Journal of Turbomachinery-Transactions of the Asme

Article	Citations
Effects of Radially Variable Sweep Vanes on Rotor–Stator Interaction Noise	34
Effect of the Key Geometry and Flow Parameters on Discharge Coefficient of Laidback Fan-Shaped Hole Under Coolant Crossflow Condition	32
Corner Separation Control Using Sweeping Jet Actuator in a Compressor Cascade	29
An Improved Particle Impact Model by Accounting for Rate of Strain and Stochastic Rebound	27
Effect of Leading Edge Erosion on the Tip Leakage Flow in a Compressor Cascade	23
Experimental Study on the High Relative Casing Motion Effect on Turbine Blade Tip Aerodynamic Characteristics	22
Coupled Time and Passage Spectral Method for an Efficient Resolution of Turbomachinery Far Upstream Wakes	22
Analysis of the Bifurcating Duct of an Inlet Particle Separator in Transonic Flow Conditions	21
Turbine Vane Passage Cooling Experiments With a Close-Coupled Combustor-Turbine Interface Geometry—Part I: Describing the Flow	20
Three-Dimensional Unsteady Aerodynamic Optimization of a Transonic Compressor Stage Using an Implicit Discrete Adjoint Harmonic Balance Method	20
On the Use of Pressure-Sensitive Paint to Determine the Rim Sealing Effectiveness	19
Exploring Topology Optimization for High Pressure Turbine Blade Tips	18
Rotating Instabilities in Shrouded Low Pressure Turbine at Design and Off-Design Conditions	18
Evaluation of Cooling Requirements for Rotating Detonation Combustors	17
Numerical Study on the Effect of Back Cavity on the Aerodynamic Behavior of a Non-Axisymmetric Casing Treatment for Transonic Axial Compressors	16
On the Divergence Mechanisms Analysis of a Vibrating Blade Subjected to Repetitive Rubs With an Abradable Coating	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
Fan Non-Synchronous Forced Vibration Under Crosswind	15
Introduction of Axisymmetric Grooves as a Tip Seal Treatment for Small-Core Turbines	14
A Method for Preliminary Design of Variable Geometry Vaned Diffuser for Centrifugal Compressor	14
Measurements of Turbulence in Compressible Low-Density Flows at the Inlet of a Transonic Linear Cascade With and Without Unsteady Wakes	14
A New Multi-Stage Turbine Stator Design for Improved Performance Retention	14
The Effects of Swirling Flows in Entropy Wave Convection Through High-Pressure Turbine Stage	14
Modeling and Simulation of Sand Particle Trajectories and Erosion in a Transonic Fan Stage	14
Nonlinear Flutter Analysis of Labyrinth Seals	14

Reviewer’s Recognition	14
Foam-Metal Casing Treatment on an Axial Flow Compressor: Stability Improvement and Noise Reduction	13
Prediction of Steady and Unsteady Flow Quantities Using Multiscale Graph Neural Networks	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
Physics-Guided Graph Neural Networks: Numerical Investigation of High-Pressure Turbine Flow	12
A Framework for Estimating Effects of Combustor Turbulence on Turbine Profile Loss Generation	12
Unsteady Pre-Stall Behavior in a Centrifugal Compressor With Vaned Diffuser	12
Film Cooling on Turbine Vane Endwalls With Different Inlet Cooling Configurations: Experimental and Computational Results	12
Loss Analysis of Cavity Leakage Flow in a Compressor Cascade	11
The Cooling Effect of Combustor Exit Louver Scheme on a Transonic Nozzle Guide Vane Endwall	11
One-Dimensional Modeling for Pulsed Flow Twin-Entry Turbine	11
Inlet Flow Distortion in an Advanced Civil Transport Boundary Layer Ingesting Engine Installation	11
Unique High-Resolution Temperature Mapping of Stage 1 Turbine Vane in a Long-Term Engine Test	11
A Study of Loss Model Parameter Sensitivity in Compressor Unsteady Flow Simulations	11
Spectral Heat Transfer Coefficient for Thermal Design Analysis—Part 1: Augmenting the Cooling Law for Non-Isothermal Wall	11
Pragmatic Prediction Model of Droplet Trajectory in a Turbine Cascade	11
Acoustic Modes in an Open Box Cavity With Variable Depth Using Two Distinct Wind Tunnels	11
Fundamentals of Scaling of Overall Cooling Effectiveness With Temperature Ratio	11
Tail-Integrated Boundary Layer Ingesting Propulsion Systems for Turbo-Electric Aircraft	11
Effects of Downstream Vortex Generators on Film Cooling a Flat Plate Fed by Crossflow	10
Analysis of Complex Total Pressure Distortion Screens Using One-Dimensional Loss Data	10
Entry Region Heat Transfer Augmentation With Pins, Fins, and Turbulators in Circular Channels	10
Impacts of Tandem Configurations on the Aerodynamic Performance of an Axial Supersonic Through-Flow Fan Cascade	10
Experimental Determination of Heat Transfer Coefficient on Impingement Cooled Gear Flanks: Validation of the Evaluation Method	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
The Influence of Turbulence and Reynolds Number on Endwall Heat Transfer in a Vane Cascade	10
Correlated Pressure–Velocity Instability in a Transonic High-Pressure Turbine Blade	10
Experimental Study on Controlling Flow Separation of Compressor Cascades With Self-Excited Sweeping Jet Actuator	9
Numerical Modeling and Design Challenges of Boundary Layer Ingesting Fans	9
Effects of Surface Waviness on Fan Blade Boundary Layer Transition and Profile Loss—Part I: Methodology and Computational Results	9
Aerodynamics and Heat Transfer Inside a Gas Turbine Mid-Passage Gap	9
Aerothermal Performance Robustness and Reliability Analysis of Turbine Blade Squealer Tip With Film Cooling	9
Unsteady Flow Structure of Corner Separation in a Highly Loaded Compressor Cascade	9
Flow and Heat Transfer in a Rotating Disc Cavity With Axial Throughflow at High-Speed Conditions	9
Experimental Investigation of Additional Loss Associated With Incoming Wakes in Low-Pressure Turbine Cascades	9
Stall Behavior in an Ultrahigh-Pressure-Ratio Centrifugal Compressor: Backward-Traveling Rotating Stall	9
Numerical Assessment of an Aerodynamic Probe to Enable Short Focal Length Laser Diagnostics in High Temperature Supersonic Flows Based on Flow Disturbance	9
Multistage Turbomachinery Optimization for High-Temperature Heat Pumps With the Reverse Rankine Cycle	9
On the Over-Prediction of Centrifugal Compressor Pressure Ratio in the High Impeller Tip Mach Number Regime	9
Unsteady Aerodynamic Forcing Due to Distortion in a Boundary Layer Ingesting Fan	9
Numerical Study on Unsteady Flow of a Supersonic Partial Admission Impulse Turbine	8
RANS Capabilities for Transonic Axial Compressor: A Perspective From GPPS Computational Fluid Dynamics Workshop	8
High-Fidelity Investigation of Vortex Shedding From a Highly Loaded Turbine Blade	8
Dirt Ingestion Impacts on Cooling Within a Double-Walled Combustor Liner	8
Blade Envelopes Part I: Concept and Methodology	8
Investigation of Tip Leakage Vortex Breakdown in a High-Speed Multistage Axial Compressor	8
Direct and Inverse Model for Single-Hole Film Cooling With Machine Learning	8
Numerical Study of Crossflow Effects on Discharge Coefficient of the Converging Slot Hole	8
Revisiting Dimensionless Parameters Quantifying Film Cooling	8

Insights Into Turbocharger Centrifugal Compressor Stability Using High-Fidelity Computational Fluid Dynamics and a Novel Impeller Diffusion Factor	8
An Improved Passage-Flow Turning Model for Forward-Curved Blades of Squirrel-Cage Fan	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
Numerical Investigation on the Influence of Wet Compression Aerodynamic Performance of Multi-Stage Transonic Compressor	8
Effect of Upstream Leakage Flow on Film Cooling Characteristic of a Turbine Convex Endwall	8
Morphing of Reversible Axial Fan Blade: A FSI-FEM Study	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
Response of Separated Boundary Layers to Steady and Pulsated Flow Injection	7
Noise Source Identification for the Unsteady Low-Pressure Turbine Flow Fields	7
Strategies for High-Accuracy Measurements of Stage Efficiency for a Cooled Turbine	7
Film-Cooling Performance Comparison of Blade Tips With a Trailing Edge, Pressure Side Cutback, or a Suction Side Squealer in a Transonic Linear Cascade	7
Investigation of the Map Width Improvement in a Radially Reduced Diffuser Design Concept for a Centrifugal Compressor	7
Particle Bounce Stick Behavior in the Rotating Frame of Reference	7
The Influence of Deterministic Surface Roughness and Freestream Turbulence on Transitional Boundary Layers: Heat Transfer Distributions and a New Transition Onset Correlation	7
Film Superposition Characteristics With Laidback Fan-Shaped Holes Under the Influence of Internal Crossflow	7
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
Suppression of Nonsynchronous Vibration Through Intentional Aerodynamic and Structural Mistuning	7
Sensitivity Analysis for Flow Stability of Axial Compressor Based on Meridional Flow	7
Advanced Design of a Transition Duct for Supersonic Inlet Turbines in Rotating Detonation Engines	7
A Review of Secondary Combustion on the Turbine Blade Cooling	7
A Detailed Loss Analysis Methodology for Centrifugal Compressors	7
Optimization of a Tip Appendage for the Control of Tip Leakage Vortices in Axial Flow Fans	7
Numerical Investigation of the Fan Flutter Mechanism Related to Acoustic Propagation Characteristics	7
The Application of Fluidic Sealing in Shrouded Gas Turbine Blades	7
Application of Advanced RANS Turbulence Models for the Prediction of Turbomachinery Flows	7
Unsteadiness in the Secondary Flows of a High-Speed Low-Pressure Turbine Cascade With Unsteady Wakes and Purge Flow	7
Dissipation in Skewed Boundary Layers	7
Impact of High-Pressure-Turbine Purge Flow on the Evolution of Turbulence in a Turbine Vane Frame	7
Heat Transfer in an Injector-Scaled Additively Manufactured Fuel Passage	6
Equation-Oriented Meanline Method for Axial Turbine Performance Prediction Under Choking Conditions	6
A Shock Loss Reduction Method Using a Concave Suction Side Profile for a Zero Inlet Swirl Turbine Rotor	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
A New Loss Generation Body Force Model for Fan/Compressor Blade Rows: Application to Uniform and Non-Uniform Inflow in Rotor 67	6
Plume Model for Buoyancy-Induced Flow and Heat Transfer in Closed Rotating Cavities	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
UHBR Open-Test Case Fan ECL5/CATANA: Non-Linear Analysis of Non-Synchronous Blade Vibration at Part-Speed Conditions	6
Cooling Performance of Additively Manufactured Pin Fins in Stacked Microchannels for the Inside-Out Ceramic Turbine Shroud-Cooling Ring	6
A Free Streamline Model for Fully Separated Turbomachine Flows	6
Robustness Analysis on Aerothermal Performance of the Winglet Squealer Tip—Part 1: Aerodynamic Performance	6
Manufacturing a Ceramic Turbine Rotor for a Compact Jet Engine	6
The Effects of Incoming Vortex and Wake on the Aerodynamics of an Intermediate Turbine Duct	6
Collaborative Robust Design Optimization of Blade Geometry and Manufacturing Tolerance for a Transonic Centrifugal Impeller	6
Impact of Low Freestream Turbulence and Surface Roughness on the Flat-Plate Boundary Layer Transition Under a High-Lift Airfoil Pressure Gradient	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
A High-Speed Disk Rotor Rig Design for Tip Aerothermal Research	6
Blade Vibration Analysis for Radial Turbine Featuring a Multi-Channel Casing Design	6
Characterizing Flow Instabilities During Transient Events in the Turbine Rim Seal Cavity	6
GPU-Accelerated Full-Wheel Large-Eddy Simulations of a Transonic Fan Stage	6
Experimental and Numerical Investigation of High Load Turbine Blade Tip Cavity Structures	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
Comparative Study of Tip Injection in a Transonic and Subsonic Compressor	6
Impact of Swirling Entropy Waves on a High Pressure Turbine	6
A New Nonlinear Time-Domain Flutter Analysis Approach for Distorted Flows	6
Highly Time Resolved, Combined Temperature, and Heat Flux Measurement Technique Based on ALTP Sensors	6
Effects of Ribbed Surfaces on Profile Losses of Low-Pressure Turbine Blades	6
Effect of Solidity and Aspect Ratio on the Aerodynamic Performance of Axial-Flow Fans With 0.2 Hub-to-Tip Ratio	6
The Influence of Combustor Hot Streaks on the Aerodynamic Performance of a Turbine Center Frame	6
Magnetic Resonance Velocimetry of a Turbine Blade With Engine-Representative Internal and Film Cooling Structures	6
Optimal Riblets Applied to Gas Turbine Compressor Blades Studied via Direct Numerical Simulation (GT2024–122305)	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
The Effect of Inlet Conditions on Turbine Endwall Loss	6
Impact of Blowing and Density Ratio on the Film Cooling and Heat Transfer in an Aggressive Turbine Center Frame	5
Quasi-Dynamic Approximation of Unsteady Pressure Distribution for Transonic Airfoils in Flutter	5
Improved Prediction of Losses With Large Eddy Simulation in a Low-Pressure Turbine	5
Turbine Nozzle Guide Vane Endwall Film Cooling and Vane Phantom Cooling Performances at Various Blocked Film Hole Configurations	5
Pressure Characteristic Rollover of a Transonic Centrifugal Impeller	5
Heat Transfer and Flow Field Characteristics of Variable Aspect Ratio, Serpentine Passages	5
Improvements in the Prediction of Steady and Unsteady Transition and Mixing in Low-Pressure Turbines by Means of Machine-Learnt Closures	5
Efficient Aerodynamic Uncertainty Quantification for a Three-Dimensional Transonic Fan Rotor	5
Innovative Cavity Modeling for Centrifugal Compressors Aeromechanical Analysis	5
Inverse Design of Compressor/Fan Blade Profiles Based on Conditional Invertible Neural Networks	5
Loss Analysis in Radial Inflow Turbines for Supercritical CO2 Mixtures	5
Experimental Investigation of Mode-Frequency Scattering at Fan Stages	5
Experimental and Numerical Analysis of Loss Characteristics of Cooled Transonic Nozzle Guide Vanes	5
An Active Turbulence Grid for Turbomachinery Flow Experiments	5

Analysis of Averaging Methods for Nonuniform Total Pressure Fields	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
Annular Dump Diffuser and Deswirl System for Back-Pressure Control in Engine-Scale Transonic Annular Cascade	5
Large Eddy Simulation of Laminar and Turbulent Shock/Boundary Layer Interactions in a Transonic Passage	5
Low Reynolds Number Effects on the Endwall Flow Field in a High-Lift Turbine Passage	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
Wake–Separation Bubble Interaction Over an Experimentally Simulated Axial Compressor Blade Under Low Reynolds Number Flow	5
Effects of Rotation on the Flow Structure in a Compressor Cascade	5
Multidisciplinary Optimization of a Mixed-Flow Impeller With 140 Parameters and Its Shapley Additive Explanations	5
Modeling of Combustor Non-Uniformities Evolution Through a High-Pressure Turbine Stage	5
Considerations for Compressible Film Cooling: A Computational Study of the Effects of Transonic Flows and Varying Mainstream Mach Number	5
Interaction Mechanism of Transonic Squealer Tip Cooling With the Effect of High-Speed Relative Casing Motion	5
Effective Clearance and Differential Gapping Impact on Seal Flutter Modeling and Validation	5
Development of Compact and Hermetic Organic Rankine Cycle Turbine Generator With Upgraded Cooling Capability	5
Scale-Resolving Simulations of Turbulent Flow Retaining the Exact Blade Count With the Time-Inclined Method	5
Effects on Film Cooling Performance in the Showerhead From Geometric Parameterization of Shaped Hole Designs	5
Impact of the Purge Flow Density Ratio on the Rim Sealing Effectiveness in Hot Gas Ingestion Measurements	5
Adaptation of von Karman Institute for Fluid Dynamics’ Isentropic Compression Tube Facility for High-Speed Low-Pressure Turbines Testing	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
The Influence of Boundary Layer State and Trailing Edge Wedge Angle on the Aerodynamic Performance of Transonic Turbine Blades	5
Turbulence Measurements at the Inlet of an Automotive Turbocharger Compressor Using Stereoscopic Particle Image Velocimetry	5
Convergence Acceleration of Favre-Averaged Non-Linear Harmonic Method	5
High-Fidelity Computational Assessment of Aero-Thermal Performance and the Reynolds’ Analogy for Additively Manufactured Anisotropic Surface Roughness	5