Journal of Turbomachinery-Transactions of the Asme

Article	Citations
Effect of the Key Geometry and Flow Parameters on Discharge Coefficient of Laidback Fan-Shaped Hole Under Coolant Crossflow Condition	57
Effects of Radially Variable Sweep Vanes on Rotor–Stator Interaction Noise	39
Rotating Instabilities in Shrouded Low Pressure Turbine at Design and Off-Design Conditions	36
Turbine Vane Passage Cooling Experiments With a Close-Coupled Combustor-Turbine Interface Geometry—Part I: Describing the Flow	34
Three-Dimensional Unsteady Aerodynamic Optimization of a Transonic Compressor Stage Using an Implicit Discrete Adjoint Harmonic Balance Method	29
Experimental Study on the High Relative Casing Motion Effect on Turbine Blade Tip Aerodynamic Characteristics	27
An Exception Algorithm to Ease Convergence in Multistage Turbomachinery Throughflow Calculations	24
Performance Sensitivity of a Grooved Tip Seal to Manufacturing and Operational Geometry Deviations	22
An Improved Particle Impact Model by Accounting for Rate of Strain and Stochastic Rebound	21
Analysis of the Bifurcating Duct of an Inlet Particle Separator in Transonic Flow Conditions	21
Effect of Leading Edge Erosion on the Tip Leakage Flow in a Compressor Cascade	20
Evaluation of Cooling Requirements for Rotating Detonation Combustors	20
On the Use of Pressure-Sensitive Paint to Determine the Rim Sealing Effectiveness	20
Corner Separation Control Using Sweeping Jet Actuator in a Compressor Cascade	20
Reviewer’s Recognition	19
The Effects of Swirling Flows in Entropy Wave Convection Through High-Pressure Turbine Stage	18
Physics-Guided Graph Neural Networks: Numerical Investigation of High-Pressure Turbine Flow	18
Nonlinear Flutter Analysis of Labyrinth Seals	18
A Method for Preliminary Design of Variable Geometry Vaned Diffuser for Centrifugal Compressor	17
Film Cooling on Turbine Vane Endwalls With Different Inlet Cooling Configurations: Experimental and Computational Results	16
Unsteady Pre-Stall Behavior in a Centrifugal Compressor With Vaned Diffuser	16
Effects of Blade Solidity and Aspect Ratio on a 0.5 Hub-to-Tip Ratio Tube-Axial Fan	15
Aerodynamic Effect of Shallow Circumferential Grooves in the Shroud of a Centrifugal Compressor	15
Numerical Study on the Effect of Back Cavity on the Aerodynamic Behavior of a Non-Axisymmetric Casing Treatment for Transonic Axial Compressors	15
Development of a Novel Pressure-Based Approach for Blade Synchronous Vibration Detection Including Mistuning	15

Impact of Nozzle Guide Vane Trailing Edge Damage on High-Pressure Turbine Stage Performance	14
Introduction of Axisymmetric Grooves as a Tip Seal Treatment for Small-Core Turbines	14
Modeling and Simulation of Sand Particle Trajectories and Erosion in a Transonic Fan Stage	13
A Framework for Estimating Effects of Combustor Turbulence on Turbine Profile Loss Generation	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	13
Prediction of Steady and Unsteady Flow Quantities Using Multiscale Graph Neural Networks	13
NUMERICAL DESIGN OF EXPERIMENTS FOR REPEATING LOW-PRESSURE TURBINE STAGES PART I: COMPUTATIONAL OPPORTUNITIES AND METHODOLOGY	12
A New Multi-Stage Turbine Stator Design for Improved Performance Retention	12
A Multi-Scale Representation of Turbulence Generation in Compressor Flows	12
Fan Non-Synchronous Forced Vibration Under Crosswind	12
Unique High-Resolution Temperature Mapping of Stage 1 Turbine Vane in a Long-Term Engine Test	12
A Study of Loss Model Parameter Sensitivity in Compressor Unsteady Flow Simulations	12
Measurements of Turbulence in Compressible Low-Density Flows at the Inlet of a Transonic Linear Cascade With and Without Unsteady Wakes	12
Wind Tunnel Continuous-Scan Acoustic Analysis of Ducted Fan Tones Interacting With a Shielding Wall	12
Spectral Heat Transfer Coefficient for Thermal Design Analysis—Part 1: Augmenting the Cooling Law for Non-Isothermal Wall	11
Fundamentals of Scaling of Overall Cooling Effectiveness With Temperature Ratio	11
Systematic Numerical Investigation on the Surface Roughness Effects on the Friction and Heat Transfer of Additively Manufactured Components	11
On the Over-Prediction of Centrifugal Compressor Pressure Ratio in the High Impeller Tip Mach Number Regime	11
Pragmatic Prediction Model of Droplet Trajectory in a Turbine Cascade	11
Tail-Integrated Boundary Layer Ingesting Propulsion Systems for Turbo-Electric Aircraft	11
Analytical Study on the Influence of Stage-Wise Distribution of Parameters on the Performance of a Multistage Axial Compressor	11
Loss Analysis of Cavity Leakage Flow in a Compressor Cascade	11
Heat Transfer Measurements in a Turbine Centre Frame at Realistic Mach Number - Part 2: Influence of Combustor Hot Streaks	11
Effect of Axial Throughflow Swirl on Flow and Heat Transfer in a Compressor Disc Cavity	11
Acoustic Modes in an Open Box Cavity With Variable Depth Using Two Distinct Wind Tunnels	11
The Cooling Effect of Combustor Exit Louver Scheme on a Transonic Nozzle Guide Vane Endwall	11
Entry Region Heat Transfer Augmentation With Pins, Fins, and Turbulators in Circular Channels	10
Analysis of Complex Total Pressure Distortion Screens Using One-Dimensional Loss Data	10
Particle Image Velocimetry in a High-Speed Short-Duration Turbine Rig	10
Unpacking Intermineral Synergies and Reactions During Dust Deposition in an Impingement Coolant Jet	10
Correlated Pressure–Velocity Instability in a Transonic High-Pressure Turbine Blade	10
Modeling Deposition in Gas Turbines With Conjugate Mesh-Morphing and Temperature Sensitivity	10
Performance and Secondary Flow Structures Characterization in a Highly Loaded Low-Pressure Compressor Under Distorted Inflow Conditions	10
Experimental Investigation of Additional Loss Associated With Incoming Wakes in Low-Pressure Turbine Cascades	10
The Influence of Turbulence and Reynolds Number on Endwall Heat Transfer in a Vane Cascade	10
An Experimental Investigation of Sweeping Mist Jet Film Cooling With Droplet Analysis	10
Revisiting Dimensionless Parameters Quantifying Film Cooling	9
Insights Into Turbocharger Centrifugal Compressor Stability Using High-Fidelity Computational Fluid Dynamics and a Novel Impeller Diffusion Factor	9
Numerical Assessment of an Aerodynamic Probe to Enable Short Focal Length Laser Diagnostics in High Temperature Supersonic Flows Based on Flow Disturbance	9
Aerothermal Performance Robustness and Reliability Analysis of Turbine Blade Squealer Tip With Film Cooling	9
Heat Transfer Analysis in a Turbine Bottom Platform Cavity With Hot Gas Ingestion: An Investigation on the Applicability of the Superposition Approach	9
Windage Torque Reduction in Low-Pressure Turbine Cavities Part II: Experimental and Numerical Results	9
An Improved Passage-Flow Turning Model for Forward-Curved Blades of Squirrel-Cage Fan	9
Numerical Study on Unsteady Flow of a Supersonic Partial Admission Impulse Turbine	9
Dirt Ingestion Impacts on Cooling Within a Double-Walled Combustor Liner	9
RANS Capabilities for Transonic Axial Compressor: A Perspective From GPPS Computational Fluid Dynamics Workshop	9
High-Fidelity Investigation of Vortex Shedding From a Highly Loaded Turbine Blade	9
Experimental Study on Controlling Flow Separation of Compressor Cascades With Self-Excited Sweeping Jet Actuator	9
Multistage Turbomachinery Optimization for High-Temperature Heat Pumps With the Reverse Rankine Cycle	9
Unsteady Flow Structure of Corner Separation in a Highly Loaded Compressor Cascade	9

Effect of Purge–Mainstream Density Ratio on the Secondary Flow Field of a Turbine Blade Row	9
Boundary layer transition induced by surface roughness distributed over a low-pressure turbine blade	9
Investigation of Tip Leakage Vortex Breakdown in a High-Speed Multistage Axial Compressor	9
Numerical Study of Crossflow Effects on Discharge Coefficient of the Converging Slot Hole	9
Impact of High-Pressure-Turbine Purge Flow on the Evolution of Turbulence in a Turbine Vane Frame	9
Numerical Investigation on the Influence of Wet Compression Aerodynamic Performance of Multi-Stage Transonic Compressor	9
Effects of Downstream Vortex Generators on Film Cooling a Flat Plate Fed by Crossflow	9
Flow and Heat Transfer in a Rotating Disc Cavity With Axial Throughflow at High-Speed Conditions	9
Numerical Modeling and Design Challenges of Boundary Layer Ingesting Fans	9
Unsteady Aerodynamic Forcing Due to Distortion in a Boundary Layer Ingesting Fan	9
Comparative Investigation of HPT Blade Cooling Concepts in an Aerothermal Test Rig	9
Film-Cooling Performance Comparison of Blade Tips With a Trailing Edge, Pressure Side Cutback, or a Suction Side Squealer in a Transonic Linear Cascade	9
Effect of Upstream Leakage Flow on Film Cooling Characteristic of a Turbine Convex Endwall	9
Heat Transfer in an Injector-Scaled Additively Manufactured Fuel Passage	8
ANALYSIS OF AEROACOUSTIC PHENOMENA IN CENTRIFUGAL COMPRESSORS USING A LATTICE BOLTZMANN FLOW SIMULATION APPROACH	8
Sensitivity Analysis for Flow Stability of Axial Compressor Based on Meridional Flow	8
Dissipation in Skewed Boundary Layers	8
A Review of Secondary Combustion on the Turbine Blade Cooling	8
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]	8
Optimal Riblets Applied to Gas Turbine Compressor Blades Studied via Direct Numerical Simulation (GT2024–122305)	8
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	8
Strategies for High-Accuracy Measurements of Stage Efficiency for a Cooled Turbine	8
Unsteadiness in the Secondary Flows of a High-Speed Low-Pressure Turbine Cascade With Unsteady Wakes and Purge Flow	8
Compressor Stator Leading Edge Instrumentation	8
The Design of Aspirated Stators for Compressor Bleed	8
The Application of Fluidic Sealing in Shrouded Gas Turbine Blades	8
Predicting Endwall Corner Separation in Compressor Cascades Using RANS: Influence of Transition Treatment and Inflow Conditions	8
UHBR Open-Test Case Fan ECL5/CATANA: Non-Linear Analysis of Non-Synchronous Blade Vibration at Part-Speed Conditions	8
Advanced Design of a Transition Duct for Supersonic Inlet Turbines in Rotating Detonation Engines	8
Noise Source Identification for the Unsteady Low-Pressure Turbine Flow Fields	8
Film Superposition Characteristics With Laidback Fan-Shaped Holes Under the Influence of Internal Crossflow	8
Investigation of the Map Width Improvement in a Radially Reduced Diffuser Design Concept for a Centrifugal Compressor	8
Response of Separated Boundary Layers to Steady and Pulsated Flow Injection	8
A Three-Dimensional Actuator Disk Model for Fan Response to Inlet Distortion: Part I - Formulation	8
GPU-Accelerated Full-Wheel Large-Eddy Simulations of a Transonic Fan Stage	8
Impact of Fan Aerodynamics on Inlet Distortion at Crosswind	7
Collaborative Robust Design Optimization of Blade Geometry and Manufacturing Tolerance for a Transonic Centrifugal Impeller	7
Impact of Low Freestream Turbulence and Surface Roughness on the Flat-Plate Boundary Layer Transition Under a High-Lift Airfoil Pressure Gradient	7
Blade Vibration Analysis for Radial Turbine Featuring a Multi-Channel Casing Design	7
Aft Fuselage Boundary Layer Ingesting Propulsion System Design	7
Multiscale Data-Driven RANS Closure for Trailing Edge Cutback Film Cooling Flows	7
Reducing Low-Pressure Turbine Shroud Leakage Loss by Optimizing Leakage-Mainstream Interaction	7
Magnetic Resonance Velocimetry of a Turbine Blade With Engine-Representative Internal and Film Cooling Structures	7
Experimental and Numerical Investigation of High Load Turbine Blade Tip Cavity Structures	7
Robustness Analysis on Aerothermal Performance of the Winglet Squealer Tip—Part 1: Aerodynamic Performance	7
Investigating the Influence of Mainstream Turbulence and Large Vortices on Gas Turbine Trenched Film Cooling Flows Using Planar Temperature-Velocity Imaging	7
Experimental Research Into Aeroelastic Phenomena in Turbine Rotor Blades Inside ARIAS EU Project	7
Effect of Solidity and Aspect Ratio on the Aerodynamic Performance of Axial-Flow Fans With 0.2 Hub-to-Tip Ratio	7
Characterizing Flow Instabilities During Transient Events in the Turbine Rim Seal Cavity	7
The Effect of Inlet Conditions on Turbine Endwall Loss	7
Particle Bounce Stick Behavior in the Rotating Frame of Reference	7
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	7
Surge Inception Point Analysis Using the Greitzer Model for Centrifugal Compressor	7
Effects of Ribbed Surfaces on Profile Losses of Low-Pressure Turbine Blades	7
Manufacturing a Ceramic Turbine Rotor for a Compact Jet Engine	7
Adaptation of von Karman Institute for Fluid Dynamics’ Isentropic Compression Tube Facility for High-Speed Low-Pressure Turbines Testing	7
Impacts of Material and Machine on the Variation of Additively Manufactured Cooling Channels	7
Influences of Particulate Deposition on Vane Trailing-Edge Film Cooling: Adiabatic and Overall Cooling Effectiveness	7
A Free Streamline Model for Fully Separated Turbomachine Flows	7
Numerical Analysis of Sealing Flows in Gas Turbines Using RANS and Large Eddy Simulation Approaches	6
THE RELATIVE EFFECTS OF INTERNAL REYNOLDS NUMBER AND ADVECTIVE CAPACITY RATIO ON THE COOLANT WARMING FACTOR	6
Heat Transfer and Flow Field Characteristics of Variable Aspect Ratio, Serpentine Passages	6
Scale-Resolving Simulations of Turbulent Flow Retaining the Exact Blade Count With the Time-Inclined Method	6
Convergence Acceleration of Favre-Averaged Non-Linear Harmonic Method	6
Development of Compact and Hermetic Organic Rankine Cycle Turbine Generator With Upgraded Cooling Capability	6
High-Fidelity Computational Assessment of Aero-Thermal Performance and the Reynolds’ Analogy for Additively Manufactured Anisotropic Surface Roughness	6
Loss Analysis in Radial Inflow Turbines for Supercritical CO2 Mixtures	6
Wake–Separation Bubble Interaction Over an Experimentally Simulated Axial Compressor Blade Under Low Reynolds Number Flow	6
Innovative Cavity Modeling for Centrifugal Compressors Aeromechanical Analysis	6
Highly Time Resolved, Combined Temperature, and Heat Flux Measurement Technique Based on ALTP Sensors	6
The Influence of Combustor Hot Streaks on the Aerodynamic Performance of a Turbine Center Frame	6
Low Reynolds Number Effects on the Endwall Flow Field in a High-Lift Turbine Passage	6
A Test Facility for the Experimental Investigation of Labyrinth Seal Flutter and Early-Stage Validation of Prediction Techniques	6
Impact of the Purge Flow Density Ratio on the Rim Sealing Effectiveness in Hot Gas Ingestion Measurements	6
Wall-Modeled Large-Eddy Simulation of a Transonic Gas Turbine Vane—Part II: Mach Number Effect and Losses Prediction	6
Annular Dump Diffuser and Deswirl System for Back-Pressure Control in Engine-Scale Transonic Annular Cascade	6
Pressure Characteristic Rollover of a Transonic Centrifugal Impeller	6
Effects of Water-to-Air Mass Ratio on Long-Term Washing Efficiency and Erosion Risk in an Axial Compressor Under Online Washing Conditions	6
Experimental Investigation of Mode-Frequency Scattering at Fan Stages	6
Inverse Design of Compressor/Fan Blade Profiles Based on Conditional Invertible Neural Networks	6

The Influence of Boundary Layer State and Trailing Edge Wedge Angle on the Aerodynamic Performance of Transonic Turbine Blades	6
A New Nonlinear Time-Domain Flutter Analysis Approach for Distorted Flows	6
A Physics-Informed Neural Network for Solving the Inverse Heat Transfer Problem in Gas Turbine Rotating Cavities	6
A Shock Loss Reduction Method Using a Concave Suction Side Profile for a Zero Inlet Swirl Turbine Rotor	6
Plume Model for Buoyancy-Induced Flow and Heat Transfer in Closed Rotating Cavities	6
Transient Temperature Field Inversion of Turbine Based on Physics-Encoded Neural Networks	6
Turbine Nozzle Guide Vane Endwall Film Cooling and Vane Phantom Cooling Performances at Various Blocked Film Hole Configurations	6
Large Eddy Simulation of Laminar and Turbulent Shock/Boundary Layer Interactions in a Transonic Passage	6
Improvements in the Prediction of Steady and Unsteady Transition and Mixing in Low-Pressure Turbines by Means of Machine-Learnt Closures	6
Viability of Fiber Optic Temperature Sensors Embedded Within Engine-Scale Turbine Blades	6
Modeling of Combustor Non-Uniformities Evolution Through a High-Pressure Turbine Stage	6
Experimental Assessment of Squealer Tip Leakage Flow Structures in a Small-Core High-Speed Turbine	6
Efficient Aerodynamic Uncertainty Quantification for a Three-Dimensional Transonic Fan Rotor	6
Data Assimilation of Transitional and Separated Turbomachinery Flows With Physics-Informed Neural Networks	6
On the Secondary Flow System of an Aggressive Inter Compressor Duct	6
On the Mechanism of Unsteady Tip Flow Occurrence in a Transonic Fan	6
Multidisciplinary Optimization of a Mixed-Flow Impeller With 140 Parameters and Its Shapley Additive Explanations	6
Equation-Oriented Meanline Method for Axial Turbine Performance Prediction Under Choking Conditions	6
Experimental Study of Impact of In-Service Deterioration on Thermal Performance of High-Pressure Nozzle Guide Vanes	5
Considerations for Compressible Film Cooling: A Computational Study of the Effects of Transonic Flows and Varying Mainstream Mach Number	5
Cavity Impact on the Base Flow Unsteadiness for a High-Speed Exhaust System	5
Large Eddy Simulation Analysis of Loss Anomaly of a Turbine Blade With Large Trailing Edge Radius	5
A Resistive Model to Characterize Overall Effectiveness Influenced by Multiple Coolant Temperatures	5
Challenges in Aerodynamic Performance of Micro Gas Turbines and Design Inefficiencies	5
Validation of Broadband Noise Prediction Methodology Based on Linearized Navier–Stokes Analyses	5
Quasi-Dynamic Approximation of Unsteady Pressure Distribution for Transonic Airfoils in Flutter	5
Unsteady Loss Mechanisms in Low-Pressure Turbines With Diverging End-Walls Studied Via High-Fidelity Simulation	5
Characterizing the Unsteady Flow Field in Low-Flow Turbine Operation	5
Impact of Blowing and Density Ratio on the Film Cooling and Heat Transfer in an Aggressive Turbine Center Frame	5
The Impact of Manufacturing Variations on the Aerothermal Performance of High-Pressure Turbine Blade Shrouds	5
An Active Turbulence Grid for Turbomachinery Flow Experiments	5
The Unsteady Topology of Corner Separations	5
Investigation on Heat Transfer Distribution of Rotating Two-Pass Smooth and Ribbed Channels Under Aero-Engine Simulated Conditions	5
High-Dimensional Uncertainty Quantification of High-Pressure Turbine Vane Based on Multifidelity Deep Neural Networks	5
Effect of Geometry and Heat Flux on Turbine Over-Tip Flow Power Extraction	5
Scaling Heat Transfer and Pressure Losses of Novel Additively Manufactured Rib Designs	5
Aerodynamic Interaction Between Main Annulus Flow and Injected Secondary Air in Transonic High-Pressure Turbine Stage	5
The Effect of Reaction on Compressor Performance	5
Boundary Layer Analysis of a Transonic High-Pressure Turbine Vane Using Ultra-Fast-Response Temperature-Sensitive Paint	5
Turbine Vane Passage Cooling Experiments With a Close-Coupled Combustor–Turbine Interface Geometry Part II: Describing the Coolant Coverage	5
Non-Intrusive Ground Force Decomposition Applied to Turbofans—Part II: Filtered Rayleigh Scattering Application	5
Interaction Mechanism of Transonic Squealer Tip Cooling With the Effect of High-Speed Relative Casing Motion	5
Numerical Investigation of the Effect of Trailing Edge Thickness of Simulated Ceramic Matrix Composite Blades on Loss Profiles	5
Computational and Experimental Study of Film-Cooling Effectiveness With and Without Downstream Vortex Generators	5
Experimental Investigation of Flame-Film Cooling Interactions With an Academic Test Rig and Optical Laser Diagnostics	5
The Impact of Multiscale Ceramic Matrix Composite Roughness on Heat Transfer and Boundary Layer Behavior	5
Using Data Assimilation to Improve Turbulence Modeling for Inclined Jets in Crossflow	5
Unsteady Investigation of Intermediate Turbine Ducts Under the Influence of Purge Flows	5
Reynolds Number Effect on Transitional Delayed Detached-Eddy Simulation	5
Analysis of Radial Inlet Distortion on Transonic Fan Performance	5
Data-Driven Radial Compressor Design Space Mapping	5
A Digital Engineering Analysis of an Additively-Manufactured Turbine Vane	5
Analysis on the Effect of Cavity Flows on the Aerothermal Performance of a High-Pressure Turbine Stage	5
Validation of Filtered Rayleigh Scattering Optical Rake Measurement Techniques in Turbomachinery Applications and Boundary Layers	5
Mitigation of Boundary Layer Ingestion Circumferential Distortion Using Nonaxisymmetric Fan Exit Guide Vanes	5
A New Axial Compressor Test Facility for the Investigation of Aerodynamic Damping Featuring an Electromagnetic Excitation System	5
A Novel Cooling Design and Improvement of a Radial-Inflow Turbine Rotor Blade	4
Unsteady Flow Structure of Rotating Instability in a 1.5-Stage Axial Compressor	4
Impact of High Freestream Turbulence on Low-Pressure Turbine Endwall Flow—Part I: Loss Development and Time-Averaged Flow Field	4
Large Eddy Simulation Investigation of Film Cooling in Rotating Detonation Combustors	4
On Intake–Compressor Interactions Within an Integrated Propulsion System	4
Direct Numerical Simulation of a High-Pressure Turbine Stage: Unsteady Boundary Layer Transition and the Resulting Flow Structures	4
Unsteady Flow Development and Reynolds Stress Measurements in a Centrifugal Compressor Vaned Diffuser	4
Experimental Investigations on the Effects of Surface Roughness for Compressor Cascades With Different Roughness Magnitude and Location	4
The Role of Turbine Operating Conditions on Combustor–Turbine Interaction—Part II: Loading Effects	4
Fan Stability Enhancement With Partial Casing Treatments	4
Fan Flutter Mechanisms Related to Blade Mode Shape and Acoustic Properties	4
Investigation of a Novel Turbine Housing to Produce a Nonuniform Spanwise Flow Field at the Inlet to a Mixed Flow Turbine and Provide Variable Geometry Capabilities	4
Assessment of Computational Fluid Dynamic Modeling of Multi-Jet Impingement Cooling and Validation With the Experiments	4
Effect of Blade Damage on Low Pressure Ratio Fan Windmill Aerodynamics	4
Advanced Compressor Stall Warning Using Cross-Correlation and Deep Learning Based Approaches	4
A Parametric Study on the Influence of Acoustic Treatments in Fan Flutter	4
Film Cooling Comparison of Full-Scale Turbine Vanes Using the Pressure Sensitive Paint Technique	4
Impact of Flow Unsteadiness on Turbine Airfoil Heat Transfer via Streaming	4
Impact of Temperature Ratio on Overall Cooling Performance: Low-Order-Model-Based Analysis of Experiment Design	4
Experimental and Numerical Comparison of Two Turbine Vane Frame Designs	4
The Adverse Effect of Pre-Swirl on Ingestion in a Downstream Cavity	4
Influence of Casing Groove on Rotating Instabilities in a Low-Speed Axial Compressor	4
The Role of Turbine Operating Conditions on Combustor–Turbine Interaction—Part I: Change in Expansion Ratio	4
Numerical Characterization of Prestall Disturbances in a Compressor Stage	4
Reduced Order Modeling of the Unsteady Pressure on Turbine Rotor Blades Using Deep Learning	4
Control of Shroud Leakage Loss and Windage Torque in a Low-Pressure Turbine Stage	4
Investigation of a Transonic Dense Gas Flow Over an Idealized Blade Vane Configuration	4
Numerical Investigations on the Rotating Stall in an Axial Compressor and Its Control by Flow Injection at Casing	4
Numerical and Experimental Investigation of Boundary Layer of a High-Lift Low-Pressure Turbine Cascade Under Periodic Wakes With Different Flow Coefficients	4
Improved Eigenspace Perturbation Framework for RANS Structural Uncertainty Quantification in Transonic Compressor Flows	4
Vortex Unsteadiness in the Endwall Region of a High-Lift Low-Pressure Turbine Passage	4
Phantom Cooling Effects on Rotor Blade Surface Heat Flux in a Transonic Full Scale 1 + 1/2 Stage Rotating Turbine	4
Comparisons of Measured Blade Temperatures With Predictions Using Available Correlations	4
Analysis of Heat Transfer Within Buoyancy Dominated Rotating Cavities of High-Pressure Compressors	4
A Fluid–Structure Interaction Tool Using a Van der Pol-Based Reduced-Order Model for Buffet and Nonsynchronous Vibrations	4
Hybrid RANS-LES Simulation of Rotor–Stator Interaction in a Compressor Stage Using a Grid-Adaptive Simulation Method	4
The Effect of Upstream Unsteadiness on the Unstarting of a Supersonic Inlet Turbine	4
A Data-Driven Tip Flow Loss Prediction Method for a Transonic Fan Under Boundary Layer Ingesting Inflow Distortion	4
Use of Multiple Tracer Gases to Quantify Vane Trailing Edge Flow Into Turbine Rim Seals	4