Journal of Turbomachinery-Transactions of the Asme

Article	Citations
Effect of Leading Edge Erosion on the Tip Leakage Flow in a Compressor Cascade	35
Effects of Radially Variable Sweep Vanes on Rotor–Stator Interaction Noise	32
An Improved Particle Impact Model by Accounting for Rate of Strain and Stochastic Rebound	30
Effect of the Key Geometry and Flow Parameters on Discharge Coefficient of Laidback Fan-Shaped Hole Under Coolant Crossflow Condition	29
On the Divergence Mechanisms Analysis of a Vibrating Blade Subjected to Repetitive Rubs With an Abradable Coating	25
Analysis of the Bifurcating Duct of an Inlet Particle Separator in Transonic Flow Conditions	23
Turbine Vane Passage Cooling Experiments With a Close-Coupled Combustor-Turbine Interface Geometry—Part I: Describing the Flow	23
Three-Dimensional Unsteady Aerodynamic Optimization of a Transonic Compressor Stage Using an Implicit Discrete Adjoint Harmonic Balance Method	22
Experimental Study on the High Relative Casing Motion Effect on Turbine Blade Tip Aerodynamic Characteristics	20
Rotating Instabilities in Shrouded Low Pressure Turbine at Design and Off-Design Conditions	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	19
Coupled Time and Passage Spectral Method for an Efficient Resolution of Turbomachinery Far Upstream Wakes	19
Exploring Topology Optimization for High Pressure Turbine Blade Tips	18
Evaluation of Cooling Requirements for Rotating Detonation Combustors	18
Unique High-Resolution Temperature Mapping of Stage 1 Turbine Vane in a Long-Term Engine Test	17
Prediction of Steady and Unsteady Flow Quantities Using Multiscale Graph Neural Networks	17
Physics-Guided Graph Neural Networks: Numerical Investigation of High-Pressure Turbine Flow	15
Nonlinear Flutter Analysis of Labyrinth Seals	15
The Effects of Swirling Flows in Entropy Wave Convection Through High-Pressure Turbine Stage	15
Unsteady Pre-Stall Behavior in a Centrifugal Compressor With Vaned Diffuser	15
An Analysis of the Secondary Flow Around a Tandem Blade Under the Presence of a Tip Gap in a High-Speed Linear Compressor Cascade	15
A Method for Preliminary Design of Variable Geometry Vaned Diffuser for Centrifugal Compressor	14
Fan Non-Synchronous Forced Vibration Under Crosswind	14
Modeling and Simulation of Sand Particle Trajectories and Erosion in a Transonic Fan Stage	14

Introduction of Axisymmetric Grooves as a Tip Seal Treatment for Small-Core Turbines	14
Measurements of Turbulence in Compressible Low-Density Flows at the Inlet of a Transonic Linear Cascade With and Without Unsteady Wakes	13
Film Cooling on Turbine Vane Endwalls With Different Inlet Cooling Configurations: Experimental and Computational Results	13
A New Multi-Stage Turbine Stator Design for Improved Performance Retention	12
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	12
Acoustic Modes in an Open Box Cavity With Variable Depth Using Two Distinct Wind Tunnels	12
A Framework for Estimating Effects of Combustor Turbulence on Turbine Profile Loss Generation	12
Aerodynamic Effect of Shallow Circumferential Grooves in the Shroud of a Centrifugal Compressor	12
Foam-Metal Casing Treatment on an Axial Flow Compressor: Stability Improvement and Noise Reduction	12
Reviewer’s Recognition	12
Numerical Study on the Effect of Back Cavity on the Aerodynamic Behavior of a Non-Axisymmetric Casing Treatment for Transonic Axial Compressors	12
Inlet Flow Distortion in an Advanced Civil Transport Boundary Layer Ingesting Engine Installation	12
The Cooling Effect of Combustor Exit Louver Scheme on a Transonic Nozzle Guide Vane Endwall	11
Pragmatic Prediction Model of Droplet Trajectory in a Turbine Cascade	11
One-Dimensional Modeling for Pulsed Flow Twin-Entry Turbine	11
Spectral Heat Transfer Coefficient for Thermal Design Analysis—Part 1: Augmenting the Cooling Law for Non-Isothermal Wall	11
Systematic Numerical Investigation on the Surface Roughness Effects on the Friction and Heat Transfer of Additively Manufactured Components	11
A Study of Loss Model Parameter Sensitivity in Compressor Unsteady Flow Simulations	11
Loss Analysis of Cavity Leakage Flow in a Compressor Cascade	11
Impacts of Tandem Configurations on the Aerodynamic Performance of an Axial Supersonic Through-Flow Fan Cascade	11
Fundamentals of Scaling of Overall Cooling Effectiveness With Temperature Ratio	11
Tail-Integrated Boundary Layer Ingesting Propulsion Systems for Turbo-Electric Aircraft	11
Unpacking Intermineral Synergies and Reactions During Dust Deposition in an Impingement Coolant Jet	10
Analysis of Complex Total Pressure Distortion Screens Using One-Dimensional Loss Data	10
Stall Behavior in an Ultrahigh-Pressure-Ratio Centrifugal Compressor: Backward-Traveling Rotating Stall	10
Effects of Downstream Vortex Generators on Film Cooling a Flat Plate Fed by Crossflow	10
Entry Region Heat Transfer Augmentation With Pins, Fins, and Turbulators in Circular Channels	10
Aerodynamics and Heat Transfer Inside a Gas Turbine Mid-Passage Gap	10
Experimental Determination of Heat Transfer Coefficient on Impingement Cooled Gear Flanks: Validation of the Evaluation Method	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	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
On the Over-Prediction of Centrifugal Compressor Pressure Ratio in the High Impeller Tip Mach Number Regime	9
Multistage Turbomachinery Optimization for High-Temperature Heat Pumps With the Reverse Rankine Cycle	9
Effects of Surface Waviness on Fan Blade Boundary Layer Transition and Profile Loss—Part I: Methodology and Computational Results	9
Aerothermal Performance Robustness and Reliability Analysis of Turbine Blade Squealer Tip With Film Cooling	9
Particle Image Velocimetry in a High-Speed Short-Duration Turbine Rig	9
Unsteady Aerodynamic Forcing Due to Distortion in a Boundary Layer Ingesting Fan	9
Experimental Investigation of Additional Loss Associated With Incoming Wakes in Low-Pressure Turbine Cascades	9
Experimental Study on Controlling Flow Separation of Compressor Cascades With Self-Excited Sweeping Jet Actuator	9
Numerical Study on Unsteady Flow of a Supersonic Partial Admission Impulse Turbine	8
Numerical Assessment of an Aerodynamic Probe to Enable Short Focal Length Laser Diagnostics in High Temperature Supersonic Flows Based on Flow Disturbance	8
AN EXPERIMENTAL INVESTIGATION OF SWEEPING MIST JET FILM COOLING WITH DROPLET ANALYSIS	8
An Improved Passage-Flow Turning Model for Forward-Curved Blades of Squirrel-Cage Fan	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
Numerical Study of Crossflow Effects on Discharge Coefficient of the Converging Slot Hole	8
Effect of Upstream Leakage Flow on Film Cooling Characteristic of a Turbine Convex Endwall	8
Blade Envelopes Part I: Concept and Methodology	8
Impact of High-Pressure-Turbine Purge Flow on the Evolution of Turbulence in a Turbine Vane Frame	8

Windage Torque Reduction in Low-Pressure Turbine Cavities Part II: Experimental and Numerical Results	8
High-Fidelity Investigation of Vortex Shedding From a Highly Loaded Turbine Blade	8
Numerical Investigation on the Influence of Wet Compression Aerodynamic Performance of Multi-Stage Transonic Compressor	8
Investigation of Tip Leakage Vortex Breakdown in a High-Speed Multistage Axial Compressor	8
Flow Check and Adiabatic Effectiveness Measurements on Traditionally Versus Additively Manufactured Film-Cooling Holes	8
Unsteady Flow Structure of Corner Separation in a Highly Loaded Compressor Cascade	8
Direct and Inverse Model for Single-Hole Film Cooling With Machine Learning	8
Insights Into Turbocharger Centrifugal Compressor Stability Using High-Fidelity Computational Fluid Dynamics and a Novel Impeller Diffusion Factor	8
Revisiting Dimensionless Parameters Quantifying Film Cooling	8
Strategies for High-Accuracy Measurements of Stage Efficiency for a Cooled Turbine	7
A Detailed Loss Analysis Methodology for Centrifugal Compressors	7
Film Superposition Characteristics With Laidback Fan-Shaped Holes Under the Influence of Internal Crossflow	7
RANS Capabilities for Transonic Axial Compressor: A Perspective From GPPS Computational Fluid Dynamics Workshop	7
Numerical Investigation of the Fan Flutter Mechanism Related to Acoustic Propagation Characteristics	7
Dissipation in Skewed Boundary Layers	7
The Influence of Deterministic Surface Roughness and Freestream Turbulence on Transitional Boundary Layers: Heat Transfer Distributions and a New Transition Onset Correlation	7
Heat Transfer in an Injector-Scaled Additively Manufactured Fuel Passage	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
Sensitivity Analysis for Flow Stability of Axial Compressor Based on Meridional Flow	7
Investigation of the Map Width Improvement in a Radially Reduced Diffuser Design Concept for a Centrifugal Compressor	7
Suppression of Nonsynchronous Vibration Through Intentional Aerodynamic and Structural Mistuning	7
The Application of Fluidic Sealing in Shrouded Gas Turbine Blades	7
Noise Source Identification for the Unsteady Low-Pressure Turbine Flow Fields	7
Application of Advanced RANS Turbulence Models for the Prediction of Turbomachinery Flows	7
A Review of Secondary Combustion on the Turbine Blade Cooling	7
Comparative Study of Tip Injection in a Transonic and Subsonic Compressor	7
Unsteadiness in the Secondary Flows of a High-Speed Low-Pressure Turbine Cascade With Unsteady Wakes and Purge Flow	7
Advanced Design of a Transition Duct for Supersonic Inlet Turbines in Rotating Detonation Engines	7
ANALYSIS OF AEROACOUSTIC PHENOMENA IN CENTRIFUGAL COMPRESSORS USING A LATTICE BOLTZMANN FLOW SIMULATION APPROACH	7
Response of Separated Boundary Layers to Steady and Pulsated Flow Injection	7
Dirt Ingestion Impacts on Cooling Within a Double-Walled Combustor Liner	7
Morphing of Reversible Axial Fan Blade: A FSI-FEM Study	7
Particle Bounce Stick Behavior in the Rotating Frame of Reference	7
Optimal Riblets Applied to Gas Turbine Compressor Blades Studied via Direct Numerical Simulation (GT2024–122305)	7
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
Effect of Solidity and Aspect Ratio on the Aerodynamic Performance of Axial-Flow Fans With 0.2 Hub-to-Tip Ratio	6
Impact of Swirling Entropy Waves on a High Pressure Turbine	6
A New Nonlinear Time-Domain Flutter Analysis Approach for Distorted Flows	6
A High-Speed Disk Rotor Rig Design for Tip Aerothermal Research	6
Influences of Particulate Deposition on Vane Trailing-Edge Film Cooling: Adiabatic and Overall Cooling Effectiveness	6
UHBR Open-Test Case Fan ECL5/CATANA: Non-Linear Analysis of Non-Synchronous Blade Vibration at Part-Speed Conditions	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
Adaptation of von Karman Institute for Fluid Dynamics’ Isentropic Compression Tube Facility for High-Speed Low-Pressure Turbines Testing	6
The Influence of Purge Flow Parameters on Heat Transfer and Film Cooling in Turbine Center Frames	6
A Shock Loss Reduction Method Using a Concave Suction Side Profile for a Zero Inlet Swirl Turbine Rotor	6
The Effects of Incoming Vortex and Wake on the Aerodynamics of an Intermediate Turbine Duct	6
Robustness Analysis on Aerothermal Performance of the Winglet Squealer Tip—Part 1: Aerodynamic Performance	6
Equation-Oriented Meanline Method for Axial Turbine Performance Prediction Under Choking Conditions	6
The Influence of Combustor Hot Streaks on the Aerodynamic Performance of a Turbine Center Frame	6
A New Loss Generation Body Force Model for Fan/Compressor Blade Rows: Application to Uniform and Non-Uniform Inflow in Rotor 67	6
Experimental Research Into Aeroelastic Phenomena in Turbine Rotor Blades Inside ARIAS EU Project	6
Impact of Low Freestream Turbulence and Surface Roughness on the Flat-Plate Boundary Layer Transition Under a High-Lift Airfoil Pressure Gradient	6
GPU-Accelerated Full-Wheel Large-Eddy Simulations of a Transonic Fan Stage	6
The Effect of Inlet Conditions on Turbine Endwall Loss	6
Characterizing Flow Instabilities During Transient Events in the Turbine Rim Seal Cavity	6
Optimization of a Tip Appendage for the Control of Tip Leakage Vortices in Axial Flow Fans	6
A Three-Dimensional Actuator Disk Model for Fan Response to Inlet Distortion: Part I - Formulation	6
Loss Analysis in Radial Inflow Turbines for Supercritical CO2 Mixtures	6
Manufacturing a Ceramic Turbine Rotor for a Compact Jet Engine	6
Collaborative Robust Design Optimization of Blade Geometry and Manufacturing Tolerance for a Transonic Centrifugal Impeller	6
Cooling Performance of Additively Manufactured Pin Fins in Stacked Microchannels for the Inside-Out Ceramic Turbine Shroud-Cooling Ring	6
Investigating the Influence of Mainstream Turbulence and Large Vortices on Gas Turbine Trenched Film Cooling Flows Using Planar Temperature-Velocity Imaging	6
Plume Model for Buoyancy-Induced Flow and Heat Transfer in Closed Rotating Cavities	6
Data Assimilation of Transitional and Separated Turbomachinery Flows With Physics-Informed Neural Networks	6
Impacts of Material and Machine on the Variation of Additively Manufactured Cooling Channels	6
Effects of Ribbed Surfaces on Profile Losses of Low-Pressure Turbine Blades	6
Magnetic Resonance Velocimetry of a Turbine Blade With Engine-Representative Internal and Film Cooling Structures	6
A Free Streamline Model for Fully Separated Turbomachine Flows	6
Experimental and Numerical Investigation of High Load Turbine Blade Tip Cavity Structures	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
Highly Time Resolved, Combined Temperature, and Heat Flux Measurement Technique Based on ALTP Sensors	6
A Physics-Informed Neural Network for Solving the Inverse Heat Transfer Problem in Gas Turbine Rotating Cavities	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
Heat Transfer and Flow Field Characteristics of Variable Aspect Ratio, Serpentine Passages	5
Innovative Cavity Modeling for Centrifugal Compressors Aeromechanical Analysis	5
Wake–Separation Bubble Interaction Over an Experimentally Simulated Axial Compressor Blade Under Low Reynolds Number Flow	5
Experimental and Numerical Analysis of Loss Characteristics of Cooled Transonic Nozzle Guide Vanes	5
Turbulence Measurements at the Inlet of an Automotive Turbocharger Compressor Using Stereoscopic Particle Image Velocimetry	5
Impact of the Purge Flow Density Ratio on the Rim Sealing Effectiveness in Hot Gas Ingestion Measurements	5

Effects of Rotation on the Flow Structure in a Compressor Cascade	5
Interaction Mechanism of Transonic Squealer Tip Cooling With the Effect of High-Speed Relative Casing Motion	5
Development of Compact and Hermetic Organic Rankine Cycle Turbine Generator With Upgraded Cooling Capability	5
The Unsteady Topology of Corner Separations	5
Improvements in the Prediction of Steady and Unsteady Transition and Mixing in Low-Pressure Turbines by Means of Machine-Learnt Closures	5
Annular Dump Diffuser and Deswirl System for Back-Pressure Control in Engine-Scale Transonic Annular Cascade	5
Turbine Nozzle Guide Vane Endwall Film Cooling and Vane Phantom Cooling Performances at Various Blocked Film Hole Configurations	5
Improved Prediction of Losses With Large Eddy Simulation in a Low-Pressure Turbine	5
The Influence of Boundary Layer State and Trailing Edge Wedge Angle on the Aerodynamic Performance of Transonic Turbine Blades	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
On the Secondary Flow System of an Aggressive Inter Compressor Duct	5
High-Fidelity Computational Assessment of Aero-Thermal Performance and the Reynolds’ Analogy for Additively Manufactured Anisotropic Surface Roughness	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
Low Reynolds Number Effects on the Endwall Flow Field in a High-Lift Turbine Passage	5
Analysis of Averaging Methods for Nonuniform Total Pressure Fields	5
Experimental Investigation of Mode-Frequency Scattering at Fan Stages	5
Wall-Modeled LES of a Transonic Gas Turbine Vane - Part II: Mach Number Effect and Losses Prediction	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
Effects of Water-to-Air Mass Ratio on Long-Term Washing Efficiency and Erosion Risk in an Axial Compressor Under Online Washing Conditions	5
Inverse Design of Compressor/Fan Blade Profiles Based on Conditional Invertible Neural Networks	5
Modeling of Combustor Non-Uniformities Evolution Through a High-Pressure Turbine Stage	5
Investigating Gas Turbine Internal Cooling Using Supercritical CO2 at Higher Reynolds Numbers for Direct Fired Cycle Applications	5
Large Eddy Simulation of Laminar and Turbulent Shock/Boundary Layer Interactions in a Transonic Passage	5
A Test Facility for the Experimental Investigation of Labyrinth Seal Flutter and Early-Stage Validation of Prediction Techniques	5
An Active Turbulence Grid for Turbomachinery Flow Experiments	5
Efficient Aerodynamic Uncertainty Quantification for a Three-Dimensional Transonic Fan Rotor	5
Effective Clearance and Differential Gapping Impact on Seal Flutter Modeling and Validation	5
Quasi-Dynamic Approximation of Unsteady Pressure Distribution for Transonic Airfoils in Flutter	5
Pressure Characteristic Rollover of a Transonic Centrifugal Impeller	5
Investigation on Heat Transfer Distribution of Rotating Two-Pass Smooth and Ribbed Channels Under Aero-Engine Simulated Conditions	4
Experimental and Numerical Comparison of Two Turbine Vane Frame Designs	4
Impact of Flow Unsteadiness on Turbine Airfoil Heat Transfer via Streaming	4
Mitigation of Boundary Layer Ingestion Circumferential Distortion Using Nonaxisymmetric Fan Exit Guide Vanes	4
The Effect of Reaction on Compressor Performance	4
Experimental Investigation of Flame-Film Cooling Interactions With an Academic Test Rig and Optical Laser Diagnostics	4
Challenges in Aerodynamic Performance of Micro Gas Turbines and Design Inefficiencies	4
Boundary Layer Analysis of a Transonic High-Pressure Turbine Vane Using Ultra-Fast-Response Temperature-Sensitive Paint	4
Using Data Assimilation to Improve Turbulence Modeling for Inclined Jets in Crossflow	4
Experimental Study of Impact of In-Service Deterioration on Thermal Performance of High-Pressure Nozzle Guide Vanes	4
A Resistive Model to Characterize Overall Effectiveness Influenced by Multiple Coolant Temperatures	4
Large Eddy Simulation Analysis of Loss Anomaly of a Turbine Blade With Large Trailing Edge Radius	4
Unsteady Structure of Compressor Tip Leakage Flows	4
Unsteady Loss Mechanisms in Low-Pressure Turbines With Diverging End-Walls Studied Via High-Fidelity Simulation	4
Unsteady Flow Development and Reynolds Stress Measurements in a Centrifugal Compressor Vaned Diffuser	4
Effect of Geometry and Heat Flux on Turbine Over-Tip Flow Power Extraction	4
A Simplified Injection Model for Variable Area Turbine Fluidic Throttling	4
Heat Transfer in a Rotating, Blade-Shaped, Two-Pass Cooling Channel With a Variable Aspect Ratio	4
Aerodynamic Influence of a Bleed on the Last Stage of a Low-Pressure Compressor and S-Duct	4
Influence of Casing Groove on Rotating Instabilities in a Low-Speed Axial Compressor	4
The Impact of the Off-Design Conditions on the Entropy Wave Interaction With a High-Pressure Turbine Stage	4
Unsteady Investigation of Intermediate Turbine Ducts Under the Influence of Purge Flows	4
Validation of Filtered Rayleigh Scattering Optical Rake Measurement Techniques in Turbomachinery Applications and Boundary Layers	4
Reynolds Number Effect on Transitional Delayed Detached-Eddy Simulation	4
Numerical Investigation of the Effect of Trailing Edge Thickness of Simulated Ceramic Matrix Composite Blades on Loss Profiles	4
Hybrid RANS-LES Simulation of Rotor–Stator Interaction in a Compressor Stage Using a Grid-Adaptive Simulation Method	4
A New Axial Compressor Test Facility for the Investigation of Aerodynamic Damping Featuring an Electromagnetic Excitation System	4
A Digital Engineering Analysis of an Additively-Manufactured Turbine Vane	4
Considerations for Compressible Film Cooling: A Computational Study of the Effects of Transonic Flows and Varying Mainstream Mach Number	4
The Effect of Upstream Unsteadiness on the Unstarting of a Supersonic Inlet Turbine	4
The Role of Turbine Operating Conditions on Combustor–Turbine Interaction—Part II: Loading Effects	4
Turbine Vane Passage Cooling Experiments With a Close-Coupled Combustor–Turbine Interface Geometry Part II: Describing the Coolant Coverage	4
The Role of Turbine Operating Conditions on Combustor–Turbine Interaction—Part I: Change in Expansion Ratio	4
On Intake–Compressor Interactions Within an Integrated Propulsion System	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
Validation of Broadband Noise Prediction Methodology Based on Linearized Navier–Stokes Analyses	4
Global Optimization of a Transonic Fan Blade Through AI-Enabled Active Subspaces	4
Fan Flutter Mechanisms Related to Blade Mode Shape and Acoustic Properties	4
Fan Stability Enhancement With Partial Casing Treatments	4
Cavity Impact on the Base Flow Unsteadiness for a High-Speed Exhaust System	4
Effect of Coolant Crossflow on Film Cooling Effectiveness of Diffusion Slot Hole With and Without Ribs	4
Data-Driven Radial Compressor Design Space Mapping	4
Computational and Experimental Study of Film-Cooling Effectiveness With and Without Downstream Vortex Generators	4
Innovative Design, Structural Optimization, and Additive Manufacturing of New-Generation Turbine Blades	4
Characterizing the Unsteady Flow Field in Low-Flow Turbine Operation	4
The Impact of Manufacturing Variations on the Aerothermal Performance of High-Pressure Turbine Blade Shrouds	4
High-Dimensional Uncertainty Quantification of High-Pressure Turbine Vane Based on Multifidelity Deep Neural Networks	4
Aero-Structural Coupling Strategy for a Morphing Blade Cascade Study	4
Scaling Heat Transfer and Pressure Losses of Novel Additively Manufactured Rib Designs	4
Analysis on the Effect of Cavity Flows on the Aerothermal Performance of a High-Pressure Turbine Stage	4
Extending Highly Loaded Axial Fan Operability Range Through Novel Blade Design	4
Experimental Investigation of the Pre-Stall and Stall Evolution in a Centrifugal Compressor With a Volute	4
Bayesian Mass Averaging in Rigs and Engines	4
Roughness-Resolved Large-Eddy Simulation of Additive Manufacturing-Like Channel Flows	3
Compressor Tip Leakage Mechanisms	3
Experiments on Tuned UHBR Open-Test-Case Fan ECL5/CATANA: Performance and Aerodynamics	3
Progresses in Particle-Laden Flows Simulations in Multistage Turbomachinery With OpenFOAM	3
Effect of Blade Damage on Low Pressure Ratio Fan Windmill Aerodynamics	3
Study on Effects of Spanwise-Expansion Parameters on Film Cooling Effectiveness of Diffusion Shaped Hole Configurations	3
Reconstruction and Reduction of Realistic Manufacturing Error Field for Uncertainty Quantification of Transonic Axial Compressor Rotor	3
Effect of Tip Vortex Reduction on Air-Cooled Condenser Axial Flow Fan Performance: An Experimental Investigation	3
PDA Laser Measurements of Droplet-Laden Flows in a Four-Stage Axial Compressor	3
Integration of Cooling Holes Into a Turbine Vane Made Using Additive Manufacturing	3
Numerical Investigation of Near-Tip Modifications for a Highly Loaded Low-Speed Rotor Under the Influence of Double Leakage	3