Journal of Turbomachinery-Transactions of the Asme

Article	Citations
On the Use of Pressure-Sensitive Paint to Determine the Rim Sealing Effectiveness	47
An Improved Particle Impact Model by Accounting for Rate of Strain and Stochastic Rebound	37
Experimental Study on the High Relative Casing Motion Effect on Turbine Blade Tip Aerodynamic Characteristics	36
Effect of the Key Geometry and Flow Parameters on Discharge Coefficient of Laidback Fan-Shaped Hole Under Coolant Crossflow Condition	29
Effects of Radially Variable Sweep Vanes on Rotor–Stator Interaction Noise	28
Rotating Instabilities in Shrouded Low Pressure Turbine at Design and Off-Design Conditions	27
On the Divergence Mechanisms Analysis of a Vibrating Blade Subjected to Repetitive Rubs With an Abradable Coating	26
Turbine Vane Passage Cooling Experiments With a Close-Coupled Combustor-Turbine Interface Geometry—Part I: Describing the Flow	24
Analysis of the Bifurcating Duct of an Inlet Particle Separator in Transonic Flow Conditions	21
Evaluation of Cooling Requirements for Rotating Detonation Combustors	19
Three-Dimensional Unsteady Aerodynamic Optimization of a Transonic Compressor Stage Using an Implicit Discrete Adjoint Harmonic Balance Method	19
Exploring Topology Optimization for High Pressure Turbine Blade Tips	18
Performance Sensitivity of a Grooved Tip Seal to Manufacturing and Operational Geometry Deviations	18
An Exception Algorithm to Ease Convergence in Multistage Turbomachinery Throughflow Calculations	18
Corner Separation Control Using Sweeping Jet Actuator in a Compressor Cascade	18
Reviewer’s Recognition	17
Effect of Leading Edge Erosion on the Tip Leakage Flow in a Compressor Cascade	17
Physics-Guided Graph Neural Networks: Numerical Investigation of High-Pressure Turbine Flow	16
Nonlinear Flutter Analysis of Labyrinth Seals	16
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	16
Modeling and Simulation of Sand Particle Trajectories and Erosion in a Transonic Fan Stage	15
Fan Non-Synchronous Forced Vibration Under Crosswind	15
Prediction of Steady and Unsteady Flow Quantities Using Multiscale Graph Neural Networks	15
Wind Tunnel Continuous-Scan Acoustic Analysis of Ducted Fan Tones Interacting With a Shielding Wall	14
Film Cooling on Turbine Vane Endwalls With Different Inlet Cooling Configurations: Experimental and Computational Results	14

Effects of Blade Solidity and Aspect Ratio on a 0.5 Hub-to-Tip Ratio Tube-Axial Fan	14
A MULTISCALE REPRESENTATION OF TURBULENCE GENERATION IN COMPRESSOR FLOWS	14
Aerodynamic Effect of Shallow Circumferential Grooves in the Shroud of a Centrifugal Compressor	14
Measurements of Turbulence in Compressible Low-Density Flows at the Inlet of a Transonic Linear Cascade With and Without Unsteady Wakes	13
A Framework for Estimating Effects of Combustor Turbulence on Turbine Profile Loss Generation	13
The Effects of Swirling Flows in Entropy Wave Convection Through High-Pressure Turbine Stage	13
Development of a Novel Pressure-Based Approach for Blade Synchronous Vibration Detection Including Mistuning	13
Numerical Study on the Effect of Back Cavity on the Aerodynamic Behavior of a Non-Axisymmetric Casing Treatment for Transonic Axial Compressors	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
Unsteady Pre-Stall Behavior in a Centrifugal Compressor With Vaned Diffuser	12
An Analysis of the Secondary Flow Around a Tandem Blade Under the Presence of a Tip Gap in a High-Speed Linear Compressor Cascade	12
A Method for Preliminary Design of Variable Geometry Vaned Diffuser for Centrifugal Compressor	12
Acoustic Modes in an Open Box Cavity With Variable Depth Using Two Distinct Wind Tunnels	11
Pragmatic Prediction Model of Droplet Trajectory in a Turbine Cascade	11
Unique High-Resolution Temperature Mapping of Stage 1 Turbine Vane in a Long-Term Engine Test	11
NUMERICAL DESIGN OF EXPERIMENTS FOR REPEATING LOW-PRESSURE TURBINE STAGES PART I: COMPUTATIONAL OPPORTUNITIES AND METHODOLOGY	11
A Study of Loss Model Parameter Sensitivity in Compressor Unsteady Flow Simulations	11
Fundamentals of Scaling of Overall Cooling Effectiveness With Temperature Ratio	11
Aerothermal Performance Robustness and Reliability Analysis of Turbine Blade Squealer Tip With Film Cooling	10
Systematic Numerical Investigation on the Surface Roughness Effects on the Friction and Heat Transfer of Additively Manufactured Components	10
Inlet Flow Distortion in an Advanced Civil Transport Boundary Layer Ingesting Engine Installation	10
Tail-Integrated Boundary Layer Ingesting Propulsion Systems for Turbo-Electric Aircraft	10
Analysis of Complex Total Pressure Distortion Screens Using One-Dimensional Loss Data	10
Spectral Heat Transfer Coefficient for Thermal Design Analysis—Part 1: Augmenting the Cooling Law for Non-Isothermal Wall	10
Heat Transfer Measurements in a Turbine Centre Frame at Realistic Mach Number - Part 2: Influence of Combustor Hot Streaks	10
Effect of Axial Throughflow Swirl on Flow and Heat Transfer in a Compressor Disc Cavity	10
One-Dimensional Modeling for Pulsed Flow Twin-Entry Turbine	10
The Cooling Effect of Combustor Exit Louver Scheme on a Transonic Nozzle Guide Vane Endwall	10
Analytical Study on the Influence of Stage-Wise Distribution of Parameters on the Performance of a Multistage Axial Compressor	10
Loss Analysis of Cavity Leakage Flow in a Compressor Cascade	10
Experimental Investigation of Additional Loss Associated With Incoming Wakes in Low-Pressure Turbine Cascades	10
Modeling Deposition in Gas Turbines With Conjugate Mesh-Morphing and Temperature Sensitivity	9
Correlated Pressure–Velocity Instability in a Transonic High-Pressure Turbine Blade	9
Unpacking Intermineral Synergies and Reactions During Dust Deposition in an Impingement Coolant Jet	9
Stall Behavior in an Ultrahigh-Pressure-Ratio Centrifugal Compressor: Backward-Traveling Rotating Stall	9
Unsteady Flow Structure of Corner Separation in a Highly Loaded Compressor Cascade	9
Dirt Ingestion Impacts on Cooling Within a Double-Walled Combustor Liner	9
Effects of Downstream Vortex Generators on Film Cooling a Flat Plate Fed by Crossflow	9
An Experimental Investigation of Sweeping Mist Jet Film Cooling With Droplet Analysis	9
Performance and Secondary Flow Structures Characterization in a Highly Loaded Low-Pressure Compressor Under Distorted Inflow Conditions	9
Particle Image Velocimetry in a High-Speed Short-Duration Turbine Rig	9
The Influence of Turbulence and Reynolds Number on Endwall Heat Transfer in a Vane Cascade	9
Experimental Study on Controlling Flow Separation of Compressor Cascades With Self-Excited Sweeping Jet Actuator	9
Unsteady Aerodynamic Forcing Due to Distortion in a Boundary Layer Ingesting Fan	9
Numerical Modeling and Design Challenges of Boundary Layer Ingesting Fans	9
On the Over-Prediction of Centrifugal Compressor Pressure Ratio in the High Impeller Tip Mach Number Regime	9
Entry Region Heat Transfer Augmentation With Pins, Fins, and Turbulators in Circular Channels	9
Multistage Turbomachinery Optimization for High-Temperature Heat Pumps With the Reverse Rankine Cycle	9
Flow and Heat Transfer in a Rotating Disc Cavity With Axial Throughflow at High-Speed Conditions	9

Effect of Upstream Leakage Flow on Film Cooling Characteristic of a Turbine Convex Endwall	9
Effect of Purge-Mainstream Density Ratio on the Secondary Flow Field of a Turbine Blade Row	9
Experimental Determination of Heat Transfer Coefficient on Impingement Cooled Gear Flanks: Validation of the Evaluation Method	9
Impact of High-Pressure-Turbine Purge Flow on the Evolution of Turbulence in a Turbine Vane Frame	8
High-Fidelity Investigation of Vortex Shedding From a Highly Loaded Turbine Blade	8
An Improved Passage-Flow Turning Model for Forward-Curved Blades of Squirrel-Cage Fan	8
Numerical Study of Crossflow Effects on Discharge Coefficient of the Converging Slot Hole	8
Numerical Investigation on the Influence of Wet Compression Aerodynamic Performance of Multi-Stage Transonic Compressor	8
Numerical Study on Unsteady Flow of a Supersonic Partial Admission Impulse Turbine	8
ANALYSIS OF AEROACOUSTIC PHENOMENA IN CENTRIFUGAL COMPRESSORS USING A LATTICE BOLTZMANN FLOW SIMULATION APPROACH	8
Numerical Assessment of an Aerodynamic Probe to Enable Short Focal Length Laser Diagnostics in High Temperature Supersonic Flows Based on Flow Disturbance	8
Revisiting Dimensionless Parameters Quantifying Film Cooling	8
Blade Envelopes Part I: Concept and Methodology	8
Comparative Investigation of HPT Blade Cooling Concepts in an Aerothermal Test Rig	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
Dissipation in Skewed Boundary Layers	8
Windage Torque Reduction in Low-Pressure Turbine Cavities Part II: Experimental and Numerical Results	8
Flow Check and Adiabatic Effectiveness Measurements on Traditionally Versus Additively Manufactured Film-Cooling Holes	8
Insights Into Turbocharger Centrifugal Compressor Stability Using High-Fidelity Computational Fluid Dynamics and a Novel Impeller Diffusion Factor	8
Investigation of Tip Leakage Vortex Breakdown in a High-Speed Multistage Axial Compressor	8
RANS Capabilities for Transonic Axial Compressor: A Perspective From GPPS Computational Fluid Dynamics Workshop	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]	7
A Three-Dimensional Actuator Disk Model for Fan Response to Inlet Distortion: Part I - Formulation	7
Multiscale Data-Driven RANS Closure for Trailing Edge Cutback Film Cooling Flows	7
Heat Transfer in an Injector-Scaled Additively Manufactured Fuel Passage	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
The Design of Aspirated Stators for Compressor Bleed	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
Film Superposition Characteristics With Laidback Fan-Shaped Holes Under the Influence of Internal Crossflow	7
Response of Separated Boundary Layers to Steady and Pulsated Flow Injection	7
Optimal Riblets Applied to Gas Turbine Compressor Blades Studied via Direct Numerical Simulation (GT2024–122305)	7
UHBR Open-Test Case Fan ECL5/CATANA: Non-Linear Analysis of Non-Synchronous Blade Vibration at Part-Speed Conditions	7
Cooling Performance of Additively Manufactured Pin Fins in Stacked Microchannels for the Inside-Out Ceramic Turbine Shroud-Cooling Ring	7
Optimization of a Tip Appendage for the Control of Tip Leakage Vortices in Axial Flow Fans	7
Comparative Study of Tip Injection in a Transonic and Subsonic Compressor	7
Strategies for High-Accuracy Measurements of Stage Efficiency for a Cooled Turbine	7
Compressor Stator Leading Edge Instrumentation	7
Noise Source Identification for the Unsteady Low-Pressure Turbine Flow Fields	7
Morphing of Reversible Axial Fan Blade: A FSI-FEM Study	7
A Detailed Loss Analysis Methodology for Centrifugal Compressors	7
Influences of Particulate Deposition on Vane Trailing-Edge Film Cooling: Adiabatic and Overall Cooling Effectiveness	7
Reducing Low-Pressure Turbine Shroud Leakage Loss by Optimizing Leakage-Mainstream Interaction	7
Characterizing Flow Instabilities During Transient Events in the Turbine Rim Seal Cavity	7
Experimental and Numerical Investigation of High Load Turbine Blade Tip Cavity Structures	7
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	7
Numerical Investigation of the Fan Flutter Mechanism Related to Acoustic Propagation Characteristics	7
Investigation of the Map Width Improvement in a Radially Reduced Diffuser Design Concept for a Centrifugal Compressor	7
A Review of Secondary Combustion on the Turbine Blade Cooling	7
Advanced Design of a Transition Duct for Supersonic Inlet Turbines in Rotating Detonation Engines	7
Sensitivity Analysis for Flow Stability of Axial Compressor Based on Meridional Flow	7
Wake–Separation Bubble Interaction Over an Experimentally Simulated Axial Compressor Blade Under Low Reynolds Number Flow	6
Effects of Rotation on the Flow Structure in a Compressor Cascade	6
A New Nonlinear Time-Domain Flutter Analysis Approach for Distorted Flows	6
Impact of Low Freestream Turbulence and Surface Roughness on the Flat-Plate Boundary Layer Transition Under a High-Lift Airfoil Pressure Gradient	6
Manufacturing a Ceramic Turbine Rotor for a Compact Jet Engine	6
Highly Time Resolved, Combined Temperature, and Heat Flux Measurement Technique Based on ALTP Sensors	6
Robustness Analysis on Aerothermal Performance of the Winglet Squealer Tip—Part 1: Aerodynamic Performance	6
Investigating the Influence of Mainstream Turbulence and Large Vortices on Gas Turbine Trenched Film Cooling Flows Using Planar Temperature-Velocity Imaging	6
Experimental Research Into Aeroelastic Phenomena in Turbine Rotor Blades Inside ARIAS EU Project	6
Effect of Solidity and Aspect Ratio on the Aerodynamic Performance of Axial-Flow Fans With 0.2 Hub-to-Tip Ratio	6
Particle Bounce Stick Behavior in the Rotating Frame of Reference	6
A Shock Loss Reduction Method Using a Concave Suction Side Profile for a Zero Inlet Swirl Turbine Rotor	6
On the Mechanism of Unsteady Tip Flow Occurrence in a Transonic Fan	6
The Influence of Combustor Hot Streaks on the Aerodynamic Performance of a Turbine Center Frame	6
Efficient Aerodynamic Uncertainty Quantification for a Three-Dimensional Transonic Fan Rotor	6
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	6
Transient Temperature Field Inversion of Turbine Based on Physics-Encoded Neural Networks	6
Effects of Ribbed Surfaces on Profile Losses of Low-Pressure Turbine Blades	6
Multidisciplinary Optimization of a Mixed-Flow Impeller With 140 Parameters and Its Shapley Additive Explanations	6
Collaborative Robust Design Optimization of Blade Geometry and Manufacturing Tolerance for a Transonic Centrifugal Impeller	6
Aft Fuselage Boundary Layer Ingesting Propulsion System Design	6
Blade Vibration Analysis for Radial Turbine Featuring a Multi-Channel Casing Design	6
A New Loss Generation Body Force Model for Fan/Compressor Blade Rows: Application to Uniform and Non-Uniform Inflow in Rotor 67	6
Predicting Endwall Corner Separation in Compressor Cascades Using RANS: Influence of Transition Treatment and Inflow Conditions	6
Impacts of Material and Machine on the Variation of Additively Manufactured Cooling Channels	6
GPU-Accelerated Full-Wheel Large-Eddy Simulations of a Transonic Fan Stage	6
The Effects of Incoming Vortex and Wake on the Aerodynamics of an Intermediate Turbine Duct	6
Innovative Cavity Modeling for Centrifugal Compressors Aeromechanical Analysis	6
The Influence of Boundary Layer State and Trailing Edge Wedge Angle on the Aerodynamic Performance of Transonic Turbine Blades	6

A Test Facility for the Experimental Investigation of Labyrinth Seal Flutter and Early-Stage Validation of Prediction Techniques	6
Plume Model for Buoyancy-Induced Flow and Heat Transfer in Closed Rotating Cavities	6
A Physics-Informed Neural Network for Solving the Inverse Heat Transfer Problem in Gas Turbine Rotating Cavities	6
The Influence of Purge Flow Parameters on Heat Transfer and Film Cooling in Turbine Center Frames	6
Data Assimilation of Transitional and Separated Turbomachinery Flows With Physics-Informed Neural Networks	6
Adaptation of von Karman Institute for Fluid Dynamics’ Isentropic Compression Tube Facility for High-Speed Low-Pressure Turbines Testing	6
Equation-Oriented Meanline Method for Axial Turbine Performance Prediction Under Choking Conditions	6
A Free Streamline Model for Fully Separated Turbomachine Flows	6
The Effect of Inlet Conditions on Turbine Endwall Loss	6
Magnetic Resonance Velocimetry of a Turbine Blade With Engine-Representative Internal and Film Cooling Structures	6
Surge Inception Point Analysis Using the Greitzer Model for Centrifugal Compressor	6
Impact of Fan Aerodynamics on Inlet Distortion at Crosswind	6
Effect of Coolant Crossflow on Film Cooling Effectiveness of Diffusion Slot Hole With and Without Ribs	5
Experimental Investigation of Mode-Frequency Scattering at Fan Stages	5
Quasi-Dynamic Approximation of Unsteady Pressure Distribution for Transonic Airfoils in Flutter	5
Inverse Design of Compressor/Fan Blade Profiles Based on Conditional Invertible Neural Networks	5
Effects on Film Cooling Performance in the Showerhead From Geometric Parameterization of Shaped Hole Designs	5
Low Reynolds Number Effects on the Endwall Flow Field in a High-Lift Turbine Passage	5
Convergence Acceleration of Favre-Averaged Non-Linear Harmonic Method	5
Impact of Blowing and Density Ratio on the Film Cooling and Heat Transfer in an Aggressive Turbine Center Frame	5
An Active Turbulence Grid for Turbomachinery Flow Experiments	5
High-Fidelity Computational Assessment of Aero-Thermal Performance and the Reynolds’ Analogy for Additively Manufactured Anisotropic Surface Roughness	5
Scale-Resolving Simulations of Turbulent Flow Retaining the Exact Blade Count With the Time-Inclined Method	5
Modeling of Combustor Non-Uniformities Evolution Through a High-Pressure Turbine Stage	5
Interaction Mechanism of Transonic Squealer Tip Cooling With the Effect of High-Speed Relative Casing Motion	5
Experimental Assessment of Squealer Tip Leakage Flow Structures in a Small-Core High-Speed Turbine	5
Experimental and Numerical Analysis of Loss Characteristics of Cooled Transonic Nozzle Guide Vanes	5
Loss Analysis in Radial Inflow Turbines for Supercritical CO2 Mixtures	5
Investigation on Heat Transfer Distribution of Rotating Two-Pass Smooth and Ribbed Channels Under Aero-Engine Simulated Conditions	5
Improved Prediction of Losses With Large Eddy Simulation in a Low-Pressure Turbine	5
On the Secondary Flow System of an Aggressive Inter Compressor Duct	5
Experimental Investigation of Flame-Film Cooling Interactions With an Academic Test Rig and Optical Laser Diagnostics	5
Effective Clearance and Differential Gapping Impact on Seal Flutter Modeling and Validation	5
Wall-Modeled Large-Eddy Simulation of a Transonic Gas Turbine Vane—Part II: Mach Number Effect and Losses Prediction	5
Pressure Characteristic Rollover of a Transonic Centrifugal Impeller	5
High-Dimensional Uncertainty Quantification of High-Pressure Turbine Vane Based on Multifidelity Deep Neural Networks	5
Heat Transfer and Flow Field Characteristics of Variable Aspect Ratio, Serpentine Passages	5
A Digital Engineering Analysis of an Additively-Manufactured Turbine Vane	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
Large Eddy Simulation of Laminar and Turbulent Shock/Boundary Layer Interactions in a Transonic Passage	5
Development of Compact and Hermetic Organic Rankine Cycle Turbine Generator With Upgraded Cooling Capability	5
Improvements in the Prediction of Steady and Unsteady Transition and Mixing in Low-Pressure Turbines by Means of Machine-Learnt Closures	5
Impact of the Purge Flow Density Ratio on the Rim Sealing Effectiveness in Hot Gas Ingestion Measurements	5
Boundary Layer Analysis of a Transonic High-Pressure Turbine Vane Using Ultra-Fast-Response Temperature-Sensitive Paint	5
Turbine Nozzle Guide Vane Endwall Film Cooling and Vane Phantom Cooling Performances at Various Blocked Film Hole Configurations	5
Annular Dump Diffuser and Deswirl System for Back-Pressure Control in Engine-Scale Transonic Annular Cascade	5
Machine Learning for the Development of Data-Driven Turbulence Closures in Coolant Systems	4
Numerical Characterization of Prestall Disturbances in a Compressor Stage	4
Extending Highly Loaded Axial Fan Operability Range Through Novel Blade Design	4
Design and Testing of a Multi-Stage Intermediate Pressure Turbine for Future Geared Turbofans	4
Data-Driven Radial Compressor Design Space Mapping	4
Phantom Cooling Effects on Rotor Blade Surface Heat Flux in a Transonic Full Scale 1 + 1/2 Stage Rotating Turbine	4
The Unsteady Topology of Corner Separations	4
Hybrid RANS-LES Simulation of Rotor–Stator Interaction in a Compressor Stage Using a Grid-Adaptive Simulation Method	4
Analysis of Averaging Methods for Nonuniform Total Pressure Fields	4
Mitigation of Boundary Layer Ingestion Circumferential Distortion Using Nonaxisymmetric Fan Exit Guide Vanes	4
Scaling Heat Transfer and Pressure Losses of Novel Additively Manufactured Rib Designs	4
Characterizing the Unsteady Flow Field in Low-Flow Turbine Operation	4
Experimental and Numerical Comparison of Two Turbine Vane Frame Designs	4
Unsteady Loss Mechanisms in Low-Pressure Turbines With Diverging End-Walls Studied Via High-Fidelity Simulation	4
Impact of Temperature Ratio on Overall Cooling Effectiveness: Experimental Validation of a Scaling Theory	4
Unsteady Structure of Compressor Tip Leakage Flows	4
Influence of Casing Groove on Rotating Instabilities in a Low-Speed Axial Compressor	4
A Data-Driven Approach for Generalizing the Laminar Kinetic Energy Model for Separation and Bypass Transition in Low- and High-Pressure Turbines	4
Impact of Flow Unsteadiness on Turbine Airfoil Heat Transfer via Streaming	4
The Effect of Upstream Unsteadiness on the Unstarting of a Supersonic Inlet Turbine	4
The Impact of the Off-Design Conditions on the Entropy Wave Interaction With a High-Pressure Turbine Stage	4
Reynolds Number Effect on Transitional Delayed Detached-Eddy Simulation	4
Experimental Investigation of the Pre-Stall and Stall Evolution in a Centrifugal Compressor With a Volute	4
Considerations for Compressible Film Cooling: A Computational Study of the Effects of Transonic Flows and Varying Mainstream Mach Number	4
Effect of Geometry and Heat Flux on Turbine Over-Tip Flow Power Extraction	4
Non-Intrusive Ground Force Decomposition Applied to Turbofans—Part II: Filtered Rayleigh Scattering Application	4
Numerical Investigation of the Effect of Trailing Edge Thickness of Simulated Ceramic Matrix Composite Blades on Loss Profiles	4
The Role of Turbine Operating Conditions on Combustor–Turbine Interaction—Part I: Change in Expansion Ratio	4
Experimental Study of Impact of In-Service Deterioration on Thermal Performance of High-Pressure Nozzle Guide Vanes	4
Unsteady Flow Development and Reynolds Stress Measurements in a Centrifugal Compressor Vaned Diffuser	4
Cavity Impact on the Base Flow Unsteadiness for a High-Speed Exhaust System	4
Validation of Broadband Noise Prediction Methodology Based on Linearized Navier–Stokes Analyses	4
Heat Transfer Coefficient and Adiabatic Wall Temperature Measurements on High-Pressure Turbine Nozzle Guide Vanes With Representative Inlet Swirl and Temperature Distortions	4
Fan Flutter Mechanisms Related to Blade Mode Shape and Acoustic Properties	4
Simplified Model and Approach to Transform Infrared Surface Temperature to Film Effectiveness in a Conjugate Heat Transfer Experiment	4
Erratum: “Scaling Roughness Effects on Pressure Loss and Heat Transfer of Additively Manufactured Channels” [J. Turbomach. 139(2), p. 021003; DOI: 10.1115/1.4034555]	4
Turbine Vane Passage Cooling Experiments With a Close-Coupled Combustor–Turbine Interface Geometry Part II: Describing the Coolant Coverage	4
A Simplified Injection Model for Variable Area Turbine Fluidic Throttling	4
Computational and Experimental Study of Film-Cooling Effectiveness With and Without Downstream Vortex Generators	4
Analysis of Radial Inlet Distortion on Transonic Fan Performance	4
The Impact of Multiscale Ceramic Matrix Composite Roughness on Heat Transfer and Boundary Layer Behavior	4
Validation of Filtered Rayleigh Scattering Optical Rake Measurement Techniques in Turbomachinery Applications and Boundary Layers	4
The Role of Turbine Operating Conditions on Combustor–Turbine Interaction—Part II: Loading Effects	4
A New Axial Compressor Test Facility for the Investigation of Aerodynamic Damping Featuring an Electromagnetic Excitation System	4
Bayesian Mass Averaging in Rigs and Engines	4
The Impact of Manufacturing Variations on the Aerothermal Performance of High-Pressure Turbine Blade Shrouds	4
Analysis of Heat Transfer Within Buoyancy Dominated Rotating Cavities of High-Pressure Compressors	4
Aero-Structural Coupling Strategy for a Morphing Blade Cascade Study	4
Stall Warning and Adaptive Control Subjected to Rotating Inlet Distortion in Axial Flow Compressor	4