Journal of Turbomachinery-Transactions of the Asme

Article	Citations
Tailoring Surface Roughness Using Additive Manufacturing to Improve Internal Cooling	27
Effect of a Combined Hot-Streak and Swirl Profile on Cooled 1.5-Stage Turbine Aerodynamics: An Experimental and Computational Study	25
The Role of Turbomachinery Performance in the Optimization of Supercritical Carbon Dioxide Power Systems	24
The Effect of Isentropic Exponent on Transonic Turbine Performance	22
Experimental and Computational Methods for the Evaluation of Double-Wall, Effusion Cooling Systems	22
Scaling Flat-Plate, Low-Temperature Adiabatic Effectiveness Results Using the Advective Capacity Ratio	19
Detached Eddy Simulation: Recent Development and Application to Compressor Tip Leakage Flow	17
Effect of Purge on the Secondary Flow-Field of a Gas Turbine Blade-Row	16
Experimental and Numerical Analysis of Additively Manufactured Inconel 718 Coupons With Lattice Structure	15
Aerodynamics of Boundary Layer Ingesting Fuselage Fans	15
Rapid Estimate of Wind Turbine Energy Loss Due to Blade Leading Edge Delamination Using Artificial Neural Networks	15
Impact of Additive Manufacturing on Internal Cooling Channels With Varying Diameters and Build Directions	14
Computational and Experimental Study of Hot Streak Transport Within the First Stage of a Gas Turbine	14
Integration of Machine Learning and Computational Fluid Dynamics to Develop Turbulence Models for Improved Low-Pressure Turbine Wake Mixing Prediction	14
Experimental Study on Aerodynamic Loss and Heat Transfer for Various Squealer Tips	14
Optimization of Slots-Groove Coupled Casing Treatment for an Axial Transonic Compressor	13
Effect of Manufacturing Tolerance in Flow Past a Compressor Blade	13
Inlet Flow Distortion in an Advanced Civil Transport Boundary Layer Ingesting Engine Installation	13
Experimental Study of Oscillating Freestream Effect on the Spatiotemporal Distributions of Leading-Edge Film Cooling	12
Adiabatic Effectiveness Measurements for a Baseline Shaped Film Cooling Hole	12
Statistical Error Estimation Methods for Engineering-Relevant Quantities From Scale-Resolving Simulations	12
Experimental Investigation of Innovative Cooling Schemes on an Additively Manufactured Engine Scale Turbine Nozzle Guide Vane	12
Study of Relative Endwall Motion Effects in a Compressor Cascade Through Direct Numerical Simulations	12
Scaling Considerations for Thermal and Pressure-Sensitive Paint Methods Used to Determine Adiabatic Effectiveness	12
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

Prestall Instability in Axial Flow Compressors	12
Multidisciplinary Design Optimization for Performance Improvement of an Axial Flow Fan Using Free-Form Deformation	12
Using a New Entropy Loss Analysis to Assess the Accuracy of RANS Predictions of an High-Pressure Turbine Vane	11
Large-Eddy Simulations of High Rossby Number Flow in the High-Pressure Compressor Inter-Disk Cavity	11
Comparison of Thin Film Heat Flux Gauge Technologies Emphasizing Continuous-Duration Operation	11
Fan Aerodynamics With a Short Intake at High Angle of Attack	11
Investigation of Endwall Heat Transfer in Staggered Pin Fin Arrays	11
Effect of Tip Clearance on Rotating Stall in a Mixed-Flow Pump	11
Pulsed Suction Control in a Highly Loaded Compressor Cascade With Low Suction Flowrates	11
Global Optimization of a Transonic Fan Blade Through AI-Enabled Active Subspaces	11
Surface Curvature Effects on Film Cooling Performance for Shaped Holes on a Model Turbine Blade	11
Flow in a Simulated Turbine Blade Cooling Channel With Spatially Varying Roughness Caused by Additive Manufacturing Orientation	11
Counter-Propagating Rotating Stall of Vaned Diffuser in a Centrifugal Compressor Near Design Condition	11
Uncertainty Quantification of Aero-Thermal Performance of a Blade Endwall Considering Slot Geometry Deviation and Mainstream Fluctuation	11
High Dimensional Matching Optimization of Impeller–Vaned Diffuser Interaction for a Centrifugal Compressor Stage	10
Interpretation of Stall Precursor Signatures	10
Thermal Optimization of Air Foil Thrust Bearings Using Different Foil Materials	10
Active Flow Control Utilizing an Adaptive Blade Geometry and an Extremum Seeking Algorithm at Periodically Transient Boundary Conditions	10
Unsteady Structure of Compressor Tip Leakage Flows	10
Computational and Experimental Study of the Unsteady Convection of Entropy Waves Within a High-Pressure Turbine Stage	10
Fully Coupled Large Eddy Simulation-Conjugate Heat Transfer Analysis of a Ribbed Cooling Passage Using the Immersed Boundary Method	10
Flow Physics During Surge and Recovery of a Multi-Stage High-Speed Compressor	9
Comparisons of Endwall Overall Effectiveness From Two Film Hole Distribution Patterns at Low and High Exit Mach Numbers	9
On High-Resolution Pressure Amplitude and Phase Measurements Comparing Fast-Response Pressure Transducers and Unsteady Pressure-Sensitive Paint	9
Upstream Film Cooling on the Contoured Endwall of a Transonic Turbine Vane in an Annular Cascade	9
Development, Validation, and Application of an Optimization Scheme for Impellers of Centrifugal Fans Using Computational Fluid Dynamics-Trained Metamodels	9
Metamodel-Driven Data Mining Model to Support Three-Dimensional Design of Centrifugal Compressor Stage	9
Foam-Metal Casing Treatment on an Axial Flow Compressor: Stability Improvement and Noise Reduction	9
Experimental and Numerical Study of the Turbulent Flow and Heat Transfer in a Wedge-Shaped Channel With Guiding Pin Fin Arrays Under Rotating Conditions	9
Effect of 45-deg Rib Orientations on Heat Transfer in a Rotating Two-Pass Channel With Aspect Ratio from 4:1 to 2:1	9
Modeling the Transient Behavior of Gas Turbines	9
The Impact of Combustor Turbulence on Turbine Loss Mechanisms	9
Optimization of Turbine Cascade Squealer Tip Cooling Design by Combining Shaping and Flow Injection	8
Surface Roughness Impact on Boundary Layer Transition and Loss Mechanisms Over a Flat-Plate Under a Low-Pressure Turbine Pressure Gradient	8
A Novel Multi-Stage Impingement Cooling Scheme—Part II: Design Optimization	8
A Comparison of Turbulence Levels From Particle Image Velocimetry and Constant Temperature Anemometry Downstream of a Low-Pressure Turbine Cascade at High-Speed Flow Conditions	8
Transonic Turbine Vane Endwall Film Cooling Using the Pressure-Sensitive Paint Measurement Technique	8
A Novel Multi-Stage Impingement Cooling Scheme—Part I: Concept Study	8
Experimental Investigation on Cooling Performance of Impingement–Effusion Full Coverage Film on Suction Surface of a Vane	8
Heat Transfer Characteristics Within the Matrix Cooling Channels	8
Extending Highly Loaded Axial Fan Operability Range Through Novel Blade Design	8
Understanding of Secondary Flows and Losses in Radial and Mixed Flow Turbines	8
Uncertainty Evaluation on Multi-Hole Aerodynamic Pressure Probes	8
Effect of Radiation on Heat Transfer Inside Aeroengine Compressor Rotors	8
Heat Transfer in a Rotating, Two-Pass, Variable Aspect Ratio Cooling Channel With Profiled V-Shaped Ribs	8
An Efficient Aeroelastic Eigenvalue Method for Analyzing Coupled-Mode Flutter in Turbomachinery	7
Investigation of Riblet Geometry and Start Locations of Herringbone Riblets on Pressure Losses in a Linear Cascade at Low Reynolds Numbers	7
DEVELOPMENT OF A LIFETIME PRESSURE SENSITIVE PAINT PROCEDURE FOR HIGH-PRESSURE VANE TESTING	7
Endwall Heat Transfer and Cooling Performance of a Transonic Turbine Vane With Upstream Injection Flow	7
Study on Effects of Spanwise-Expansion Parameters on Film Cooling Effectiveness of Diffusion Shaped Hole Configurations	7

Pulsed Impingement Turbine Cooling and Its Effect on the Efficiency of Gas Turbines With Pressure Gain Combustion	7
Numerical Investigation of Effects of Blockage, Inclination Angle, and Hole-Size on Film Cooling Effectiveness at Concave Surface	7
Acquisition and Processing Considerations for Infrared Images of Rotating Turbine Blades	7
Machine Learning for the Development of Data-Driven Turbulence Closures in Coolant Systems	7
Direct and Inverse Model for Single-Hole Film Cooling With Machine Learning	7
Analysis of the Unsteady Flow Field Inside a Fan-Shaped Cooling Hole Predicted by Large Eddy Simulation	7
Investigation of Unsteady Rotor–Stator Interaction and Deterministic Correlation Analysis in a Transonic Compressor Stage	7
The Impact of Manufacturing Variations on Performance of a Transonic Axial Compressor Rotor	7
Efficiency Scaling: Influence of Reynolds and Mach Numbers on Fan Performance	7
Effect of Differential Tip Clearance on the Performance of a Tandem Rotor	7
Eddy Resolving Strategies in Turbomachinery and Peripheral Components	7
Single and Multiple Circumferential Casing Groove for Stall Margin Improvement in a Transonic Axial Compressor	7
Development and Validation of a Model for Centrifugal Compressors in Reversed Flow Regimes	7
Scalar Diffusion Equation-Based Model to Predict 2-Dimensional Film Cooling Effectiveness of a Shaped Hole	7
Free-Stream Turbulence-Induced Boundary-Layer Transition in Low-Pressure Turbines	7
A Detailed Loss Analysis Methodology for Centrifugal Compressors	7
Analysis Method of Nonsynchronous Vibration and Influence of Tip Clearance Flow Instabilities on Nonsynchronous Vibration in an Axial Transonic Compressor Rotor	7
Analysis of the Loss Production Mechanism Due to Cavity–Main Flow Interaction in a Low-Pressure Turbine Stage	6
Instabilities Everywhere! Hard Problems in Aero-Engines	6
Infrared Temperature Measurements of the Blade Tip for a Turbine Operating at Corrected Engine Conditions	6
Averaging for High Fidelity Modeling—Toward Large Eddy Simulations in Multi-Passage Multi-Row Configurations	6
Experimental Study on the Influence of Film Cooling Hole Extraction on Heat Transfer and Flow Field in Internal Ribbed Cooling Channels of Turbine Blades	6
Estimation of Aircraft Engine Flight Mission Severity Caused by Erosion	6
Plume Model for Buoyancy-Induced Flow and Heat Transfer in Closed Rotating Cavities	6
Aerodynamic Effects of an Incoming Vortex on Turbines With Different Tip Geometries	6
Effects of Inlet Guide Vanes on the Performance and Stability of an Aeronautical Centrifugal Compressor	6
The Effects of Reynolds Number on the Stall and Pre-Stall Behavior of Compact Axial Compressors	6
NASA's Role in Gas Turbine Technology Development: Accelerating Technical Progress Via Collaboration Between Academia, Industry, and Government Agencies	6
Understanding Capacity Sensitivity of Cooled Transonic Nozzle Guide Vanes: A Parametric Experimental and Computational Study of the Impact of Trailing Edge Geometry	6
Computer 3D Vision-Aided Full-3D Optimization of a Centrifugal Impeller	6
Analysis of Averaging Methods for Nonuniform Total Pressure Fields	6
High-Fidelity Simulations of a High-Pressure Turbine Vane Subject to Large Disturbances: Effect of Exit Mach Number on Losses	6
Accurate Prediction of Loss Using High Fidelity Methods	6
Experimental and Computational Investigation of Integrated Internal and Film Cooling Designs Incorporating a Thermal Barrier Coating	6
Physical Mechanisms Investigation of Sharkskin-Inspired Compressor Cascade Based on Large Eddy Simulations	6
Low Reynolds Number Effects on the Separation and Wake of a Compressor Blade	6
A Robust Implementation of a Reynolds Stress Model for Turbomachinery Applications in a Coupled Solver Environment	6
Innovative Design, Structural Optimization, and Additive Manufacturing of New-Generation Turbine Blades	6
Heat Transfer in a Rotating, Blade-Shaped, Two-Pass Cooling Channel With a Variable Aspect Ratio	6
The Development and Applications of a Loading Distribution Based Tip Leakage Loss Model for Unshrouded Gas Turbines	6
Investigations Into Heat Transfer and Aerodynamic Performance of a Worn Squealer Tipped Turbine Stage	6
Aerodynamic Investigation of a Composite Low-Speed Fan for UHBR Application	6
Application of Multiscale Methodology for Transonic Turbine Blade Tip Cooling Design	6
Uncertainty Quantification of Spalart–Allmaras Turbulence Model Coefficients for Compressor Stall	6
Evaluating the Effect of Vane Trailing Edge Flow on Turbine Rim Sealing	6
Modeling of Axial Compressor With Large Tip Clearances	6
Sweeping Jet Film Cooling at High Blowing Ratio on a Turbine Vane	6
Time-Resolved Flow Field Analysis of Effusion Cooling System With Representative Swirling Main Flow	6
Higher Order Conceptual Model for Labyrinth Seal Flutter	6
Casing Treatment: Its Potential and Limitations	5
A Deep Insight Into the Transonic Flow of an Advanced Centrifugal Compressor Design	5
The Effects of Specific Heat and Viscosity on Film Cooling Behavior	5
Investigating Gas Turbine Internal Cooling Using Supercritical CO2 at Higher Reynolds Numbers for Direct Fired Cycle Applications	5
Impacts of Pin Fin Shape and Spacing on Heat Transfer and Pressure Losses	5
Non-Dimensional Parameters for Comparing Conventional and Counter-Rotating Turbomachines	5
Evaluation of Turbulent Spot Production Rate in Boundary Layers Under Variable Pressure Gradients for Gas Turbine Applications	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
Effect of Boundary Layer Suction on the Corner Separation in a Highly Loaded Axial Compressor Cascade	5
Heat Transfer and Pressure Loss of Additively Manufactured Internal Cooling Channels With Various Shapes	5
Impact of Turbine-Strut Clocking on the Performance of a Turbine Center Frame	5
Stratified and Buoyancy-Induced Flow in Closed Compressor Rotors	5
The Impact of Various Modeling Decisions on Flow Field Predictions in a Centrifugal Compressor	5
Unsteady Lattice Boltzmann Simulations of Corner Separation in a Compressor Cascade	5
Azimuthal Mode Characteristics of Rotating Instability in Axial Compressor Using Compressed Sensing Method	5
Experimental and Numerical Analysis of Loss Characteristics of Cooled Transonic Nozzle Guide Vanes	5
Effects of Jet Impingement on Convective Heat Transfer in Effusion Holes	5
Impact of Exit Duct Dynamic Response on Compressor Stability	5
Microstructure of IN738LC Fabricated Using Laser Powder Bed Fusion Additive Manufacturing	5
Stall Margin Improvement in a Transonic Compressor With a Casing Treatment: Flow Mechanism	5
Heat Transfer Measurements for Array Jet Impingement With Castellated Wall	5
Super Aggressive S-Ducts for Air Breathing Rocket Engines	5
Vortex Tracking of Purge-Mainstream Interactions in a Rotating Turbine Stage	5
Numerical and Experimental Aerodynamic Investigation of an S-Shaped Intermediate Compressor Duct With Bleed	5
Deficiencies in the Spalart–Allmaras Turbulence Model for the Prediction of the Stability Boundary in Highly Loaded Compressors	5
Heat Transfer in Rotating, Trailing-Edge, Converging Channels With Smooth Walls and Pin-Fins	5
Blade Envelopes Part I: Concept and Methodology	5
Design of a Tip Appendage for the Control of Tip Leakage Vortices in Axial Flow Fans	5
Experimental Heat Transfer and Boundary Layer Measurements on a Ceramic Matrix Composite Surface	5
Volumetric Velocimetry Measurements of Purge–Mainstream Interaction in a One-Stage Turbine	5
Experiment-Based Preliminary Design Guidelines for Consideration of Profile Vortex Shedding From Low-Speed Axial Fan Blades	5

Ice-Crystal Icing Investigation on a Honeywell Uncertified Research Engine in an Altitude Simulation Icing Facility	5
Impacts of Tandem Configurations on the Aerodynamic Performance of an Axial Supersonic Through-Flow Fan Cascade	5
Comparative Study of Tip Injection in a Transonic and Subsonic Compressor	5
Application of Advanced RANS Turbulence Models for the Prediction of Turbomachinery Flows	5
Aerodynamic Influence of a Bleed on the Last Stage of a Low-Pressure Compressor and S-Duct	5
Aeroelastic Aspects of Axial Compressor Stage With Self-Recirculating Casing Treatment	5
Aero-Thermal Aspects of Film Cooled Nozzle Guide Vane Endwall—Part 1: Aerodynamics	5
Application of an Immersed Boundary Method on an Instrumented Turbine Blade With Large Eddy Simulation	5
Modeling Axisymmetric Centrifugal Compressor Characteristics From First Principles	5
Effect of Coolant Crossflow on Film Cooling Effectiveness of Diffusion Slot Hole With and Without Ribs	5
Aerodynamic Loading Considerations of Three-Shaft Engine Compression System During Surge	5
Computational and Experimental Study of Film-Cooling Effectiveness With and Without Downstream Vortex Generators	4
AN EXPERIMENTALLY VALIDATED LOW ORDER MODEL OF THE THERMAL RESPONSE OF DOUBLE-WALL EFFUSION COOLING SYSTEMS FOR HP TURBINE BLADES	4
Loss Analysis of Unsteady Turbomachinery Flows Based on the Mechanical Work Potential	4
Low Rank Education of Cascade Loss Sensitivity to Unsteady Parameters by Proper Orthogonal Decomposition	4
The Role of Turbine Operating Conditions on Combustor–Turbine Interaction—Part I: Change in Expansion Ratio	4
Experimental Study of Vaneless Diffuser Rotating Stall Development and Cell-Merging Phenomena	4
Effect of Axial Casing Groove Geometry on Rotor-Groove Interactions in the Tip Region of a Compressor	4
Analysis of Transonic Bladerows With Non-Uniform Geometry Using the Spectral Method	4
Reconstructing Compressor Non-Uniform Circumferential Flow Field From Spatially Undersampled Data—Part 1: Methodology and Sensitivity Analysis	4
Characterization of an Apparatus to Study Solid Deposit Formation in Lubricating Oils at High Temperatures	4
Unsteady Analysis of Heat Transfer Coefficient Distribution in a Static Ribbed Channel for An Established Flow	4
Exploring Applicability of Acoustic Heat Transfer Enhancement Across Various Perturbation Elements	4
Evaluating the Use of Leaned Stator Vanes to Produce a Non-Uniform Flow Distribution Across the Inlet Span of a Mixed Flow Turbine Rotor	4
Wall Temperature Measurements in a Full-Scale Gas Turbine Combustor Test Rig With Fiber Coupled Phosphor Thermometry	4
Large-Eddy Simulation of Variable Speed Power Turbine Cascade With Inflow Turbulence	4
Forced Response Due to Vane Stagger Angle Variation in an Axial Compressor	4
Experimental and Numerical Study of Heat Transfer and Pressure Loss in a Swirl Multi-Pass Channel With Convergent Jet Slots	4
A Method for Predicting the Aeroelastic Response of Radial Turbomachines	4
Investigation of Tip Leakage Vortex Breakdown in a High-Speed Multistage Axial Compressor	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
Effective Clearance and Differential Gapping Impact on Seal Flutter Modeling and Validation	4
Aerothermal Optimization of Turbine Squealer Tip Geometries With Arbitrary Cooling Injection	4
Experimental and Numerical Investigation of High Load Turbine Blade Tip Cavity Structures	4
A Simplified Method for the Deposition Rate Assessment on the Vanes of a Multistage Axial-Flow Compressor	4
Automatic Design Optimization of a Transonic Compressor Rotor for Improving Aeroacoustic and Aerodynamic Performance	4
Influence of Boundary Layer Skew on the Tip Leakage Vortex of an Axial Compressor Stator	4
Heat Transfer Measurements Using Multiple Thermochromic Liquid Crystals in Symmetric Cooling Channels	4
Impact of Varying High- and Low-Pressure Turbine Purge Flows on a Turbine Center Frame and Low-Pressure Turbine System	4
Stall Behavior in an Ultrahigh-Pressure-Ratio Centrifugal Compressor: Backward-Traveling Rotating Stall	4
Analysis of the Heat Transfer Within Combustor Liners Using a Combined Monte Carlo and Two-Flux Method	4
Enhancing Turbine Deposition Prediction Capability With Conjugate Mesh Morphing	4
Numerical and Experimental Investigation of the Reynolds Number and Reduced Frequency Effects on Low-Pressure Turbine Airfoils	4
High-Fidelity Simulations of Multi-Jet Impingement Cooling Flows	4
Stress-Blended Eddy Simulation/Flamelet Generated Manifold Simulation of Film-Cooled Surface Heat Transfer and Near-Wall Reaction	4
The Effect of Gapping on Compressor Performance	4
Experimental Investigation of Film Cooling Performance on Blade Endwall With Diffusion Slot Holes and Stator–Rotor Purge Flow	4
Effects of Cooling Configurations on the Aerothermal Performance of a Turbine Endwall With Jet Impingement and Film Cooling	4
Experimental Study of Impact of In-Service Deterioration on Thermal Performance of High-Pressure Nozzle Guide Vanes	4
Flow Non-Uniformity and Secondary Flow Characteristics Within a Serpentine Cooling Channel of a Realistic Gas Turbine Blade	4
Large Eddy Simulation of Heat Transfer Within a Multi-Perforation Synthetic Jets Configuration	4
Leakage Flow Impact on Shrouded Stator Cavity Flow Topology and Associated High-Speed Axial Compressor Stage Performance	4
Experimental and Numerical Quantification of the Aerodynamic Damping of a Turbine Blisk	4
On the Importance of Transition Control at Transonic Compressor Blades	4
Analysis of the Honeywell Uncertified Research Engine With Ice Crystal Cloud Ingestion at Simulated Altitudes	4
Zonal Detached Eddy Simulation of the Fan-Outlet Guide Vanes Stage of a Turbofan Engine: Part II—Broadband Noise Predictions	4
Performance Improvement of Turbofans by Electric Power Transfer	4
Impacts of the Additive Manufacturing Process on the Roughness of Engine Scale Vanes and Cooling Channels	4
Evaluating the Effects of Transient Purge Flow on Stator-Rotor Seal Performance	4
The Effect of Step Misalignment on Purge Flow Cooling of Nozzle Guide Vane at Transonic Conditions	4
Dynamics of Shock Waves Interacting With Laminar Separated Transonic Turbine Flow Investigated by High-Speed Schlieren and Surface Hot-Film Sensors	4
The Effect of Gas and Surface Temperature on Cold-Side and Hot-Side Turbine Deposition	4
Loss Analysis of Cavity Leakage Flow in a Compressor Cascade	4
Turbine Endwall Contouring Through Advanced Optimization Techniques	4
Effect of Tip Vortex Reduction on Air-Cooled Condenser Axial Flow Fan Performance: An Experimental Investigation	4
Effects of Axial Casing Grooves on the Structure of Turbulence in the Tip Region of an Axial Turbomachine Rotor	4
Numerical Predictions of Turbine Cascade Secondary Flows and Heat Transfer With Inflow Turbulence	4
The Effects of Swirling Flows in Entropy Wave Convection Through High-Pressure Turbine Stage	4
Numerical Assessment of Density Ratio and Mainstream Turbulence Effects on Leading-Edge Film Cooling: Heat and Mass Transfer Methods	4
Zonal Detached Eddy Simulation of the Fan-Outlet Guide Vanes Stage of a Turbofan Engine: Part I—Methodology, Numerical Setup, and Aerodynamic Analysis	4