shaped Hole Under Coolant Crossflow Condition	20
Three-Dimensional Unsteady Aerodynamic Optimization of a Transonic Compressor Stage Using an Implicit Discrete Adjoint Harmonic Balance Method	19
Effects of Radially Variable Sweep Vanes on Rotor–Stator Interaction Noise	19
Analysis of the Bifurcating Duct of an Inlet Particle Separator in Transonic Flow Conditions	19
Coupled Time and Passage Spectral Method for an Efficient Resolution of Turbomachinery Far Upstream Wakes	18
Experimental and Numerical Study of an Open Impeller Centrifugal Compressor Stage Utilizing Three-Dimensional (3D) Diffuser End Wall Contouring for Operating Range Extension	18
Turbine Vane Passage Cooling Experiments With a Close-Coupled Combustor-Turbine Interface Geometry—Part I: Describing the Flow	17
An Improved Particle Impact Model by Accounting for Rate of Strain and Stochastic Rebound	17
Corner Separation Control Using Sweeping Jet Actuator in a Compressor Cascade	16
Modeling and Simulation of Sand Particle Trajectories and Erosion in a Transonic Fan Stage	15
Measurements of Turbulence in Compressible Low-Density Flows at the Inlet of a Transonic Linear Cascade With and Without Unsteady Wakes	15
Effect of Leading Edge Erosion on the Tip Leakage Flow in a Compressor Cascade	15
Exploring Topology Optimization for High Pressure Turbine Blade Tips	15
EXPERIMENTAL STUDY ON THE HIGH RELATIVE CASING MOTION EFFECT ON TURBINE BLADE TIP AERODYNAMIC CHARACTERISTICS	15
An Analysis of the Secondary Flow Around a Tandem Blade Under the Presence of a Tip Gap in a High-Speed Linear Compressor Cascade	15
A Framework for Estimating Effects of Combustor Turbulence on Turbine Profile Loss Generation	14
Numerical Study on the Effect of Back Cavity on the Aerodynamic Behavior of a Non-Axisymmetric Casing Treatment for Transonic Axial Compressors	13
The Effects of Swirling Flows in Entropy Wave Convection Through High-Pressure Turbine Stage	13
Fan Non-Synchronous Forced Vibration Under Crosswind	13
Nonlinear Flutter Analysis of Labyrinth Seals	13

A Method for Preliminary Design of Variable Geometry Vaned Diffuser for Centrifugal Compressor	13
Roughness Investigations on In-Service High-Pressure Compressor Blades—Part II: Roughness Parameterization and Computational Fluid Dynamics-Based Modeling of Its Impact on Turbulent Flows	12
Introduction of Axisymmetric Grooves as a Tip Seal Treatment for Small-Core Turbines	12
A New Multi-Stage Turbine Stator Design for Improved Performance Retention	12
Foam-Metal Casing Treatment on an Axial Flow Compressor: Stability Improvement and Noise Reduction	12
Film Cooling on Turbine Vane Endwalls With Different Inlet Cooling Configurations: Experimental and Computational Results	12
Prediction of Steady and Unsteady Flow Quantities Using Multiscale Graph Neural Networks	12
Reviewer’s Recognition	12
Unsteady Pre-Stall Behavior in a Centrifugal Compressor With Vaned Diffuser	12
Unique High-Resolution Temperature Mapping of Stage 1 Turbine Vane in a Long-Term Engine Test	12
Spectral Heat Transfer Coefficient for Thermal Design Analysis—Part 1: Augmenting the Cooling Law for Non-Isothermal Wall	11
Generalized Predictions of Particle-Vane Retention Probability in Gas Turbine Engines	11
The Cooling Effect of Combustor Exit Louver Scheme on a Transonic Nozzle Guide Vane Endwall	11
Prediction of the Acoustic Reflection in a Realistic Aeroengine Intake With Three Numerical Methods to Analyze Fan Flutter	11
Impacts of Tandem Configurations on the Aerodynamic Performance of an Axial Supersonic Through-Flow Fan Cascade	11
One-Dimensional Modeling for Pulsed Flow Twin-Entry Turbine	11
Pragmatic Prediction Model of Droplet Trajectory in a Turbine Cascade	11
A Study of Loss Model Parameter Sensitivity in Compressor Unsteady Flow Simulations	11
Inlet Flow Distortion in an Advanced Civil Transport Boundary Layer Ingesting Engine Installation	11
Tail-Integrated Boundary Layer Ingesting Propulsion Systems for Turbo-Electric Aircraft	11
Fundamentals of Scaling of Overall Cooling Effectiveness With Temperature Ratio	11
Correlated Pressure–Velocity Instability in a Transonic High-Pressure Turbine Blade	10
Particle Image Velocimetry in a High-Speed Short-Duration Turbine Rig	10
Acoustic Modes in an Open Box Cavity With Variable Depth Using Two Distinct Wind Tunnels	10
Numerical Modeling and Design Challenges of Boundary Layer Ingesting Fans	10
Aerodynamics and Heat Transfer Inside a Gas Turbine Mid-Passage Gap	10
Effects of Surface Waviness on Fan Blade Boundary Layer Transition and Profile Loss—Part I: Methodology and Computational Results	10
Loss Analysis of Cavity Leakage Flow in a Compressor Cascade	10
Effect of Tip Clearance on Rotating Stall in a Mixed-Flow Pump	9
Experimental Investigation of Additional Loss Associated With Incoming Wakes in Low-Pressure Turbine Cascades	9
Flow and Heat Transfer in a Rotating Disc Cavity With Axial Throughflow at High-Speed Conditions	9
Stall Behavior in an Ultrahigh-Pressure-Ratio Centrifugal Compressor: Backward-Traveling Rotating Stall	9
Experimental Determination of Heat Transfer Coefficient on Impingement Cooled Gear Flanks: Validation of the Evaluation Method	9
Experimental Study on Controlling Flow Separation of Compressor Cascades With Self-Excited Sweeping Jet Actuator	9
Aerothermal Performance Robustness and Reliability Analysis of Turbine Blade Squealer Tip With Film Cooling	9
The Influence of Turbulence and Reynolds Number on Endwall Heat Transfer in a Vane Cascade	9
On the Over-Prediction of Centrifugal Compressor Pressure Ratio in the High Impeller Tip Mach Number Regime	9
Numerical Assessment of an Aerodynamic Probe to Enable Short Focal Length Laser Diagnostics in High Temperature Supersonic Flows Based on Flow Disturbance	8
Unsteady Flow Structure of Corner Separation in a Highly Loaded Compressor Cascade	8
Unpacking Intermineral Synergies and Reactions During Dust Deposition in an Impingement Coolant Jet	8
Effects of Downstream Vortex Generators on Film Cooling a Flat Plate Fed by Crossflow	8
Impact of High-Pressure-Turbine Purge Flow on the Evolution of Turbulence in a Turbine Vane Frame	8
Windage Torque Reduction in Low-Pressure Turbine Cavities Part II: Experimental and Numerical Results	8
Numerical Investigation on the Influence of Wet Compression Aerodynamic Performance of Multi-Stage Transonic Compressor	8
ENTRY REGION HEAT TRANSFER AUGMENTATION WITH PINS, FINS, AND TURBULATORS IN CIRCULAR CHANNELS	8
Analysis of Complex Total Pressure Distortion Screens Using One-Dimensional Loss Data	8
Multistage turbomachinery optimization for high temperature heat pumps with the reverse Rankine cycle	8
Blade Envelopes Part I: Concept and Methodology	8
Numerical Study of Crossflow Effects on Discharge Coefficient of the Converging Slot Hole	8
Flow Check and Adiabatic Effectiveness Measurements on Traditionally Versus Additively Manufactured Film-Cooling Holes	8

Unsteady Aerodynamic Forcing Due to Distortion in a Boundary Layer Ingesting Fan	8
Application of Scale Adaptive Simulation Model to Studying Cooling Characteristics of a High Pressure Turbine Blade Cutback Trailing Edge With Different Cooling Configurations	8
Dirt Ingestion Impacts on Cooling Within a Double-Walled Combustor Liner	8
Film-Cooling Performance Comparison of Blade Tips With a Trailing Edge, Pressure Side Cutback, or a Suction Side Squealer in a Transonic Linear Cascade	8
Sensitivity Analysis for Flow Stability of Axial Compressor Based on Meridional Flow	7
Response of Separated Boundary Layers to Steady and Pulsated Flow Injection	7
Strategies for High-Accuracy Measurements of Stage Efficiency for a Cooled Turbine	7
Insights Into Turbocharger Centrifugal Compressor Stability Using High-Fidelity Computational Fluid Dynamics and a Novel Impeller Diffusion Factor	7
High-Fidelity Investigation of Vortex Shedding From a Highly Loaded Turbine Blade	7
An Improved Passage-Flow Turning Model for Forward-Curved Blades of Squirrel-Cage Fan	7
Application of Advanced RANS Turbulence Models for the Prediction of Turbomachinery Flows	7
Investigation of the Map Width Improvement in a Radially Reduced Diffuser Design Concept for a Centrifugal Compressor	7
Film Superposition Characteristics With Laidback Fan-Shaped Holes Under the Influence of Internal Crossflow	7
Investigation of Tip Leakage Vortex Breakdown in a High-Speed Multistage Axial Compressor	7
RANS Capabilities for Transonic Axial Compressor: A Perspective From GPPS Computational Fluid Dynamics Workshop	7
Numerical Study on Unsteady Flow of a Supersonic Partial Admission Impulse Turbine	7
Advanced Design of a Transition Duct for Supersonic Inlet Turbines in Rotating Detonation Engines	7
Suppression of Nonsynchronous Vibration Through Intentional Aerodynamic and Structural Mistuning	7
The Application of Fluidic Sealing in Shrouded Gas Turbine Blades	7
Unsteadiness in the Secondary Flows of a High-Speed Low-Pressure Turbine Cascade With Unsteady Wakes and Purge Flow	7
Revisiting Dimensionless Parameters Quantifying Film Cooling	7
Effect of Upstream Leakage Flow on Film Cooling Characteristic of a Turbine Convex Endwall	7
A REVIEW OF SECONDARY COMBUSTION ON TURBINE BLADE COOLING	7
Direct and Inverse Model for Single-Hole Film Cooling With Machine Learning	7
GPU-Accelerated Full-Wheel Large-Eddy Simulations of a Transonic Fan Stage	6
A New Loss Generation Body Force Model for Fan/Compressor Blade Rows: Application to Uniform and Non-Uniform Inflow in Rotor 67	6
A New Nonlinear Time-Domain Flutter Analysis Approach for Distorted Flows	6
Experimental Research Into Aeroelastic Phenomena in Turbine Rotor Blades Inside ARIAS EU Project	6
Heat Transfer in an Injector-Scaled Additively Manufactured Fuel Passage	6
Comparative Study of Tip Injection in a Transonic and Subsonic Compressor	6
Magnetic Resonance Velocimetry of a Turbine Blade With Engine-Representative Internal and Film Cooling Structures	6
Effects of Ribbed Surfaces on Profile Losses of Low-Pressure Turbine Blades	6
Characterizing Flow Instabilities During Transient Events in the Turbine Rim Seal Cavity	6
The Effect of Inlet Conditions on Turbine Endwall Loss	6
Noise Source Identification for the Unsteady Low-Pressure Turbine Flow Fields	6
Influences of Particulate Deposition on Vane Trailing-Edge Film Cooling: Adiabatic and Overall Cooling Effectiveness	6
Morphing of Reversible Axial Fan Blade: A FSI-FEM Study	6
Highly Time Resolved, Combined Temperature, and Heat Flux Measurement Technique Based on ALTP Sensors	6
Impact of Swirling Entropy Waves on a High Pressure Turbine	6
A Physics-Informed Neural Network for Solving the Inverse Heat Transfer Problem in Gas Turbine Rotating Cavities	6
Experimental Study of the Endwall Heat Transfer of a Transonic Nozzle Guide Vane With Upstream Jet Purge Cooling Part 2—Effect of Combustor-Nozzle Guide Vane Misalignment	6
Effects of Inlet Guide Vanes on the Performance and Stability of an Aeronautical Centrifugal Compressor	6
Direct Numerical Simulation of Transitional and Turbulent Flows Over Multi-Scale Surface Roughness—Part II: The Effect of Roughness on the Performance of a High-Pressure Turbine Blade	6
Erratum: “Formation of High-Temperature Minerals From an Evaporite-Rich Dust in Gas Turbine Engine Ingestion Tests” [ASME J. Turbomach. 143(6), p. 061003; DOI: 10.1115/1.4050146]	6
Optimization of a Tip Appendage for the Control of Tip Leakage Vortices in Axial Flow Fans	6
Impacts of Material and Machine on the Variation of Additively Manufactured Cooling Channels	6
The Influence of Deterministic Surface Roughness and Freestream Turbulence on Transitional Boundary Layers: Heat Transfer Distributions and a New Transition Onset Correlation	6
UHBR Open-Test Case Fan ECL5/CATANA: Non-Linear Analysis of Non-Synchronous Blade Vibration at Part-Speed Conditions	6
A Free Streamline Model for Fully Separated Turbomachine Flows	6
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	6
Effect of Solidity and Aspect Ratio on the Aerodynamic Performance of Axial-Flow Fans With 0.2 Hub-to-Tip Ratio	6
Blade Vibration Analysis for Radial Turbine Featuring a Multi-Channel Casing Design	6
Experimental and Numerical Investigation of High Load Turbine Blade Tip Cavity Structures	6
Particle Bounce Stick Behavior in the Rotating Frame of Reference	6
Optimal Riblets Applied to Gas Turbine Compressor Blades Studied via Direct Numerical Simulation (GT2024–122305)	6
Cooling Performance of Additively Manufactured Pin Fins in Stacked Microchannels for the Inside-Out Ceramic Turbine Shroud-Cooling Ring	6
A Detailed Loss Analysis Methodology for Centrifugal Compressors	6
Numerical Investigation of the Fan Flutter Mechanism Related to Acoustic Propagation Characteristics	6
Dissipation in Skewed Boundary Layers	6
An Aerodynamic Investigation of a High-Pressure Turbine Using Rotor Casing Static Pressure Measurements at Engine Representative Conditions With Different Tip Designs, Tip Gaps, and Inlet Temperature	6
Improvements in the Prediction of Steady and Unsteady Transition and Mixing in Low-Pressure Turbines by Means of Machine-Learnt Closures	5
Multidisciplinary Optimization of a Mixed-Flow Impeller With 140 Parameters and Its Shapley Additive Explanations	5
High-Fidelity Computational Assessment of Aero-Thermal Performance and the Reynolds’ Analogy for Additively Manufactured Anisotropic Surface Roughness	5
Heat Transfer in a Rotating, Two-Pass, Variable Aspect Ratio Cooling Channel With Profiled V-Shaped Ribs	5
Inverse Design of Compressor/fan Blade Profiles Based on Conditional Invertible Neural Networks	5
DATA-ASSIMILATION OF TRANSITIONAL AND SEPARATED TURBOMACHINERY FLOWS WITH PHYSICS-INFORMED NEURAL NETWORKS	5
Low Reynolds Number Effects on the Endwall Flow Field in a High-Lift Turbine Passage	5
The Effects of Incoming Vortex and Wake on the Aerodynamics of an Intermediate Turbine Duct	5
Plume Model for Buoyancy-Induced Flow and Heat Transfer in Closed Rotating Cavities	5
The Influence of Combustor Hot Streaks on the Aerodynamic Performance of a Turbine Center Frame	5
Impact of Low Freestream Turbulence and Surface Roughness on the Flat-Plate Boundary Layer Transition Under a High-Lift Airfoil Pressure Gradient	5
Innovative Cavity Modeling for Centrifugal Compressors Aeromechanical Analysis	5
Influence of Boundary Layer Skew on the Tip Leakage Vortex of an Axial Compressor Stator	5
Heat Transfer and Flow Field Characteristics of Variable Aspect Ratio, Serpentine Passages	5
Impact of the Purge Flow Density Ratio on the Rim Sealing Effectiveness in Hot Gas Ingestion Measurements	5
Effects of Water-to-Air Mass Ratio on Long-Term Washing Efficiency and Erosion Risk in an Axial Compressor Under Online Washing Conditions	5
Effects of Rotation on the Flow Structure in a Compressor Cascade	5
A High-Speed Disk Rotor Rig Design for Tip Aerothermal Research	5
Development of Compact and Hermetic Organic Rankine Cycle Turbine Generator With Upgraded Cooling Capability	5
Manufacturing a Ceramic Turbine Rotor for a Compact Jet Engine	5

The Influence of Boundary Layer State and Trailing Edge Wedge Angle on the Aerodynamic Performance of Transonic Turbine Blades	5
Adaptation of von Karman Institute for Fluid Dynamics’ Isentropic Compression Tube Facility for High-Speed Low-Pressure Turbines Testing	5
The Influence of Purge Flow Parameters on Heat Transfer and Film Cooling in Turbine Center Frames	5
Robustness Analysis on Aerothermal Performance of the Winglet Squealer Tip—Part 1: Aerodynamic Performance	5
Investigating Gas Turbine Internal Cooling Using Supercritical CO2 at Higher Reynolds Numbers for Direct Fired Cycle Applications	5
On the Secondary Flow System of an Aggressive Inter Compressor Duct	5
Large Eddy Simulation of Laminar and Turbulent Shock/Boundary Layer Interactions in a Transonic Passage	5
Generation Mechanism of Broadband Whoosh Noise in an Automotive Turbocharger Centrifugal Compressor	5
Modeling of Combustor Non-Uniformities Evolution Through a High-Pressure Turbine Stage	5
Turbulence Measurements at the Inlet of an Automotive Turbocharger Compressor Using Stereoscopic Particle Image Velocimetry	5
Wake–Separation Bubble Interaction Over an Experimentally Simulated Axial Compressor Blade Under Low Reynolds Number Flow	5
A Shock Loss Reduction Method Using a Concave Suction Side Profile for a Zero Inlet Swirl Turbine Rotor	5
Loss Analysis in Radial Inflow Turbines for Supercritical CO2 Mixtures	5
Equation-Oriented Meanline Method for Axial Turbine Performance Prediction Under Choking Conditions	5
Unsteady Analysis of Heat Transfer Coefficient Distribution in a Static Ribbed Channel for An Established Flow	5
Collaborative Robust Design Optimization of Blade Geometry and Manufacturing Tolerance for a Transonic Centrifugal Impeller	5
Investigating the Influence of Mainstream Turbulence and Large Vortices on Gas Turbine Trenched Film Cooling Flows Using Planar Temperature-Velocity Imaging	5
Efficient Aerodynamic Uncertainty Quantification for a Three-Dimensional Transonic Fan Rotor	5
Investigation on the Contribution of Large-Scale Fluctuation and Small-Scale Disturbance of Coolant to Heat Transfer Enhancement in a Rectangular Channel With Pin Fins	5
Experimental Investigation of Mode-Frequency Scattering at Fan Stages	5
Improved Prediction of Losses With Large Eddy Simulation in a Low-Pressure Turbine	5
Scale-Resolving Simulations of Turbulent Flow Retaining the Exact Blade Count With the Time-Inclined Method	5
Mitigation of Boundary Layer Ingestion Circumferential Distortion Using Nonaxisymmetric Fan Exit Guide Vanes	4
Quasi-Dynamic Approximation of Unsteady Pressure Distribution for Transonic Airfoils in Flutter	4
A Resistive Model to Characterize Overall Effectiveness Influenced by Multiple Coolant Temperatures	4
Analysis of Averaging Methods for Nonuniform Total Pressure Fields	4
Unsteady Loss Mechanisms in Low-Pressure Turbines With Diverging End-Walls Studied Via High-Fidelity Simulation	4
Computational and Experimental Study of Film-Cooling Effectiveness With and Without Downstream Vortex Generators	4
Validation of Broadband Noise Prediction Methodology Based on Linearized Navier–Stokes Analyses	4
Detailed Experimental Study of the Flow in a Turbine Rear Structure at Engine-Realistic Flow Conditions	4
A Digital Engineering Analysis of an Additively-Manufactured Turbine Vane	4
Infrared Temperature Measurements of the Blade Tip for a Turbine Operating at Corrected Engine Conditions	4
Effective Clearance and Differential Gapping Impact on Seal Flutter Modeling and Validation	4
Validation of Filtered Rayleigh Scattering Optical Rake Measurement Techniques in Turbomachinery Applications and Boundary Layers	4
Effects on Film Cooling Performance in the Showerhead From Geometric Parameterization of Shaped Hole Designs	4
Turbine Vane Passage Cooling Experiments With a Close-Coupled Combustor–Turbine Interface Geometry Part II: Describing the Coolant Coverage	4
A New Axial Compressor Test Facility for the Investigation of Aerodynamic Damping Featuring an Electromagnetic Excitation System	4
Pressure Characteristic Rollover of a Transonic Centrifugal Impeller	4
Annular Dump Diffuser and Deswirl System for Back-Pressure Control in Engine-Scale Transonic Annular Cascade	4
Considerations for Compressible Film Cooling: A Computational Study of the Effects of Transonic Flows and Varying Mainstream Mach Number	4
An Active Turbulence Grid for Turbomachinery Flow Experiments	4
The Effects of Reynolds Number on the Stall and Pre-Stall Behavior of Compact Axial Compressors	4
Effect of Coolant Crossflow on Film Cooling Effectiveness of Diffusion Slot Hole With and Without Ribs	4
Aero-Structural Coupling Strategy for a Morphing Blade Cascade Study	4
Influence of Casing Groove on Rotating Instabilities in a Low-Speed Axial Compressor	4
Experimental Investigation of Flame-Film Cooling Interactions With an Academic Test Rig and Optical Laser Diagnostics	4
The Effect of Reaction on Compressor Performance	4
Impact of Blowing and Density Ratio on the Film Cooling and Heat Transfer in an Aggressive Turbine Center Frame	4
The Impact of Manufacturing Variations on the Aerothermal Performance of High-Pressure Turbine Blade Shrouds	4
Investigation on Heat Transfer Distribution of Rotating Two-Pass Smooth and Ribbed Channels Under Aero-Engine Simulated Conditions	4
Aero-Thermal Aspects of Film Cooled Nozzle Guide Vane Endwall—Part 2: Thermal Measurements	4
Experimental Study of Impact of In-Service Deterioration on Thermal Performance of High-Pressure Nozzle Guide Vanes	4
The Effect of Upstream Unsteadiness on the Unstarting of a Supersonic Inlet Turbine	4
“I-Spots” and Emmons’ Spot Production Rate	4
Convergence Acceleration of Favre-Averaged Non-Linear Harmonic Method	4
Boundary Layer Analysis of a Transonic High-Pressure Turbine Vane Using Ultra-Fast-Response Temperature-Sensitive Paint	4
Numerical Investigation of the Effect of Trailing Edge Thickness of Simulated Ceramic Matrix Composite Blades on Loss Profiles	4
Data-Driven Radial Compressor Design Space Mapping	4
Large Eddy Simulation Analysis of Loss Anomaly of a Turbine Blade With Large Trailing Edge Radius	4
Numerical and Experimental Aerodynamic Investigation of an S-Shaped Intermediate Compressor Duct With Bleed	4
Scaling Heat Transfer and Pressure Losses of Novel Additively Manufactured Rib Designs	4
Unsteady Investigation of Intermediate Turbine Ducts Under the Influence of Purge Flows	4
High-Dimensional Uncertainty Quantification of High-Pressure Turbine Vane Based on Multifidelity Deep Neural Networks	4
The Effect of Wall Thermal Boundary Condition on Natural Convective Shutdown Cooling in a Gas Turbine	4
Turbine Nozzle Guide Vane Endwall Film Cooling and Vane Phantom Cooling Performances at Various Blocked Film Hole Configurations	4
The Unsteady Topology of Corner Separations	4
Interaction Mechanism of Transonic Squealer Tip Cooling With the Effect of High-Speed Relative Casing Motion	4
On Intake–Compressor Interactions Within an Integrated Propulsion System	4
Characterizing the Unsteady Flow Field in Low-Flow Turbine Operation	4
Experimental and Numerical Analysis of Loss Characteristics of Cooled Transonic Nozzle Guide Vanes	4
MULTIDISCIPLINARY DESIGN OPTIMIZATION OF A LOW-NOISE AND EFFICIENT NEXT-GENERATION AERO-ENGINE FAN	4
Vortex Unsteadiness in the Endwall Region of a High-Lift Low-Pressure Turbine Passage	3
Film Cooling Comparison of Full-Scale Turbine Vanes Using the Pressure Sensitive Paint Technique	3
Compressor Tip Leakage Mechanisms	3
Effect of Tip Vortex Reduction on Air-Cooled Condenser Axial Flow Fan Performance: An Experimental Investigation	3
Experimental Investigations of Centrifugal Compressor Surge Noise	3
Effect of Blade Damage on Low Pressure Ratio Fan Windmill Aerodynamics	3
Progresses in Particle-Laden Flows Simulations in Multistage Turbomachinery With OpenFOAM	3
Use of Multiple Tracer Gases to Quantify Vane Trailing Edge Flow Into Turbine Rim Seals	3
Numerical Investigations on the Rotating Stall in an Axial Compressor and Its Control by Flow Injection at Casing	3
Direct Numerical Simulation of a High-Pressure Turbine Stage: Unsteady Boundary Layer Transition and the Resulting Flow Structures	3
Experimental Investigations on the Effects of Surface Roughness for Compressor Cascades With Different Roughness Magnitude and Location	3
Control of Shroud Leakage Loss and Windage Torque in a Low-Pressure Turbine Stage	3
Multi-Objective Aerodynamic and Aeroelastic Coupled Design Optimization Using a Full Viscosity Discrete Adjoint Harmonic Balance Method	3
Study on Effects of Spanwise-Expansion Parameters on Film Cooling Effectiveness of Diffusion Shaped Hole Configurations	3
Experimental and Computational Investigation of Integrated Internal and Film Cooling Designs Incorporating a Thermal Barrier Coating	3
A Data-Driven Tip Flow Loss Prediction Method for a Transonic Fan Under Boundary Layer Ingesting Inflow Distortion	3
Numerical and Experimental Investigation of Boundary Layer of a High-Lift Low-Pressure Turbine Cascade Under Periodic Wakes With Different Flow Coefficients	3
IMPACT OF HIGH FREESTREAM TURBULENCE ON LPT ENDWALL FLOW: PART I – LOSS DEVELOPMENT AND TIME-AVERAGED FLOW FIELD	3
Reduced-Order Models for Effusion Modeling in Gas Turbine Combustors	3
Development of Heat Exchanger Modeling Capability for a Finite-Volume Aeroelasticity Solver	3
Roughness-Resolved Large-Eddy Simulation of Additive Manufacturing-Like Channel Flows	3
Evaluating the Influence of Rotor-Casing Eccentricity on Turbine Efficiency Including Time-Resolved Flow Field Measurements	3
Metamodel-Interpreted Data Mining for Stability and Efficiency Enhancement of Multistage Axial-Flow Compressors	3
Unsteady Flow Structure of Rotating Instability in a 1.5-Stage Axial Compressor	3