Journal of Turbomachinery-Transactions of the Asme

Article	Citations
Experimental Study on the High Relative Casing Motion Effect on Turbine Blade Tip Aerodynamic Characteristics	56
Corner Separation Control Using Sweeping Jet Actuator in a Compressor Cascade	38
Effect of the Key Geometry and Flow Parameters on Discharge Coefficient of Laidback Fan-Shaped Hole Under Coolant Crossflow Condition	34
Effects of Radially Variable Sweep Vanes on Rotor–Stator Interaction Noise	32
Rotating Instabilities in Shrouded Low Pressure Turbine at Design and Off-Design Conditions	28
Turbine Vane Passage Cooling Experiments With a Close-Coupled Combustor-Turbine Interface Geometry—Part I: Describing the Flow	27
Three-Dimensional Unsteady Aerodynamic Optimization of a Transonic Compressor Stage Using an Implicit Discrete Adjoint Harmonic Balance Method	22
Evaluation of Cooling Requirements for Rotating Detonation Combustors	21
Performance Sensitivity of a Grooved Tip Seal to Manufacturing and Operational Geometry Deviations	21
An Exception Algorithm to Ease Convergence in Multistage Turbomachinery Throughflow Calculations	21
An Improved Particle Impact Model by Accounting for Rate of Strain and Stochastic Rebound	20
Effect of Leading Edge Erosion on the Tip Leakage Flow in a Compressor Cascade	19
On the Use of Pressure-Sensitive Paint to Determine the Rim Sealing Effectiveness	19
Analysis of the Bifurcating Duct of an Inlet Particle Separator in Transonic Flow Conditions	18
Nonlinear Flutter Analysis of Labyrinth Seals	18
Reviewer’s Recognition	18
Physics-Guided Graph Neural Networks: Numerical Investigation of High-Pressure Turbine Flow	17
The Effects of Swirling Flows in Entropy Wave Convection Through High-Pressure Turbine Stage	17
Effects of Blade Solidity and Aspect Ratio on a 0.5 Hub-to-Tip Ratio Tube-Axial Fan	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	16
Unsteady Pre-Stall Behavior in a Centrifugal Compressor With Vaned Diffuser	16
Numerical Study on the Effect of Back Cavity on the Aerodynamic Behavior of a Non-Axisymmetric Casing Treatment for Transonic Axial Compressors	15
Aerodynamic Effect of Shallow Circumferential Grooves in the Shroud of a Centrifugal Compressor	15
Prediction of Steady and Unsteady Flow Quantities Using Multiscale Graph Neural Networks	15

A Framework for Estimating Effects of Combustor Turbulence on Turbine Profile Loss Generation	14
Film Cooling on Turbine Vane Endwalls With Different Inlet Cooling Configurations: Experimental and Computational Results	14
A New Multi-Stage Turbine Stator Design for Improved Performance Retention	14
Wind Tunnel Continuous-Scan Acoustic Analysis of Ducted Fan Tones Interacting With a Shielding Wall	13
Introduction of Axisymmetric Grooves as a Tip Seal Treatment for Small-Core Turbines	13
Development of a Novel Pressure-Based Approach for Blade Synchronous Vibration Detection Including Mistuning	13
A Method for Preliminary Design of Variable Geometry Vaned Diffuser for Centrifugal Compressor	12
IMPACT OF NOZZLE GUIDE VANE TRAILING EDGE DAMAGE ON HIGH PRESSURE TURBINE STAGE PERFORMANCE	12
Modeling and Simulation of Sand Particle Trajectories and Erosion in a Transonic Fan Stage	12
Measurements of Turbulence in Compressible Low-Density Flows at the Inlet of a Transonic Linear Cascade With and Without Unsteady Wakes	12
A Multi-Scale Representation of Turbulence Generation in Compressor Flows	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
Acoustic Modes in an Open Box Cavity With Variable Depth Using Two Distinct Wind Tunnels	11
Effect of Axial Throughflow Swirl on Flow and Heat Transfer in a Compressor Disc Cavity	11
Heat Transfer Measurements in a Turbine Centre Frame at Realistic Mach Number - Part 2: Influence of Combustor Hot Streaks	11
A Study of Loss Model Parameter Sensitivity in Compressor Unsteady Flow Simulations	11
Pragmatic Prediction Model of Droplet Trajectory in a Turbine Cascade	11
Systematic Numerical Investigation on the Surface Roughness Effects on the Friction and Heat Transfer of Additively Manufactured Components	11
The Cooling Effect of Combustor Exit Louver Scheme on a Transonic Nozzle Guide Vane Endwall	11
NUMERICAL DESIGN OF EXPERIMENTS FOR REPEATING LOW-PRESSURE TURBINE STAGES PART I: COMPUTATIONAL OPPORTUNITIES AND METHODOLOGY	11
Loss Analysis of Cavity Leakage Flow in a Compressor 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
Aerothermal Performance Robustness and Reliability Analysis of Turbine Blade Squealer Tip With Film Cooling	10
Unpacking Intermineral Synergies and Reactions During Dust Deposition in an Impingement Coolant Jet	10
Fundamentals of Scaling of Overall Cooling Effectiveness With Temperature Ratio	10
Entry Region Heat Transfer Augmentation With Pins, Fins, and Turbulators in Circular Channels	10
Multistage Turbomachinery Optimization for High-Temperature Heat Pumps With the Reverse Rankine Cycle	10
Experimental Investigation of Additional Loss Associated With Incoming Wakes in Low-Pressure Turbine Cascades	10
On the Over-Prediction of Centrifugal Compressor Pressure Ratio in the High Impeller Tip Mach Number Regime	10
Correlated Pressure–Velocity Instability in a Transonic High-Pressure Turbine Blade	10
The Influence of Turbulence and Reynolds Number on Endwall Heat Transfer in a Vane Cascade	9
An Experimental Investigation of Sweeping Mist Jet Film Cooling With Droplet Analysis	9
Heat Transfer Analysis in a Turbine Bottom Platform Cavity With Hot Gas Ingestion: An Investigation on the Applicability of the Superposition Approach	9
Flow and Heat Transfer in a Rotating Disc Cavity With Axial Throughflow at High-Speed Conditions	9
Unsteady Aerodynamic Forcing Due to Distortion in a Boundary Layer Ingesting Fan	9
An Improved Passage-Flow Turning Model for Forward-Curved Blades of Squirrel-Cage Fan	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
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
Effects of Downstream Vortex Generators on Film Cooling a Flat Plate Fed by Crossflow	9
Analysis of Complex Total Pressure Distortion Screens Using One-Dimensional Loss Data	9
Numerical Assessment of an Aerodynamic Probe to Enable Short Focal Length Laser Diagnostics in High Temperature Supersonic Flows Based on Flow Disturbance	9
Numerical Study on Unsteady Flow of a Supersonic Partial Admission Impulse Turbine	9
Insights Into Turbocharger Centrifugal Compressor Stability Using High-Fidelity Computational Fluid Dynamics and a Novel Impeller Diffusion Factor	9
Numerical Modeling and Design Challenges of Boundary Layer Ingesting Fans	9
Modeling Deposition in Gas Turbines With Conjugate Mesh-Morphing and Temperature Sensitivity	9
Effect of Purge–Mainstream Density Ratio on the Secondary Flow Field of a Turbine Blade Row	9
Experimental Study on Controlling Flow Separation of Compressor Cascades With Self-Excited Sweeping Jet Actuator	9

Unsteady Flow Structure of Corner Separation in a Highly Loaded Compressor Cascade	9
Windage Torque Reduction in Low-Pressure Turbine Cavities Part II: Experimental and Numerical Results	9
Comparative Investigation of HPT Blade Cooling Concepts in an Aerothermal Test Rig	9
Impact of High-Pressure-Turbine Purge Flow on the Evolution of Turbulence in a Turbine Vane Frame	9
A Free Streamline Model for Fully Separated Turbomachine Flows	8
ANALYSIS OF AEROACOUSTIC PHENOMENA IN CENTRIFUGAL COMPRESSORS USING A LATTICE BOLTZMANN FLOW SIMULATION APPROACH	8
Response of Separated Boundary Layers to Steady and Pulsated Flow Injection	8
RANS Capabilities for Transonic Axial Compressor: A Perspective From GPPS Computational Fluid Dynamics Workshop	8
Strategies for High-Accuracy Measurements of Stage Efficiency for a Cooled Turbine	8
Numerical Investigation on the Influence of Wet Compression Aerodynamic Performance of Multi-Stage Transonic Compressor	8
Noise Source Identification for the Unsteady Low-Pressure Turbine Flow Fields	8
Sensitivity Analysis for Flow Stability of Axial Compressor Based on Meridional Flow	8
Compressor Stator Leading Edge Instrumentation	8
A Three-Dimensional Actuator Disk Model for Fan Response to Inlet Distortion: Part I - Formulation	8
Dirt Ingestion Impacts on Cooling Within a Double-Walled Combustor Liner	8
The Application of Fluidic Sealing in Shrouded Gas Turbine Blades	8
Investigation of Tip Leakage Vortex Breakdown in a High-Speed Multistage Axial Compressor	8
Film Superposition Characteristics With Laidback Fan-Shaped Holes Under the Influence of Internal Crossflow	8
A Review of Secondary Combustion on the Turbine Blade Cooling	8
Advanced Design of a Transition Duct for Supersonic Inlet Turbines in Rotating Detonation Engines	8
Heat Transfer in an Injector-Scaled Additively Manufactured Fuel Passage	8
Effect of Upstream Leakage Flow on Film Cooling Characteristic of a Turbine Convex Endwall	8
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	8
Dissipation in Skewed Boundary Layers	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
Revisiting Dimensionless Parameters Quantifying Film Cooling	8
The Design of Aspirated Stators for Compressor Bleed	8
High-Fidelity Investigation of Vortex Shedding From a Highly Loaded Turbine Blade	8
Numerical Study of Crossflow Effects on Discharge Coefficient of the Converging Slot Hole	8
Unsteadiness in the Secondary Flows of a High-Speed Low-Pressure Turbine Cascade With Unsteady Wakes and Purge Flow	8
Characterizing Flow Instabilities During Transient Events in the Turbine Rim Seal Cavity	8
Investigation of the Map Width Improvement in a Radially Reduced Diffuser Design Concept for a Centrifugal Compressor	8
Experimental and Numerical Investigation of High Load Turbine Blade Tip Cavity Structures	7
Multiscale Data-Driven RANS Closure for Trailing Edge Cutback Film Cooling Flows	7
UHBR Open-Test Case Fan ECL5/CATANA: Non-Linear Analysis of Non-Synchronous Blade Vibration at Part-Speed Conditions	7
Optimal Riblets Applied to Gas Turbine Compressor Blades Studied via Direct Numerical Simulation (GT2024–122305)	7
Data Assimilation of Transitional and Separated Turbomachinery Flows With Physics-Informed Neural Networks	7
Impact of Low Freestream Turbulence and Surface Roughness on the Flat-Plate Boundary Layer Transition Under a High-Lift Airfoil Pressure Gradient	7
Reducing Low-Pressure Turbine Shroud Leakage Loss by Optimizing Leakage-Mainstream Interaction	7
Impacts of Material and Machine on the Variation of Additively Manufactured Cooling Channels	7
The Effect of Inlet Conditions on Turbine Endwall Loss	7
Predicting Endwall Corner Separation in Compressor Cascades Using RANS: Influence of Transition Treatment and Inflow Conditions	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
Plume Model for Buoyancy-Induced Flow and Heat Transfer in Closed Rotating Cavities	7
Robustness Analysis on Aerothermal Performance of the Winglet Squealer Tip—Part 1: Aerodynamic Performance	7
Adaptation of von Karman Institute for Fluid Dynamics’ Isentropic Compression Tube Facility for High-Speed Low-Pressure Turbines Testing	7
Particle Bounce Stick Behavior in the Rotating Frame of Reference	7
Magnetic Resonance Velocimetry of a Turbine Blade With Engine-Representative Internal and Film Cooling Structures	7
GPU-Accelerated Full-Wheel Large-Eddy Simulations of a Transonic Fan Stage	7
Influences of Particulate Deposition on Vane Trailing-Edge Film Cooling: Adiabatic and Overall Cooling Effectiveness	7
Viability of Fiber Optic Temperature Sensors Embedded Within Engine-Scale Turbine Blades	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
Transient Temperature Field Inversion of Turbine Based on Physics-Encoded Neural Networks	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 Research Into Aeroelastic Phenomena in Turbine Rotor Blades Inside ARIAS EU Project	6
Experimental Assessment of Squealer Tip Leakage Flow Structures in a Small-Core High-Speed Turbine	6
A New Nonlinear Time-Domain Flutter Analysis Approach for Distorted Flows	6
The Influence of Combustor Hot Streaks on the Aerodynamic Performance of a Turbine Center Frame	6
Surge Inception Point Analysis Using the Greitzer Model for Centrifugal Compressor	6
A Physics-Informed Neural Network for Solving the Inverse Heat Transfer Problem in Gas Turbine Rotating Cavities	6
A Test Facility for the Experimental Investigation of Labyrinth Seal Flutter and Early-Stage Validation of Prediction Techniques	6
High-Fidelity Computational Assessment of Aero-Thermal Performance and the Reynolds’ Analogy for Additively Manufactured Anisotropic Surface Roughness	6
THE RELATIVE EFFECTS OF INTERNAL REYNOLDS NUMBER AND ADVECTIVE CAPACITY RATIO ON THE COOLANT WARMING FACTOR	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
Wake–Separation Bubble Interaction Over an Experimentally Simulated Axial Compressor Blade Under Low Reynolds Number Flow	6
Investigating the Influence of Mainstream Turbulence and Large Vortices on Gas Turbine Trenched Film Cooling Flows Using Planar Temperature-Velocity Imaging	6
Effect of Solidity and Aspect Ratio on the Aerodynamic Performance of Axial-Flow Fans With 0.2 Hub-to-Tip Ratio	6
Aft Fuselage Boundary Layer Ingesting Propulsion System Design	6
Impact of Fan Aerodynamics on Inlet Distortion at Crosswind	6
Multidisciplinary Optimization of a Mixed-Flow Impeller With 140 Parameters and Its Shapley Additive Explanations	6
Blade Vibration Analysis for Radial Turbine Featuring a Multi-Channel Casing Design	6
The Influence of Boundary Layer State and Trailing Edge Wedge Angle on the Aerodynamic Performance of Transonic Turbine Blades	6
Inverse Design of Compressor/Fan Blade Profiles Based on Conditional Invertible Neural Networks	6
Low Reynolds Number Effects on the Endwall Flow Field in a High-Lift Turbine Passage	6
Loss Analysis in Radial Inflow Turbines for Supercritical CO2 Mixtures	6
Experimental Investigation of Mode-Frequency Scattering at Fan Stages	6
Collaborative Robust Design Optimization of Blade Geometry and Manufacturing Tolerance for a Transonic Centrifugal Impeller	6
Highly Time Resolved, Combined Temperature, and Heat Flux Measurement Technique Based on ALTP Sensors	6

A Shock Loss Reduction Method Using a Concave Suction Side Profile for a Zero Inlet Swirl Turbine Rotor	6
Equation-Oriented Meanline Method for Axial Turbine Performance Prediction Under Choking Conditions	6
On the Mechanism of Unsteady Tip Flow Occurrence in a Transonic Fan	6
Development of Compact and Hermetic Organic Rankine Cycle Turbine Generator With Upgraded Cooling Capability	6
Innovative Cavity Modeling for Centrifugal Compressors Aeromechanical Analysis	6
Numerical Analysis of Sealing Flows in Gas Turbines Using RANS and Large Eddy Simulation Approaches	6
Investigation on Heat Transfer Distribution of Rotating Two-Pass Smooth and Ribbed Channels Under Aero-Engine Simulated Conditions	5
Validation of Filtered Rayleigh Scattering Optical Rake Measurement Techniques in Turbomachinery Applications and Boundary Layers	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
Quasi-Dynamic Approximation of Unsteady Pressure Distribution for Transonic Airfoils in Flutter	5
The Impact of Manufacturing Variations on the Aerothermal Performance of High-Pressure Turbine Blade Shrouds	5
Mitigation of Boundary Layer Ingestion Circumferential Distortion Using Nonaxisymmetric Fan Exit Guide Vanes	5
Modeling of Combustor Non-Uniformities Evolution Through a High-Pressure Turbine Stage	5
Impact of the Purge Flow Density Ratio on the Rim Sealing Effectiveness in Hot Gas Ingestion Measurements	5
Wall-Modeled Large-Eddy Simulation of a Transonic Gas Turbine Vane—Part II: Mach Number Effect and Losses Prediction	5
Unsteady Investigation of Intermediate Turbine Ducts Under the Influence of Purge Flows	5
Impact of Blowing and Density Ratio on the Film Cooling and Heat Transfer in an Aggressive Turbine Center Frame	5
Cavity Impact on the Base Flow Unsteadiness for a High-Speed Exhaust System	5
High-Dimensional Uncertainty Quantification of High-Pressure Turbine Vane Based on Multifidelity Deep Neural Networks	5
Computational and Experimental Study of Film-Cooling Effectiveness With and Without Downstream Vortex Generators	5
The Effect of Reaction on Compressor Performance	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
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
Characterizing the Unsteady Flow Field in Low-Flow Turbine Operation	5
Pressure Characteristic Rollover of a Transonic Centrifugal Impeller	5
Heat Transfer and Flow Field Characteristics of Variable Aspect Ratio, Serpentine Passages	5
Large Eddy Simulation of Laminar and Turbulent Shock/Boundary Layer Interactions in a Transonic Passage	5
Scale-Resolving Simulations of Turbulent Flow Retaining the Exact Blade Count With the Time-Inclined Method	5
A Resistive Model to Characterize Overall Effectiveness Influenced by Multiple Coolant Temperatures	5
Turbine Nozzle Guide Vane Endwall Film Cooling and Vane Phantom Cooling Performances at Various Blocked Film Hole Configurations	5
Data-Driven Radial Compressor Design Space Mapping	5
Boundary Layer Analysis of a Transonic High-Pressure Turbine Vane Using Ultra-Fast-Response Temperature-Sensitive Paint	5
Experimental Investigation of Flame-Film Cooling Interactions With an Academic Test Rig and Optical Laser Diagnostics	5
Unsteady Loss Mechanisms in Low-Pressure Turbines With Diverging End-Walls Studied Via High-Fidelity Simulation	5
The Impact of Multiscale Ceramic Matrix Composite Roughness on Heat Transfer and Boundary Layer Behavior	5
Experimental Study of Impact of In-Service Deterioration on Thermal Performance of High-Pressure Nozzle Guide Vanes	5
An Active Turbulence Grid for Turbomachinery Flow Experiments	5
Numerical Investigation of the Effect of Trailing Edge Thickness of Simulated Ceramic Matrix Composite Blades on Loss Profiles	5
A New Axial Compressor Test Facility for the Investigation of Aerodynamic Damping Featuring an Electromagnetic Excitation System	5
Improvements in the Prediction of Steady and Unsteady Transition and Mixing in Low-Pressure Turbines by Means of Machine-Learnt Closures	5
On Intake–Compressor Interactions Within an Integrated Propulsion System	5
Convergence Acceleration of Favre-Averaged Non-Linear Harmonic Method	5
Annular Dump Diffuser and Deswirl System for Back-Pressure Control in Engine-Scale Transonic Annular Cascade	5
The Effect of Upstream Unsteadiness on the Unstarting of a Supersonic Inlet Turbine	5
On the Secondary Flow System of an Aggressive Inter Compressor Duct	5
The Unsteady Topology of Corner Separations	5