Journal of Turbomachinery-Transactions of the Asme

Article	Citations
Tailoring Surface Roughness Using Additive Manufacturing to Improve Internal Cooling	26
Effect of a Combined Hot-Streak and Swirl Profile on Cooled 1.5-Stage Turbine Aerodynamics: An Experimental and Computational Study	24
The Role of Turbomachinery Performance in the Optimization of Supercritical Carbon Dioxide Power Systems	23
The Effect of Isentropic Exponent on Transonic Turbine Performance	21
Experimental and Computational Methods for the Evaluation of Double-Wall, Effusion Cooling Systems	20
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
Analysis of the Thermomechanical Stresses in Double-Wall Effusion Cooled Systems	17
Experimental and Numerical Analysis of Additively Manufactured Inconel 718 Coupons With Lattice Structure	15
Effect of Purge on the Secondary Flow-Field of a Gas Turbine Blade-Row	15
Rapid Estimate of Wind Turbine Energy Loss Due to Blade Leading Edge Delamination Using Artificial Neural Networks	15
Aerodynamics of Boundary Layer Ingesting Fuselage Fans	14
Impact of Additive Manufacturing on Internal Cooling Channels With Varying Diameters and Build Directions	14
Optimization of Slots-Groove Coupled Casing Treatment for an Axial Transonic Compressor	13
Inlet Flow Distortion in an Advanced Civil Transport Boundary Layer Ingesting Engine Installation	13
A Computational Technique to Evaluate the Relative Influence of Internal and External Cooling on Overall Effectiveness	13
Computational and Experimental Study of Hot Streak Transport Within the First Stage of a Gas Turbine	13
Experimental Study on Aerodynamic Loss and Heat Transfer for Various Squealer Tips	13
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
Effect of Manufacturing Tolerance in Flow Past a Compressor Blade	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
Study of Relative Endwall Motion Effects in a Compressor Cascade Through Direct Numerical Simulations	12
Validation Studies of Linear Oscillating Compressor Cascade and Use of Influence Coefficient Method	12

Integration of Machine Learning and Computational Fluid Dynamics to Develop Turbulence Models for Improved Low-Pressure Turbine Wake Mixing Prediction	12
Effect of Additive Manufacturing Process Parameters on Turbine Cooling	12
Investigation of Endwall Heat Transfer in Staggered Pin Fin Arrays	11
Comparison of Thin Film Heat Flux Gauge Technologies Emphasizing Continuous-Duration Operation	11
Counter-Propagating Rotating Stall of Vaned Diffuser in a Centrifugal Compressor Near Design Condition	11
Multidisciplinary Design Optimization for Performance Improvement of an Axial Flow Fan Using Free-Form Deformation	11
Experimental Study of Oscillating Freestream Effect on the Spatiotemporal Distributions of Leading-Edge Film Cooling	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
Fan Aerodynamics With a Short Intake at High Angle of Attack	11
Uncertainty Quantification of Aero-Thermal Performance of a Blade Endwall Considering Slot Geometry Deviation and Mainstream Fluctuation	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
Prestall Instability in Axial Flow Compressors	11
Global Optimization of a Transonic Fan Blade Through AI-Enabled Active Subspaces	11
Large-Eddy Simulations of High Rossby Number Flow in the High-Pressure Compressor Inter-Disk Cavity	10
Unsteady Structure of Compressor Tip Leakage Flows	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
Using a New Entropy Loss Analysis to Assess the Accuracy of RANS Predictions of an High-Pressure Turbine Vane	10
Fully Coupled Large Eddy Simulation-Conjugate Heat Transfer Analysis of a Ribbed Cooling Passage Using the Immersed Boundary Method	10
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
On High-Resolution Pressure Amplitude and Phase Measurements Comparing Fast-Response Pressure Transducers and Unsteady Pressure-Sensitive Paint	9
The Impact of Combustor Turbulence on Turbine Loss Mechanisms	9
Computational and Experimental Study of the Unsteady Convection of Entropy Waves Within a High-Pressure Turbine Stage	9
High Dimensional Matching Optimization of Impeller–Vaned Diffuser Interaction for a Centrifugal Compressor Stage	9
Comparisons of Endwall Overall Effectiveness From Two Film Hole Distribution Patterns at Low and High Exit Mach Numbers	9
Foam-Metal Casing Treatment on an Axial Flow Compressor: Stability Improvement and Noise Reduction	9
Flow Physics During Surge and Recovery of a Multi-Stage High-Speed Compressor	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
Upstream Film Cooling on the Contoured Endwall of a Transonic Turbine Vane in an Annular Cascade	9
Performance of Public Film Cooling Geometries Produced Through Additive Manufacturing	9
Adiabatic Effectiveness Measurements for a Baseline Shaped Film Cooling Hole	9
Optimization of Turbine Cascade Squealer Tip Cooling Design by Combining Shaping and Flow Injection	8
Understanding of Secondary Flows and Losses in Radial and Mixed Flow Turbines	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
Experimental and Numerical Study of the Turbulent Flow and Heat Transfer in a Wedge-Shaped Channel With Guiding Pin Fin Arrays Under Rotating Conditions	8
A Novel Multi-Stage Impingement Cooling Scheme—Part I: Concept Study	8
Effect of Radiation on Heat Transfer Inside Aeroengine Compressor Rotors	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
Uncertainty Evaluation on Multi-Hole Aerodynamic Pressure Probes	8
Transonic Turbine Vane Endwall Film Cooling Using the Pressure-Sensitive Paint Measurement Technique	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
Effect of Non-Axisymmetric Endwall Profiling on Heat Transfer and Film Cooling Effectiveness of a Transonic Rotor Blade	7
Scalar Diffusion Equation-Based Model to Predict 2-Dimensional Film Cooling Effectiveness of a Shaped Hole	7
Heat Transfer in a Rotating, Two-Pass, Variable Aspect Ratio Cooling Channel With Profiled V-Shaped Ribs	7
Interpretation of Stall Precursor Signatures	7

An Efficient Aeroelastic Eigenvalue Method for Analyzing Coupled-Mode Flutter in Turbomachinery	7
A Detailed Loss Analysis Methodology for Centrifugal Compressors	7
Efficiency Scaling: Influence of Reynolds and Mach Numbers on Fan Performance	7
Analysis of the Unsteady Flow Field Inside a Fan-Shaped Cooling Hole Predicted by Large Eddy Simulation	7
Study on Effects of Spanwise-Expansion Parameters on Film Cooling Effectiveness of Diffusion Shaped Hole Configurations	7
The Impact of Manufacturing Variations on Performance of a Transonic Axial Compressor Rotor	7
Numerical Investigation of Effects of Blockage, Inclination Angle, and Hole-Size on Film Cooling Effectiveness at Concave Surface	7
Machine Learning for the Development of Data-Driven Turbulence Closures in Coolant Systems	7
Extending Highly Loaded Axial Fan Operability Range Through Novel Blade Design	7
Acquisition and Processing Considerations for Infrared Images of Rotating Turbine Blades	7
Single and Multiple Circumferential Casing Groove for Stall Margin Improvement in a Transonic Axial Compressor	7
Endwall Heat Transfer and Cooling Performance of a Transonic Turbine Vane With Upstream Injection Flow	7
Modeling the Transient Behavior of Gas Turbines	7
Free-Stream Turbulence-Induced Boundary-Layer Transition in Low-Pressure Turbines	7
Analysis Method of Nonsynchronous Vibration and Influence of Tip Clearance Flow Instabilities on Nonsynchronous Vibration in an Axial Transonic Compressor Rotor	7
Eddy Resolving Strategies in Turbomachinery and Peripheral Components	7
Pulsed Impingement Turbine Cooling and Its Effect on the Efficiency of Gas Turbines With Pressure Gain Combustion	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
Investigation of Unsteady Rotor–Stator Interaction and Deterministic Correlation Analysis in a Transonic Compressor Stage	6
Plume Model for Buoyancy-Induced Flow and Heat Transfer in Closed Rotating Cavities	6
Sweeping Jet Film Cooling at High Blowing Ratio on a Turbine Vane	6
Modeling of Axial Compressor With Large Tip Clearances	6
Understanding Capacity Sensitivity of Cooled Transonic Nozzle Guide Vanes: A Parametric Experimental and Computational Study of the Impact of Trailing Edge Geometry	6
Aerodynamic Investigation of a Composite Low-Speed Fan for UHBR Application	6
Infrared Temperature Measurements of the Blade Tip for a Turbine Operating at Corrected Engine Conditions	6
Development and Validation of a Model for Centrifugal Compressors in Reversed Flow Regimes	6
Estimation of Aircraft Engine Flight Mission Severity Caused by Erosion	6
Accurate Prediction of Loss Using High Fidelity Methods	6
Effect of Differential Tip Clearance on the Performance of a Tandem Rotor	6
A Robust Implementation of a Reynolds Stress Model for Turbomachinery Applications in a Coupled Solver Environment	6
Time-Resolved Flow Field Analysis of Effusion Cooling System With Representative Swirling Main Flow	6
NASA's Role in Gas Turbine Technology Development: Accelerating Technical Progress Via Collaboration Between Academia, Industry, and Government Agencies	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
Averaging for High Fidelity Modeling—Toward Large Eddy Simulations in Multi-Passage Multi-Row Configurations	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
Physical Mechanisms Investigation of Sharkskin-Inspired Compressor Cascade Based on Large Eddy Simulations	6
Predicting the Operability of Damaged Compressors Using Machine Learning	6
Heat Transfer in a Rotating, Blade-Shaped, Two-Pass Cooling Channel With a Variable Aspect Ratio	6
Direct and Inverse Model for Single-Hole Film Cooling With Machine Learning	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
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
Ice-Crystal Icing Investigation on a Honeywell Uncertified Research Engine in an Altitude Simulation Icing Facility	5
The Effects of Reynolds Number on the Stall and Pre-Stall Behavior of Compact Axial Compressors	5
Experimental and Computational Investigation of Integrated Internal and Film Cooling Designs Incorporating a Thermal Barrier Coating	5
Super Aggressive S-Ducts for Air Breathing Rocket Engines	5
Heat Transfer Measurements for Array Jet Impingement With Castellated Wall	5
Higher Order Conceptual Model for Labyrinth Seal Flutter	5
Comparative Study of Tip Injection in a Transonic and Subsonic Compressor	5
Instabilities Everywhere! Hard Problems in Aero-Engines	5
Effects of Inlet Guide Vanes on the Performance and Stability of an Aeronautical Centrifugal Compressor	5
Heat Transfer in Rotating, Trailing-Edge, Converging Channels With Smooth Walls and Pin-Fins	5
Deficiencies in the Spalart–Allmaras Turbulence Model for the Prediction of the Stability Boundary in Highly Loaded Compressors	5
Application of an Immersed Boundary Method on an Instrumented Turbine Blade With Large Eddy Simulation	5
Azimuthal Mode Characteristics of Rotating Instability in Axial Compressor Using Compressed Sensing Method	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
Impact of Exit Duct Dynamic Response on Compressor Stability	5
Microstructure of IN738LC Fabricated Using Laser Powder Bed Fusion Additive Manufacturing	5
Application of Advanced RANS Turbulence Models for the Prediction of Turbomachinery Flows	5
Modeling Axisymmetric Centrifugal Compressor Characteristics From First Principles	5
Aeroelastic Aspects of Axial Compressor Stage With Self-Recirculating Casing Treatment	5
Aerodynamic Influence of a Bleed on the Last Stage of a Low-Pressure Compressor and S-Duct	5
Analysis of the Loss Production Mechanism Due to Cavity–Main Flow Interaction in a Low-Pressure Turbine Stage	5
Aerodynamic Effects of an Incoming Vortex on Turbines With Different Tip Geometries	5
Stratified and Buoyancy-Induced Flow in Closed Compressor Rotors	5
Aero-Thermal Aspects of Film Cooled Nozzle Guide Vane Endwall—Part 1: Aerodynamics	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
Casing Treatment: Its Potential and Limitations	5
Experimental and Numerical Analysis of Loss Characteristics of Cooled Transonic Nozzle Guide Vanes	5
Impacts of Pin Fin Shape and Spacing on Heat Transfer and Pressure Losses	5
Investigating Gas Turbine Internal Cooling Using Supercritical CO2 at Higher Reynolds Numbers for Direct Fired Cycle Applications	5
Stall Margin Improvement in a Transonic Compressor With a Casing Treatment: Flow Mechanism	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
Evaluation of Turbulent Spot Production Rate in Boundary Layers Under Variable Pressure Gradients for Gas Turbine Applications	5

Heat Transfer and Pressure Loss of Additively Manufactured Internal Cooling Channels With Various Shapes	5
Effect of Boundary Layer Suction on the Corner Separation in a Highly Loaded Axial Compressor Cascade	5
Blade Envelopes Part I: Concept and Methodology	5
Low Reynolds Number Effects on the Separation and Wake of a Compressor Blade	5
Computer 3D Vision-Aided Full-3D Optimization of a Centrifugal Impeller	5
Impact of Turbine-Strut Clocking on the Performance of a Turbine Center Frame	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
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
Effects of Jet Impingement on Convective Heat Transfer in Effusion Holes	5
Evaluating the Effects of Transient Purge Flow on Stator-Rotor Seal Performance	4
On the Importance of Transition Control at Transonic Compressor Blades	4
Loss Analysis of Unsteady Turbomachinery Flows Based on the Mechanical Work Potential	4
Zonal Detached Eddy Simulation of the Fan-Outlet Guide Vanes Stage of a Turbofan Engine: Part II—Broadband Noise Predictions	4
Impacts of the Additive Manufacturing Process on the Roughness of Engine Scale Vanes and Cooling Channels	4
Design of a Tip Appendage for the Control of Tip Leakage Vortices in Axial Flow Fans	4
Stall Behavior in an Ultrahigh-Pressure-Ratio Centrifugal Compressor: Backward-Traveling Rotating Stall	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
Analysis of the Heat Transfer Within Combustor Liners Using a Combined Monte Carlo and Two-Flux Method	4
Experiment-Based Preliminary Design Guidelines for Consideration of Profile Vortex Shedding From Low-Speed Axial Fan Blades	4
The Effect of Gapping on Compressor Performance	4
Flow Non-Uniformity and Secondary Flow Characteristics Within a Serpentine Cooling Channel of a Realistic Gas Turbine Blade	4
Non-Dimensional Parameters for Comparing Conventional and Counter-Rotating Turbomachines	4
Performance Improvement of Turbofans by Electric Power Transfer	4
Numerical and Experimental Aerodynamic Investigation of an S-Shaped Intermediate Compressor Duct With Bleed	4
Analysis of the Honeywell Uncertified Research Engine With Ice Crystal Cloud Ingestion at Simulated Altitudes	4
Numerical Assessment of Density Ratio and Mainstream Turbulence Effects on Leading-Edge Film Cooling: Heat and Mass Transfer Methods	4
Reconstructing Compressor Non-Uniform Circumferential Flow Field From Spatially Undersampled Data—Part 1: Methodology and Sensitivity Analysis	4
Large Eddy Simulation of Heat Transfer Within a Multi-Perforation Synthetic Jets Configuration	4
Aerothermal Optimization of Turbine Squealer Tip Geometries With Arbitrary Cooling Injection	4
Experimental Study of Vaneless Diffuser Rotating Stall Development and Cell-Merging Phenomena	4
Analysis of Transonic Bladerows With Non-Uniform Geometry Using the Spectral Method	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
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
Uncertainty Propagation Analyses of Lean Burn Combustor Exit Conditions for a Robust Nozzle Cooling Design	4
Forced Response Due to Vane Stagger Angle Variation in an Axial Compressor	4
Innovative Design, Structural Optimization, and Additive Manufacturing of New-Generation Turbine Blades	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
Leakage Flow Impact on Shrouded Stator Cavity Flow Topology and Associated High-Speed Axial Compressor Stage Performance	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
Effect of Axial Casing Groove Geometry on Rotor-Groove Interactions in the Tip Region of a Compressor	4
Experimental and Numerical Study of Heat Transfer and Pressure Loss in a Swirl Multi-Pass Channel With Convergent Jet Slots	4
Vortex Tracking of Purge-Mainstream Interactions in a Rotating Turbine Stage	4
Investigation of Tip Leakage Vortex Breakdown in a High-Speed Multistage Axial Compressor	4
Enhancing Turbine Deposition Prediction Capability With Conjugate Mesh Morphing	4
Low Rank Education of Cascade Loss Sensitivity to Unsteady Parameters by Proper Orthogonal Decomposition	4
Computational and Experimental Study of Film-Cooling Effectiveness With and Without Downstream Vortex Generators	4
Influence of Boundary Layer Skew on the Tip Leakage Vortex of an Axial Compressor Stator	4
Impact of Varying High- and Low-Pressure Turbine Purge Flows on a Turbine Center Frame and Low-Pressure Turbine System	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
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
Wall Temperature Measurements in a Full-Scale Gas Turbine Combustor Test Rig With Fiber Coupled Phosphor Thermometry	4
Impacts of Tandem Configurations on the Aerodynamic Performance of an Axial Supersonic Through-Flow Fan Cascade	4
AN EXPERIMENTALLY VALIDATED LOW ORDER MODEL OF THE THERMAL RESPONSE OF DOUBLE-WALL EFFUSION COOLING SYSTEMS FOR HP TURBINE BLADES	4
A Method for Predicting the Aeroelastic Response of Radial Turbomachines	4
Experimental Investigation of Film Cooling Performance on Blade Endwall With Diffusion Slot Holes and Stator–Rotor Purge Flow	4
Heat Transfer Measurements Using Multiple Thermochromic Liquid Crystals in Symmetric Cooling Channels	4
Experimental Study of Impact of In-Service Deterioration on Thermal Performance of High-Pressure Nozzle Guide Vanes	4