Journal of Turbomachinery-Transactions of the Asme

Article	Citations
Rotating Instabilities in Shrouded Low Pressure Turbine at Design and Off-Design Conditions	59
Turbine Vane Passage Cooling Experiments With a Close-Coupled Combustor-Turbine Interface Geometry—Part I: Describing the Flow	43
Performance Sensitivity of a Grooved Tip Seal to Manufacturing and Operational Geometry Deviations	37
Three-Dimensional Unsteady Aerodynamic Optimization of a Transonic Compressor Stage Using an Implicit Discrete Adjoint Harmonic Balance Method	34
On the Use of Pressure-Sensitive Paint to Determine the Rim Sealing Effectiveness	30
Evaluation of Cooling Requirements for Rotating Detonation Combustors	29
An Improved Particle Impact Model by Accounting for Rate of Strain and Stochastic Rebound	28
Effect of Leading Edge Erosion on the Tip Leakage Flow in a Compressor Cascade	26
Corner Separation Control Using Sweeping Jet Actuator in a Compressor Cascade	24
Experimental Study on the High Relative Casing Motion Effect on Turbine Blade Tip Aerodynamic Characteristics	23
Effects of Radially Variable Sweep Vanes on Rotor–Stator Interaction Noise	23
Reviewer’s Recognition	21
Analysis of the Bifurcating Duct of an Inlet Particle Separator in Transonic Flow Conditions	21
Effect of the Key Geometry and Flow Parameters on Discharge Coefficient of Laidback Fan-Shaped Hole Under Coolant Crossflow Condition	21
Nonlinear Flutter Analysis of Labyrinth Seals	21
An Exception Algorithm to Ease Convergence in Multistage Turbomachinery Throughflow Calculations	21
A Method for Preliminary Design of Variable Geometry Vaned Diffuser for Centrifugal Compressor	20
The Effects of Swirling Flows in Entropy Wave Convection Through High-Pressure Turbine Stage	20
Effects of Blade Solidity and Aspect Ratio on a 0.5 Hub-to-Tip Ratio Tube-Axial Fan	20
A Framework for Estimating Effects of Combustor Turbulence on Turbine Profile Loss Generation	17
Wind Tunnel Continuous-Scan Acoustic Analysis of Ducted Fan Tones Interacting With a Shielding Wall	17
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	17
Modeling and Simulation of Sand Particle Trajectories and Erosion in a Transonic Fan Stage	16
A New Multi-Stage Turbine Stator Design for Improved Performance Retention	16
Film Cooling on Turbine Vane Endwalls With Different Inlet Cooling Configurations: Experimental and Computational Results	16

Introduction of Axisymmetric Grooves as a Tip Seal Treatment for Small-Core Turbines	15
Unsteady Pre-Stall Behavior in a Centrifugal Compressor With Vaned Diffuser	15
Physics-Guided Graph Neural Networks: Numerical Investigation of High-Pressure Turbine Flow	15
Measurements of Turbulence in Compressible Low-Density Flows at the Inlet of a Transonic Linear Cascade With and Without Unsteady Wakes	14
Development of a Novel Pressure-Based Approach for Blade Synchronous Vibration Detection Including Mistuning	14
Fan Non-Synchronous Forced Vibration Under Crosswind	14
Numerical Study on the Effect of Back Cavity on the Aerodynamic Behavior of a Non-Axisymmetric Casing Treatment for Transonic Axial Compressors	14
Prediction of Steady and Unsteady Flow Quantities Using Multiscale Graph Neural Networks	14
NUMERICAL DESIGN OF EXPERIMENTS FOR REPEATING LOW-PRESSURE TURBINE STAGES PART I: COMPUTATIONAL OPPORTUNITIES AND METHODOLOGY	13
A Multi-Scale Representation of Turbulence Generation in Compressor Flows	13
Aerodynamic Effect of Shallow Circumferential Grooves in the Shroud of a Centrifugal Compressor	13
Unique High-Resolution Temperature Mapping of Stage 1 Turbine Vane in a Long-Term Engine Test	13
Pragmatic Prediction Model of Droplet Trajectory in a Turbine Cascade	13
Impact of Nozzle Guide Vane Trailing Edge Damage on High-Pressure Turbine Stage Performance	13
Heat Transfer Measurements in a Turbine Centre Frame at Realistic Mach Number - Part 2: Influence of Combustor Hot Streaks	12
Tail-Integrated Boundary Layer Ingesting Propulsion Systems for Turbo-Electric Aircraft	12
Loss Analysis of Cavity Leakage Flow in a Compressor Cascade	12
Analytical Study on the Influence of Stage-Wise Distribution of Parameters on the Performance of a Multistage Axial Compressor	12
Fundamentals of Scaling of Overall Cooling Effectiveness With Temperature Ratio	12
A Study of Loss Model Parameter Sensitivity in Compressor Unsteady Flow Simulations	12
Spectral Heat Transfer Coefficient for Thermal Design Analysis—Part 1: Augmenting the Cooling Law for Non-Isothermal Wall	12
The Cooling Effect of Combustor Exit Louver Scheme on a Transonic Nozzle Guide Vane Endwall	12
Systematic Numerical Investigation on the Surface Roughness Effects on the Friction and Heat Transfer of Additively Manufactured Components	12
Acoustic Modes in an Open Box Cavity With Variable Depth Using Two Distinct Wind Tunnels	11
Entry Region Heat Transfer Augmentation With Pins, Fins, and Turbulators in Circular Channels	11
Particle Image Velocimetry in a High-Speed Short-Duration Turbine Rig	11
Unsteady Aerodynamic Forcing Due to Distortion in a Boundary Layer Ingesting Fan	11
Effect of Axial Throughflow Swirl on Flow and Heat Transfer in a Compressor Disc Cavity	11
Correlated Pressure–Velocity Instability in a Transonic High-Pressure Turbine Blade	11
Numerical Modeling and Design Challenges of Boundary Layer Ingesting Fans	11
The Influence of Turbulence and Reynolds Number on Endwall Heat Transfer in a Vane Cascade	11
Experimental Investigation of Additional Loss Associated With Incoming Wakes in Low-Pressure Turbine Cascades	11
Unpacking Intermineral Synergies and Reactions During Dust Deposition in an Impingement Coolant Jet	11
Effects of Downstream Vortex Generators on Film Cooling a Flat Plate Fed by Crossflow	11
On the Over-Prediction of Centrifugal Compressor Pressure Ratio in the High Impeller Tip Mach Number Regime	10
An Experimental Investigation of Sweeping Mist Jet Film Cooling With Droplet Analysis	10
Aerothermal Performance Robustness and Reliability Analysis of Turbine Blade Squealer Tip With Film Cooling	10
Effect of Purge–Mainstream Density Ratio on the Secondary Flow Field of a Turbine Blade Row	10
Mechanisms of Loss Surge and Evolution in a Highly Loaded Transonic Turbine Nozzle Guide Vane: A Novel Loss Decomposition Method via Micro-Streamtube Energy Analysis	10
Efficient Quantification of Structural Uncertainty in RANS Simulations of a Transonic Axial Compressor using Anisotropic Perturbations	10
Analysis of Complex Total Pressure Distortion Screens Using One-Dimensional Loss Data	10
Experimental Study on Controlling Flow Separation of Compressor Cascades With Self-Excited Sweeping Jet Actuator	10
Performance and Secondary Flow Structures Characterization in a Highly Loaded Low-Pressure Compressor Under Distorted Inflow Conditions	10
Multistage Turbomachinery Optimization for High-Temperature Heat Pumps With the Reverse Rankine Cycle	10
Flow and Heat Transfer in a Rotating Disc Cavity With Axial Throughflow at High-Speed Conditions	10
Unsteady Flow Structure of Corner Separation in a Highly Loaded Compressor Cascade	10
Boundary Layer Transition Induced By Surface Roughness Distributed Over a Low-Pressure Turbine Blade	10
Heat Transfer Analysis in a Turbine Bottom Platform Cavity With Hot Gas Ingestion: An Investigation on the Applicability of the Superposition Approach	10
Modeling Deposition in Gas Turbines With Conjugate Mesh-Morphing and Temperature Sensitivity	10
Numerical Study on Unsteady Flow of a Supersonic Partial Admission Impulse Turbine	9

Advanced Design of a Transition Duct for Supersonic Inlet Turbines in Rotating Detonation Engines	9
Strategies for High-Accuracy Measurements of Stage Efficiency for a Cooled Turbine	9
Film Superposition Characteristics With Laidback Fan-Shaped Holes Under the Influence of Internal Crossflow	9
Revisiting Dimensionless Parameters Quantifying Film Cooling	9
Comparative Investigation of HPT Blade Cooling Concepts in an Aerothermal Test Rig	9
Effect of Upstream Leakage Flow on Film Cooling Characteristic of a Turbine Convex Endwall	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
Impact of High-Pressure-Turbine Purge Flow on the Evolution of Turbulence in a Turbine Vane Frame	9
ANALYSIS OF AEROACOUSTIC PHENOMENA IN CENTRIFUGAL COMPRESSORS USING A LATTICE BOLTZMANN FLOW SIMULATION APPROACH	9
Noise Source Identification for the Unsteady Low-Pressure Turbine Flow Fields	9
Compressor Stator Leading Edge Instrumentation	9
A Review of Secondary Combustion on the Turbine Blade Cooling	9
Windage Torque Reduction in Low-Pressure Turbine Cavities Part II: Experimental and Numerical Results	9
Numerical Study of Crossflow Effects on Discharge Coefficient of the Converging Slot Hole	9
High-Fidelity Investigation of Vortex Shedding From a Highly Loaded Turbine Blade	9
Insights Into Turbocharger Centrifugal Compressor Stability Using High-Fidelity Computational Fluid Dynamics and a Novel Impeller Diffusion Factor	9
Investigation of Tip Leakage Vortex Breakdown in a High-Speed Multistage Axial Compressor	9
Sensitivity Analysis for Flow Stability of Axial Compressor Based on Meridional Flow	9
Numerical Assessment of an Aerodynamic Probe to Enable Short Focal Length Laser Diagnostics in High Temperature Supersonic Flows Based on Flow Disturbance	9
Dissipation in Skewed Boundary Layers	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
An Improved Passage-Flow Turning Model for Forward-Curved Blades of Squirrel-Cage Fan	9
Numerical Investigation on the Influence of Wet Compression Aerodynamic Performance of Multi-Stage Transonic Compressor	9
The Design of Aspirated Stators for Compressor Bleed	8
Unsteadiness in the Secondary Flows of a High-Speed Low-Pressure Turbine Cascade With Unsteady Wakes and Purge Flow	8
Impacts of Material and Machine on the Variation of Additively Manufactured Cooling Channels	8
Magnetic Resonance Velocimetry of a Turbine Blade With Engine-Representative Internal and Film Cooling Structures	8
Reducing Low-Pressure Turbine Shroud Leakage Loss by Optimizing Leakage-Mainstream Interaction	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
Experimental and Numerical Investigation of High Load Turbine Blade Tip Cavity Structures	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
Investigation of the Map Width Improvement in a Radially Reduced Diffuser Design Concept for a Centrifugal Compressor	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
Influences of Particulate Deposition on Vane Trailing-Edge Film Cooling: Adiabatic and Overall Cooling Effectiveness	8
Multiscale Data-Driven RANS Closure for Trailing Edge Cutback Film Cooling Flows	8
Robustness Analysis on Aerothermal Performance of the Winglet Squealer Tip—Part 1: Aerodynamic Performance	8
Heat Transfer in an Injector-Scaled Additively Manufactured Fuel Passage	8
The Application of Fluidic Sealing in Shrouded Gas Turbine Blades	8
Response of Separated Boundary Layers to Steady and Pulsated Flow Injection	8
A Free Streamline Model for Fully Separated Turbomachine Flows	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
Optimal Riblets Applied to Gas Turbine Compressor Blades Studied via Direct Numerical Simulation (GT2024–122305)	8
Predicting Endwall Corner Separation in Compressor Cascades Using RANS: Influence of Transition Treatment and Inflow Conditions	8
Characterizing Flow Instabilities During Transient Events in the Turbine Rim Seal Cavity	8
Particle Bounce Stick Behavior in the Rotating Frame of Reference	8
UHBR Open-Test Case Fan ECL5/CATANA: Non-Linear Analysis of Non-Synchronous Blade Vibration at Part-Speed Conditions	8
Blade Vibration Analysis for Radial Turbine Featuring a Multi-Channel Casing Design	7
Impact of Low Freestream Turbulence and Surface Roughness on the Flat-Plate Boundary Layer Transition Under a High-Lift Airfoil Pressure Gradient	7
Highly Time Resolved, Combined Temperature, and Heat Flux Measurement Technique Based on ALTP Sensors	7
Data Assimilation of Transitional and Separated Turbomachinery Flows With Physics-Informed Neural Networks	7
A New Nonlinear Time-Domain Flutter Analysis Approach for Distorted Flows	7
Aft Fuselage Boundary Layer Ingesting Propulsion System Design	7
Plume Model for Buoyancy-Induced Flow and Heat Transfer in Closed Rotating Cavities	7
Multidisciplinary Optimization of a Mixed-Flow Impeller With 140 Parameters and Its Shapley Additive Explanations	7
The Influence of Combustor Hot Streaks on the Aerodynamic Performance of a Turbine Center Frame	7
Manufacturing a Ceramic Turbine Rotor for a Compact Jet Engine	7
Effects of Ribbed Surfaces on Profile Losses of Low-Pressure Turbine Blades	7
Equation-Oriented Meanline Method for Axial Turbine Performance Prediction Under Choking Conditions	7
Viability of Fiber Optic Temperature Sensors Embedded Within Engine-Scale Turbine Blades	7
Impact of Fan Aerodynamics on Inlet Distortion at Crosswind	7
A Physics-Informed Neural Network for Solving the Inverse Heat Transfer Problem in Gas Turbine Rotating Cavities	7
Effect of Solidity and Aspect Ratio on the Aerodynamic Performance of Axial-Flow Fans With 0.2 Hub-to-Tip Ratio	7
A Shock Loss Reduction Method Using a Concave Suction Side Profile for a Zero Inlet Swirl Turbine Rotor	7
Adaptation of von Karman Institute for Fluid Dynamics’ Isentropic Compression Tube Facility for High-Speed Low-Pressure Turbines Testing	7
On the Mechanism of Unsteady Tip Flow Occurrence in a Transonic Fan	7
Experimental Research Into Aeroelastic Phenomena in Turbine Rotor Blades Inside ARIAS EU Project	7
Surge Inception Point Analysis Using the Greitzer Model for Centrifugal Compressor	7
Collaborative Robust Design Optimization of Blade Geometry and Manufacturing Tolerance for a Transonic Centrifugal Impeller	7
Convergence Acceleration of Favre-Averaged Non-Linear Harmonic Method	6
Numerical Investigation of the Effect of Trailing Edge Thickness of Simulated Ceramic Matrix Composite Blades on Loss Profiles	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
Transient Temperature Field Inversion of Turbine Based on Physics-Encoded Neural Networks	6
Large Eddy Simulation of Laminar and Turbulent Shock/Boundary Layer Interactions in a Transonic Passage	6
Investigation on Heat Transfer Distribution of Rotating Two-Pass Smooth and Ribbed Channels Under Aero-Engine Simulated Conditions	6
Validation of Filtered Rayleigh Scattering Optical Rake Measurement Techniques in Turbomachinery Applications and Boundary Layers	6
A Test Facility for the Experimental Investigation of Labyrinth Seal Flutter and Early-Stage Validation of Prediction Techniques	6
High-Dimensional Uncertainty Quantification of High-Pressure Turbine Vane Based on Multifidelity Deep Neural Networks	6

Pressure Characteristic Rollover of a Transonic Centrifugal Impeller	6
Computational and Experimental Study of Film-Cooling Effectiveness With and Without Downstream Vortex Generators	6
Wake–Separation Bubble Interaction Over an Experimentally Simulated Axial Compressor Blade Under Low Reynolds Number Flow	6
Interaction Mechanism of Transonic Squealer Tip Cooling With the Effect of High-Speed Relative Casing Motion	6
Numerical Analysis of Sealing Flows in Gas Turbines Using RANS and Large Eddy Simulation Approaches	6
Wall-Modeled Large-Eddy Simulation of a Transonic Gas Turbine Vane—Part II: Mach Number Effect and Losses Prediction	6
Experimental Investigation of Mode-Frequency Scattering at Fan Stages	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
Improvements in the Prediction of Steady and Unsteady Transition and Mixing in Low-Pressure Turbines by Means of Machine-Learnt Closures	6
On the Secondary Flow System of an Aggressive Inter Compressor Duct	6
Quasi-Dynamic Approximation of Unsteady Pressure Distribution for Transonic Airfoils in Flutter	6
Inverse Design of Compressor/Fan Blade Profiles Based on Conditional Invertible Neural Networks	6
A Digital Engineering Analysis of an Additively-Manufactured Turbine Vane	6
High-Fidelity Computational Assessment of Aero-Thermal Performance and the Reynolds’ Analogy for Additively Manufactured Anisotropic Surface Roughness	6
Mitigation of Boundary Layer Ingestion Circumferential Distortion Using Nonaxisymmetric Fan Exit Guide Vanes	6
Annular Dump Diffuser and Deswirl System for Back-Pressure Control in Engine-Scale Transonic Annular Cascade	6
The Impact of Manufacturing Variations on the Aerothermal Performance of High-Pressure Turbine Blade Shrouds	6
Development of Compact and Hermetic Organic Rankine Cycle Turbine Generator With Upgraded Cooling Capability	6
Turbine Nozzle Guide Vane Endwall Film Cooling and Vane Phantom Cooling Performances at Various Blocked Film Hole Configurations	6
Heat Transfer and Flow Field Characteristics of Variable Aspect Ratio, Serpentine Passages	6
Loss Analysis in Radial Inflow Turbines for Supercritical CO2 Mixtures	6
Experimental Assessment of Squealer Tip Leakage Flow Structures in a Small-Core High-Speed Turbine	6
Impact of the Purge Flow Density Ratio on the Rim Sealing Effectiveness in Hot Gas Ingestion Measurements	6
Modeling of Combustor Non-Uniformities Evolution Through a High-Pressure Turbine Stage	6
Impact of freestream turbulence on the aerodynamics of a high-speed, low-Reynolds turbine rotor cascade usingWall-Resolved Large Eddy Simulations	6
Considerations for Compressible Film Cooling: A Computational Study of the Effects of Transonic Flows and Varying Mainstream Mach Number	6
Efficient Aerodynamic Uncertainty Quantification for a Three-Dimensional Transonic Fan Rotor	6
Boundary Layer Analysis of a Transonic High-Pressure Turbine Vane Using Ultra-Fast-Response Temperature-Sensitive Paint	6
Scale-Resolving Simulations of Turbulent Flow Retaining the Exact Blade Count With the Time-Inclined Method	6
Experimental Investigation of Flame-Film Cooling Interactions With an Academic Test Rig and Optical Laser Diagnostics	6
The Relative Effects of Internal Reynolds Number and Advective Capacity Ratio on the Coolant Warming Factor	6
An Active Turbulence Grid for Turbomachinery Flow Experiments	6
Low Reynolds Number Effects on the Endwall Flow Field in a High-Lift Turbine Passage	6