Journal of Turbomachinery-Transactions of the Asme

Article	Citations
Effect of a Combined Hot-Streak and Swirl Profile on Cooled 1.5-Stage Turbine Aerodynamics: An Experimental and Computational Study	29
Detached Eddy Simulation: Recent Development and Application to Compressor Tip Leakage Flow	19
Impact of Additive Manufacturing on Internal Cooling Channels With Varying Diameters and Build Directions	18
Effect of Manufacturing Tolerance in Flow Past a Compressor Blade	18
Aerodynamics of Boundary Layer Ingesting Fuselage Fans	18
Experimental Study on Aerodynamic Loss and Heat Transfer for Various Squealer Tips	18
Experimental Investigation of Innovative Cooling Schemes on an Additively Manufactured Engine Scale Turbine Nozzle Guide Vane	15
Adiabatic Effectiveness Measurements for a Baseline Shaped Film Cooling Hole	15
Integration of Machine Learning and Computational Fluid Dynamics to Develop Turbulence Models for Improved Low-Pressure Turbine Wake Mixing Prediction	15
Inlet Flow Distortion in an Advanced Civil Transport Boundary Layer Ingesting Engine Installation	15
Scaling Considerations for Thermal and Pressure-Sensitive Paint Methods Used to Determine Adiabatic Effectiveness	14
Experimental Study of Oscillating Freestream Effect on the Spatiotemporal Distributions of Leading-Edge Film Cooling	14
Fan Aerodynamics With a Short Intake at High Angle of Attack	14
Flow in a Simulated Turbine Blade Cooling Channel With Spatially Varying Roughness Caused by Additive Manufacturing Orientation	14
Study on Effects of Spanwise-Expansion Parameters on Film Cooling Effectiveness of Diffusion Shaped Hole Configurations	13
Multidisciplinary Design Optimization for Performance Improvement of an Axial Flow Fan Using Free-Form Deformation	13
Global Optimization of a Transonic Fan Blade Through AI-Enabled Active Subspaces	13
Pulsed Suction Control in a Highly Loaded Compressor Cascade With Low Suction Flowrates	13
Uncertainty Quantification of Aero-Thermal Performance of a Blade Endwall Considering Slot Geometry Deviation and Mainstream Fluctuation	13
Large-Eddy Simulations of High Rossby Number Flow in the High-Pressure Compressor Inter-Disk Cavity	13
Statistical Error Estimation Methods for Engineering-Relevant Quantities From Scale-Resolving Simulations	13
Unsteady Structure of Compressor Tip Leakage Flows	13
Effect of Surface Roughness and Inlet Turbulence Intensity on a Turbine Nozzle Guide Vane External Heat Transfer: Experimental Investigation on a Literature Test Case	12
Interpretation of Stall Precursor Signatures	12
A Detailed Loss Analysis Methodology for Centrifugal Compressors	12

Effect of Tip Clearance on Rotating Stall in a Mixed-Flow Pump	12
Investigation of Endwall Heat Transfer in Staggered Pin Fin Arrays	12
Active Flow Control Utilizing an Adaptive Blade Geometry and an Extremum Seeking Algorithm at Periodically Transient Boundary Conditions	12
Computational and Experimental Study of the Unsteady Convection of Entropy Waves Within a High-Pressure Turbine Stage	11
Metamodel-Driven Data Mining Model to Support Three-Dimensional Design of Centrifugal Compressor Stage	11
Free-Stream Turbulence-Induced Boundary-Layer Transition in Low-Pressure Turbines	11
On High-Resolution Pressure Amplitude and Phase Measurements Comparing Fast-Response Pressure Transducers and Unsteady Pressure-Sensitive Paint	11
Foam-Metal Casing Treatment on an Axial Flow Compressor: Stability Improvement and Noise Reduction	11
Study of Relative Endwall Motion Effects in a Compressor Cascade Through Direct Numerical Simulations	11
Upstream Film Cooling on the Contoured Endwall of a Transonic Turbine Vane in an Annular Cascade	11
Experimental and Numerical Study of the Turbulent Flow and Heat Transfer in a Wedge-Shaped Channel With Guiding Pin Fin Arrays Under Rotating Conditions	10
Flow Physics During Surge and Recovery of a Multi-Stage High-Speed Compressor	10
Heat Transfer Characteristics Within the Matrix Cooling Channels	10
Investigation of Unsteady Rotor–Stator Interaction and Deterministic Correlation Analysis in a Transonic Compressor Stage	10
Optimization of Turbine Cascade Squealer Tip Cooling Design by Combining Shaping and Flow Injection	10
Effect of Radiation on Heat Transfer Inside Aeroengine Compressor Rotors	10
Impacts of Pin Fin Shape and Spacing on Heat Transfer and Pressure Losses	10
Experimental and Numerical Investigation of High Load Turbine Blade Tip Cavity Structures	10
Pulsed Impingement Turbine Cooling and Its Effect on the Efficiency of Gas Turbines With Pressure Gain Combustion	10
Single and Multiple Circumferential Casing Groove for Stall Margin Improvement in a Transonic Axial Compressor	10
Casing Treatment: Its Potential and Limitations	10
Fully Coupled Large Eddy Simulation-Conjugate Heat Transfer Analysis of a Ribbed Cooling Passage Using the Immersed Boundary Method	10
Eddy Resolving Strategies in Turbomachinery and Peripheral Components	10
Effect of Coolant Crossflow on Film Cooling Effectiveness of Diffusion Slot Hole With and Without Ribs	9
Analysis Method of Nonsynchronous Vibration and Influence of Tip Clearance Flow Instabilities on Nonsynchronous Vibration in an Axial Transonic Compressor Rotor	9
Direct and Inverse Model for Single-Hole Film Cooling With Machine Learning	9
Experimental Investigation on Cooling Performance of Impingement–Effusion Full Coverage Film on Suction Surface of a Vane	9
Low Reynolds Number Effects on the Separation and Wake of a Compressor Blade	9
Surface Roughness Impact on Boundary Layer Transition and Loss Mechanisms Over a Flat-Plate Under a Low-Pressure Turbine Pressure Gradient	9
Heat Transfer Measurements for Array Jet Impingement With Castellated Wall	9
Application of Advanced RANS Turbulence Models for the Prediction of Turbomachinery Flows	8
Analysis of the Loss Production Mechanism Due to Cavity–Main Flow Interaction in a Low-Pressure Turbine Stage	8
Aerodynamic Investigation of a Composite Low-Speed Fan for UHBR Application	8
Experimental Heat Transfer and Boundary Layer Measurements on a Ceramic Matrix Composite Surface	8
Accurate Prediction of Loss Using High Fidelity Methods	8
Stall Margin Improvement in a Transonic Compressor With a Casing Treatment: Flow Mechanism	8
Heat Transfer in a Rotating, Two-Pass, Variable Aspect Ratio Cooling Channel With Profiled V-Shaped Ribs	8
Machine Learning for the Development of Data-Driven Turbulence Closures in Coolant Systems	8
Uncertainty Evaluation on Multi-Hole Aerodynamic Pressure Probes	8
A Novel Multi-Stage Impingement Cooling Scheme—Part I: Concept Study	8
Blade Envelopes Part I: Concept and Methodology	8
A Novel Multi-Stage Impingement Cooling Scheme—Part II: Design Optimization	8
Scalar Diffusion Equation-Based Model to Predict 2-Dimensional Film Cooling Effectiveness of a Shaped Hole	8
Effect of Differential Tip Clearance on the Performance of a Tandem Rotor	8
Effect of Boundary Layer Suction on the Corner Separation in a Highly Loaded Axial Compressor Cascade	8
Effects of Inlet Guide Vanes on the Performance and Stability of an Aeronautical Centrifugal Compressor	8
Heat Transfer in a Rotating, Blade-Shaped, Two-Pass Cooling Channel With a Variable Aspect Ratio	8
Acquisition and Processing Considerations for Infrared Images of Rotating Turbine Blades	8
InstabilitiesEverywhere!Hard Problems in Aero-Engines	8
Analysis of the Unsteady Flow Field Inside a Fan-Shaped Cooling Hole Predicted by Large Eddy Simulation	8

Estimation of Aircraft Engine Flight Mission Severity Caused by Erosion	8
Plume Model for Buoyancy-Induced Flow and Heat Transfer in Closed Rotating Cavities	8
Numerical Investigation of Effects of Blockage, Inclination Angle, and Hole-Size on Film Cooling Effectiveness at Concave Surface	8
Extending Highly Loaded Axial Fan Operability Range Through Novel Blade Design	8
An Efficient Aeroelastic Eigenvalue Method for Analyzing Coupled-Mode Flutter in Turbomachinery	8
Uncertainty Quantification of Spalart–Allmaras Turbulence Model Coefficients for Compressor Stall	7
Aerodynamic Effects of an Incoming Vortex on Turbines With Different Tip Geometries	7
Efficiency Scaling: Influence of Reynolds and Mach Numbers on Fan Performance	7
High-Fidelity Simulations of a High-Pressure Turbine Vane Subject to Large Disturbances: Effect of Exit Mach Number on Losses	7
Analysis of Averaging Methods for Nonuniform Total Pressure Fields	7
Endwall Heat Transfer and Cooling Performance of a Transonic Turbine Vane With Upstream Injection Flow	7
Experimental and Numerical Analysis of Loss Characteristics of Cooled Transonic Nozzle Guide Vanes	7
Forced Response Due to Vane Stagger Angle Variation in an Axial Compressor	7
Heat Transfer and Pressure Loss of Additively Manufactured Internal Cooling Channels With Various Shapes	7
Physical Mechanisms Investigation of Sharkskin-Inspired Compressor Cascade Based on Large Eddy Simulations	7
The Effects of Reynolds Number on the Stall and Pre-Stall Behavior of Compact Axial Compressors	7
Aerodynamic Loading Considerations of Three-Shaft Engine Compression System During Surge	7
Impacts of the Additive Manufacturing Process on the Roughness of Engine Scale Vanes and Cooling Channels	7
Effects of Jet Impingement on Convective Heat Transfer in Effusion Holes	7
Sweeping Jet Film Cooling at High Blowing Ratio on a Turbine Vane	7
Innovative Design, Structural Optimization, and Additive Manufacturing of New-Generation Turbine Blades	7
Computer 3D Vision-Aided Full-3D Optimization of a Centrifugal Impeller	7
DEVELOPMENT OF A LIFETIME PRESSURE SENSITIVE PAINT PROCEDURE FOR HIGH-PRESSURE VANE TESTING	7
Numerical and Experimental Study on Rotating Stall in Industrial Centrifugal Compressor	7
Development and Validation of a Model for Centrifugal Compressors in Reversed Flow Regimes	7
Heat Transfer in Rotating, Trailing-Edge, Converging Channels With Smooth Walls and Pin-Fins	6
Comparative Study of Tip Injection in a Transonic and Subsonic Compressor	6
Stratified and Buoyancy-Induced Flow in Closed Compressor Rotors	6
Experimental and Numerical Quantification of the Aerodynamic Damping of a Turbine Blisk	6
Application of Scale Adaptive Simulation Model to Studying Cooling Characteristics of a High Pressure Turbine Blade Cutback Trailing Edge With Different Cooling Configurations	6
Generation Mechanism of Broadband Whoosh Noise in an Automotive Turbocharger Centrifugal Compressor	6
The Effects of Inlet Boundary Layer Condition and Periodically Incoming Wakes on Secondary Flow in a Low Pressure Turbine Cascade	6
Zonal Detached Eddy Simulation of the Fan-Outlet Guide Vanes Stage of a Turbofan Engine: Part I—Methodology, Numerical Setup, and Aerodynamic Analysis	6
Non-Dimensional Parameters for Comparing Conventional and Counter-Rotating Turbomachines	6
Heat Transfer in Rotating, Trailing Edge, Converging Channels With Full- and Partial-Height Strip-Fins	6
Vortex Tracking of Purge-Mainstream Interactions in a Rotating Turbine Stage	6
High-Fidelity Simulations of Multi-Jet Impingement Cooling Flows	6
Exploring Applicability of Acoustic Heat Transfer Enhancement Across Various Perturbation Elements	6
A Robust Implementation of a Reynolds Stress Model for Turbomachinery Applications in a Coupled Solver Environment	6
Aerothermal Optimization of Turbine Squealer Tip Geometries With Arbitrary Cooling Injection	6
Aero-Thermal Aspects of Film Cooled Nozzle Guide Vane Endwall—Part 1: Aerodynamics	6
Experimental Investigation of Film Cooling Performance on Blade Endwall With Diffusion Slot Holes and Stator–Rotor Purge Flow	6
Effects of Turning Angle and Turning Internal Radius on Channel Impingement Cooling for a Novel Internal Cooling Structure	6
Averaging for High Fidelity Modeling—Toward Large Eddy Simulations in Multi-Passage Multi-Row Configurations	6
Azimuthal Mode Characteristics of Rotating Instability in Axial Compressor Using Compressed Sensing Method	6
Nonlinear Stability Analysis of a Generic Fan With Distorted Inflow Using Passage-Spectral Method	6
Impacts of Tandem Configurations on the Aerodynamic Performance of an Axial Supersonic Through-Flow Fan Cascade	6
Experimental and Computational Investigation of Integrated Internal and Film Cooling Designs Incorporating a Thermal Barrier Coating	6
Automatic Design Optimization of a Transonic Compressor Rotor for Improving Aeroacoustic and Aerodynamic Performance	6
Wall Temperature Measurements in a Full-Scale Gas Turbine Combustor Test Rig With Fiber Coupled Phosphor Thermometry	6
Turbine Endwall Contouring Through Advanced Optimization Techniques	6
Experimental and Numerical Study of an Open Impeller Centrifugal Compressor Stage Utilizing Three-Dimensional (3D) Diffuser End Wall Contouring for Operating Range Extension	6
NASA's Role in Gas Turbine Technology Development: Accelerating Technical Progress Via Collaboration Between Academia, Industry, and Government Agencies	6
Modeling of Axial Compressor With Large Tip Clearances	6
Investigation of Tip Leakage Vortex Breakdown in a High-Speed Multistage Axial Compressor	6
Reconstructing Compressor Non-Uniform Circumferential Flow Field From Spatially Undersampled Data—Part 1: Methodology and Sensitivity Analysis	6
Infrared Temperature Measurements of the Blade Tip for a Turbine Operating at Corrected Engine Conditions	6
On the Importance of Transition Control at Transonic Compressor Blades	6
Unsteady Lattice Boltzmann Simulations of Corner Separation in a Compressor Cascade	6
Stall Behavior in an Ultrahigh-Pressure-Ratio Centrifugal Compressor: Backward-Traveling Rotating Stall	6
Microstructure of IN738LC Fabricated Using Laser Powder Bed Fusion Additive Manufacturing	6
Collaborative Robust Design Optimization of Blade Geometry and Manufacturing Tolerance for a Transonic Centrifugal Impeller	6
Flow Non-Uniformity and Secondary Flow Characteristics Within a Serpentine Cooling Channel of a Realistic Gas Turbine Blade	6
Exploring Topology Optimization for High Pressure Turbine Blade Tips	6
Higher Order Conceptual Model for Labyrinth Seal Flutter	6
Understanding Capacity Sensitivity of Cooled Transonic Nozzle Guide Vanes: A Parametric Experimental and Computational Study of the Impact of Trailing Edge Geometry	6
Influence of Purge Flow Injection on the Performance of an Axial Turbine With Three-Dimensional Airfoils and Non-Axisymmetric Endwall Contouring	6
The Impact of Various Modeling Decisions on Flow Field Predictions in a Centrifugal Compressor	6
Effect of Axial Casing Groove Geometry on Rotor-Groove Interactions in the Tip Region of a Compressor	6
Experimental Investigation Into the Effect of a Ceramic Matrix Composite Surface on Film Cooling	5
Loss Analysis of Cavity Leakage Flow in a Compressor Cascade	5
Ice-Crystal Icing Investigation on a Honeywell Uncertified Research Engine in an Altitude Simulation Icing Facility	5
Numerical Investigation of the Fan Flutter Mechanism Related to Acoustic Propagation Characteristics	5
Aerodynamic Performance and Leakage Flow in Turbine Cascades With Sweeping Jet Actuators	5
Aerothermal Effect of Cavity Welding Beads on a Transonic Squealer Tip	5
Effect of a Ceramic Matrix Composite Surface on Film Cooling	5
Aerodynamic Influence of a Bleed on the Last Stage of a Low-Pressure Compressor and S-Duct	5
Experimental Study of the Endwall Heat Transfer of a Transonic Nozzle Guide Vane With Upstream Jet Purge Cooling Part 1—Effect of Density Ratio	5
High-Fidelity Computational Fluid Dynamics Analysis of In-Serviced Shrouded High-Pressure Turbine Rotor Blades	5
Numerical and Experimental Aerodynamic Investigation of an S-Shaped Intermediate Compressor Duct With Bleed	5

Analysis of Transonic Bladerows With Non-Uniform Geometry Using the Spectral Method	5
The Effects of Specific Heat and Viscosity on Film Cooling Behavior	5
Experiment-Based Preliminary Design Guidelines for Consideration of Profile Vortex Shedding From Low-Speed Axial Fan Blades	5
A Fluid–Structure Interaction Tool Using a Van der Pol-Based Reduced-Order Model for Buffet and Nonsynchronous Vibrations	5
The Effect of Gas and Surface Temperature on Cold-Side and Hot-Side Turbine Deposition	5
Investigation on Flow Characteristics and Its Effect on Heat Transfer Enhancement in a Wide Channel With Staggered Diamond-S Pin Fins	5
Application of a Distributed Element Roughness Model to Additively Manufactured Internal Cooling Channels	5
Acoustic Resonance in an Axial Multistage Compressor Leading to Non-Synchronous Blade Vibration	5
Profile Loss Reduction of High-Lift Turbine Blades With Rough and Ribbed Surfaces	5
The Effect of Gapping on Compressor Performance	5
Experimental and Numerical Study of Heat Transfer and Pressure Loss in a Swirl Multi-Pass Channel With Convergent Jet Slots	5
Effects of Upstream Wakes on the Boundary Layer Over a Low-Pressure Turbine Blade	5
Design of a Tip Appendage for the Control of Tip Leakage Vortices in Axial Flow Fans	5
Experimental Study of Vaneless Diffuser Rotating Stall Development and Cell-Merging Phenomena	5
Investigating Gas Turbine Internal Cooling Using Supercritical CO2 at Higher Reynolds Numbers for Direct Fired Cycle Applications	5
Analysis of the Heat Transfer Within Combustor Liners Using a Combined Monte Carlo and Two-Flux Method	5
The Effects of Swirling Flows in Entropy Wave Convection Through High-Pressure Turbine Stage	5
Super Aggressive S-Ducts for Air Breathing Rocket Engines	5
AN EXPERIMENTALLY VALIDATED LOW ORDER MODEL OF THE THERMAL RESPONSE OF DOUBLE-WALL EFFUSION COOLING SYSTEMS FOR HP TURBINE BLADES	5
Impact of Turbine-Strut Clocking on the Performance of a Turbine Center Frame	5
Deficiencies in the Spalart–Allmaras Turbulence Model for the Prediction of the Stability Boundary in Highly Loaded Compressors	5
Experimental Study of Turbulent Flow and Heat Transfer Behaviors Over a Micro-Rib-Dimple-Structured Surface	5
Aeroelastic Aspects of Axial Compressor Stage With Self-Recirculating Casing Treatment	5
Application of an Immersed Boundary Method on an Instrumented Turbine Blade With Large Eddy Simulation	5
Stator Blades Manufacturing Geometrical Variability in Axial Compressors and Impact on the Aeroelastic Excitation Forces	5
Effective Clearance and Differential Gapping Impact on Seal Flutter Modeling and Validation	4
The Role of Turbine Operating Conditions on Combustor–Turbine Interaction—Part I: Change in Expansion Ratio	4
Formation of High-Temperature Minerals From an Evaporite-Rich Dust in Gas Turbine Engine Ingestion Tests	4
Evaluating the Effects of Transient Purge Flow on Stator-Rotor Seal Performance	4
Zonal Detached Eddy Simulation of the Fan-Outlet Guide Vanes Stage of a Turbofan Engine: Part II—Broadband Noise Predictions	4
A New Experimental Approach for Heat Transfer Coefficient and Adiabatic Wall Temperature Measurements on a Nozzle Guide Vane With Inlet Temperature Distortions	4
Unsteady Analysis of Heat Transfer Coefficient Distribution in a Static Ribbed Channel for An Established Flow	4
Influence of Vane Trailing Edge Flow on the Formation of Cavity Cells and Rim Sealing	4
Characterization of an Apparatus to Study Solid Deposit Formation in Lubricating Oils at High Temperatures	4
Numerical Investigations on Effect of Inflow Parameters on Development of Secondary Flow Field for Linear Low-Pressure Turbine Cascade	4
Adiabatic Effectiveness and Thermal Field Measurements of a Shaped Hole in the Showerhead of a Model Turbine Blade	4
Effect of Upstream Leakage Flow on Film Cooling Characteristic of a Turbine Convex Endwall	4
Generalized Predictions of Particle-Vane Retention Probability in Gas Turbine Engines	4
Numerical Predictions of Turbine Cascade Secondary Flows and Heat Transfer With Inflow Turbulence	4
Convection in Scaled Turbine Internal Cooling Passages With Additive Manufacturing Roughness	4
The Unsteady Topology of Corner Separations	4
Numerical Investigations on the Rotating Stall in an Axial Compressor and Its Control by Flow Injection at Casing	4
Low Rank Education of Cascade Loss Sensitivity to Unsteady Parameters by Proper Orthogonal Decomposition	4
Effects of Cooling Configurations on the Aerothermal Performance of a Turbine Endwall With Jet Impingement and Film Cooling	4
Large-Eddy Simulation of Variable Speed Power Turbine Cascade With Inflow Turbulence	4
Leakage Flow Impact on Shrouded Stator Cavity Flow Topology and Associated High-Speed Axial Compressor Stage Performance	4
Computational and Experimental Study of Film-Cooling Effectiveness With and Without Downstream Vortex Generators	4
Heat Transfer Measurements Using Multiple Thermochromic Liquid Crystals in Symmetric Cooling Channels	4
Enhancing Turbine Deposition Prediction Capability With Conjugate Mesh Morphing	4
Uncertainty Quantification on the Cooling Performance of a Transonic Turbine Vane With Upstream Endwall Misalignment	4
Experimental Study of Outflow Effects in a Rotating Turbulated Channel	4
Aero-Thermal Aspects of Film Cooled Nozzle Guide Vane Endwall—Part 2: Thermal Measurements	4
Influence of Boundary Layer Skew on the Tip Leakage Vortex of an Axial Compressor Stator	4
The Effect of Blade Count on Body Force Model Performance for Axial Fans	4
Dynamics of Shock Waves Interacting With Laminar Separated Transonic Turbine Flow Investigated by High-Speed Schlieren and Surface Hot-Film Sensors	4
Effect of the Honeycomb Tip With Injection on the Aerodynamic Performance in a 1.5-Stage Turbine	4
Improved Prediction of Losses With Large Eddy Simulation in a Low-Pressure Turbine	4
Thermal Performance of Double-Sided, Partial Height Strip Fin Arrays in a High Aspect Ratio, Rectangular Channel	4
Stress-Blended Eddy Simulation/Flamelet Generated Manifold Simulation of Film-Cooled Surface Heat Transfer and Near-Wall Reaction	4
The Role of Endwall Shape Optimization in the Design of Supersonic Turbines for Rotating Detonation Engines	4
Low Reynolds Number Effects on the Endwall Flow Field in a High-Lift Turbine Passage	4
Numerical Assessment of Density Ratio and Mainstream Turbulence Effects on Leading-Edge Film Cooling: Heat and Mass Transfer Methods	4
A Method for Predicting the Aeroelastic Response of Radial Turbomachines	4
Analysis of Turbomachinery Averaging Techniques	4
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	4
Mitigation of Boundary Layer Ingestion Circumferential Distortion Using Nonaxisymmetric Fan Exit Guide Vanes	4
Vane–Probe Interactions in Transonic Flows	4
Improving the Film Cooling Performance of a Turbine Endwall With Multi-Fidelity Modeling Considering Conjugate Heat Transfer	4
Heat Transfer Coefficient Augmentation for a Shaped Film Cooling Hole at a Range of Compound Angles	4
Unsteady Flow Structure of Corner Separation in a Highly Loaded Compressor Cascade	4
Numerical and Experimental Investigation of the Reynolds Number and Reduced Frequency Effects on Low-Pressure Turbine Airfoils	4
Film Cooling Effectiveness on Pressure Surface and Suction Surface of Turbine Guide Vane With Diffusion Slot Holes	4
A Simplified Method for the Deposition Rate Assessment on the Vanes of a Multistage Axial-Flow Compressor	4
Experimental Investigation of the Pre-Stall and Stall Evolution in a Centrifugal Compressor With a Volute	4
Volumetric Velocimetry Measurements of Purge–Mainstream Interaction in a One-Stage Turbine	4
Loss Characterization of Advanced VIGV Configurations With Adjustable Blade Geometry	4
Effect of Tip Vortex Reduction on Air-Cooled Condenser Axial Flow Fan Performance: An Experimental Investigation	4
Numerical Model of a Deep Surge Cycle in Low-Speed Centrifugal Compressor	4
Roughness-Resolved Large-Eddy Simulation of Additive Manufacturing-Like Channel Flows	4
Experimental Study of Impact of In-Service Deterioration on Thermal Performance of High-Pressure Nozzle Guide Vanes	4
Heat Transfer and Pressure Loss in a Two-Pass, Rectangular Channel Featuring a Reduced Cross-Sectional Area After the 180-Deg Tip Turn With Different Turning Vane Configurations	4
Experimental and Computational Investigation of an Advanced Casing Treatment in a Single-Stage High-Speed Compressor	4
LES-CHT for a Rotating Cavity With Axial Throughflow	4
Effects of Axial Casing Grooves on the Structure of Turbulence in the Tip Region of an Axial Turbomachine Rotor	4
A Data-Driven Tip Flow Loss Prediction Method for a Transonic Fan Under Boundary Layer Ingesting Inflow Distortion	4