Journal of Turbomachinery-Transactions of the Asme

Article	Citations
Experimental Study on the High Relative Casing Motion Effect on Turbine Blade Tip Aerodynamic Characteristics	43
Three-Dimensional Unsteady Aerodynamic Optimization of a Transonic Compressor Stage Using an Implicit Discrete Adjoint Harmonic Balance Method	32
Analysis of the Bifurcating Duct of an Inlet Particle Separator in Transonic Flow Conditions	32
Effects of Radially Variable Sweep Vanes on Rotor–Stator Interaction Noise	26
Effect of the Key Geometry and Flow Parameters on Discharge Coefficient of Laidback Fan-Shaped Hole Under Coolant Crossflow Condition	26
An Improved Particle Impact Model by Accounting for Rate of Strain and Stochastic Rebound	24
Rotating Instabilities in Shrouded Low Pressure Turbine at Design and Off-Design Conditions	24
On the Divergence Mechanisms Analysis of a Vibrating Blade Subjected to Repetitive Rubs With an Abradable Coating	23
Turbine Vane Passage Cooling Experiments With a Close-Coupled Combustor-Turbine Interface Geometry—Part I: Describing the Flow	21
Effect of Leading Edge Erosion on the Tip Leakage Flow in a Compressor Cascade	19
Performance Sensitivity of a Grooved Tip Seal to Manufacturing and Operational Geometry Deviations	18
Exploring Topology Optimization for High Pressure Turbine Blade Tips	18
Corner Separation Control Using Sweeping Jet Actuator in a Compressor Cascade	18
Evaluation of Cooling Requirements for Rotating Detonation Combustors	17
On the Use of Pressure-Sensitive Paint to Determine the Rim Sealing Effectiveness	17
Reviewer’s Recognition	17
Roughness Investigations on In-Service High-Pressure Compressor Blades—Part II: Roughness Parameterization and Computational Fluid Dynamics-Based Modeling of Its Impact on Turbulent Flows	16
Nonlinear Flutter Analysis of Labyrinth Seals	16
A New Multi-Stage Turbine Stator Design for Improved Performance Retention	16
A Framework for Estimating Effects of Combustor Turbulence on Turbine Profile Loss Generation	16
Physics-Guided Graph Neural Networks: Numerical Investigation of High-Pressure Turbine Flow	15
Modeling and Simulation of Sand Particle Trajectories and Erosion in a Transonic Fan Stage	15
Measurements of Turbulence in Compressible Low-Density Flows at the Inlet of a Transonic Linear Cascade With and Without Unsteady Wakes	15
Introduction of Axisymmetric Grooves as a Tip Seal Treatment for Small-Core Turbines	15
Unique High-Resolution Temperature Mapping of Stage 1 Turbine Vane in a Long-Term Engine Test	14

Prediction of Steady and Unsteady Flow Quantities Using Multiscale Graph Neural Networks	14
A MULTISCALE REPRESENTATION OF TURBULENCE GENERATION IN COMPRESSOR FLOWS	13
Fan Non-Synchronous Forced Vibration Under Crosswind	13
Aerodynamic Effect of Shallow Circumferential Grooves in the Shroud of a Centrifugal Compressor	13
Wind Tunnel Continuous-Scan Acoustic Analysis of Ducted Fan Tones Interacting With a Shielding Wall	13
Development of a novel pressure-based approach for blade synchronous vibration detection including mistuning	13
An Analysis of the Secondary Flow Around a Tandem Blade Under the Presence of a Tip Gap in a High-Speed Linear Compressor Cascade	13
Effects of Blade Solidity and Aspect Ratio on a 0.5 Hub-to-Tip Ratio Tube-Axial Fan	13
Numerical Study on the Effect of Back Cavity on the Aerodynamic Behavior of a Non-Axisymmetric Casing Treatment for Transonic Axial Compressors	13
The Effects of Swirling Flows in Entropy Wave Convection Through High-Pressure Turbine Stage	12
Acoustic Modes in an Open Box Cavity With Variable Depth Using Two Distinct Wind Tunnels	12
Film Cooling on Turbine Vane Endwalls With Different Inlet Cooling Configurations: Experimental and Computational Results	12
A Method for Preliminary Design of Variable Geometry Vaned Diffuser for Centrifugal Compressor	12
Unsteady Pre-Stall Behavior in a Centrifugal Compressor With Vaned Diffuser	12
Spectral Heat Transfer Coefficient for Thermal Design Analysis—Part 1: Augmenting the Cooling Law for Non-Isothermal Wall	11
Fundamentals of Scaling of Overall Cooling Effectiveness With Temperature Ratio	11
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
A Study of Loss Model Parameter Sensitivity in Compressor Unsteady Flow Simulations	11
Inlet Flow Distortion in an Advanced Civil Transport Boundary Layer Ingesting Engine Installation	11
NUMERICAL DESIGN OF EXPERIMENTS FOR REPEATING LOW-PRESSURE TURBINE STAGES PART I: COMPUTATIONAL OPPORTUNITIES AND METHODOLOGY	11
Systematic Numerical Investigation on the Surface Roughness Effects on the Friction and Heat Transfer of Additively Manufactured Components	10
Impacts of Tandem Configurations on the Aerodynamic Performance of an Axial Supersonic Through-Flow Fan Cascade	10
One-Dimensional Modeling for Pulsed Flow Twin-Entry Turbine	10
On the Over-Prediction of Centrifugal Compressor Pressure Ratio in the High Impeller Tip Mach Number Regime	10
Heat Transfer Measurements in a Turbine Centre Frame at Realistic Mach Number - Part 2: Influence of Combustor Hot Streaks	10
Tail-Integrated Boundary Layer Ingesting Propulsion Systems for Turbo-Electric Aircraft	10
Experimental Investigation of Additional Loss Associated With Incoming Wakes in Low-Pressure Turbine Cascades	10
Loss Analysis of Cavity Leakage Flow in a Compressor Cascade	10
Analytical Study on the Influence of Stage-Wise Distribution of Parameters on the Performance of a Multistage Axial Compressor	10
Effect of Axial Throughflow Swirl on Flow and Heat Transfer in a Compressor Disc Cavity	10
Multistage Turbomachinery Optimization for High-Temperature Heat Pumps With the Reverse Rankine Cycle	9
The Influence of Turbulence and Reynolds Number on Endwall Heat Transfer in a Vane Cascade	9
Effects of Downstream Vortex Generators on Film Cooling a Flat Plate Fed by Crossflow	9
Entry Region Heat Transfer Augmentation With Pins, Fins, and Turbulators in Circular Channels	9
Unpacking Intermineral Synergies and Reactions During Dust Deposition in an Impingement Coolant Jet	9
An Experimental Investigation of Sweeping Mist Jet Film Cooling With Droplet Analysis	9
Experimental Study on Controlling Flow Separation of Compressor Cascades With Self-Excited Sweeping Jet Actuator	9
Numerical Modeling and Design Challenges of Boundary Layer Ingesting Fans	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
Aerodynamics and Heat Transfer Inside a Gas Turbine Mid-Passage Gap	9
Unsteady Aerodynamic Forcing Due to Distortion in a Boundary Layer Ingesting Fan	9
Stall Behavior in an Ultrahigh-Pressure-Ratio Centrifugal Compressor: Backward-Traveling Rotating Stall	9
Experimental Determination of Heat Transfer Coefficient on Impingement Cooled Gear Flanks: Validation of the Evaluation Method	9
Analysis of Complex Total Pressure Distortion Screens Using One-Dimensional Loss Data	9
Correlated Pressure–Velocity Instability in a Transonic High-Pressure Turbine Blade	9
Modeling Deposition in Gas Turbines With Conjugate Mesh-Morphing and Temperature Sensitivity	8
Numerical Study on Unsteady Flow of a Supersonic Partial Admission Impulse Turbine	8
Revisiting Dimensionless Parameters Quantifying Film Cooling	8

Windage Torque Reduction in Low-Pressure Turbine Cavities Part II: Experimental and Numerical Results	8
Direct and Inverse Model for Single-Hole Film Cooling With Machine Learning	8
Dirt Ingestion Impacts on Cooling Within a Double-Walled Combustor Liner	8
An Improved Passage-Flow Turning Model for Forward-Curved Blades of Squirrel-Cage Fan	8
Flow and Heat Transfer in a Rotating Disc Cavity With Axial Throughflow at High-Speed Conditions	8
Effect of Upstream Leakage Flow on Film Cooling Characteristic of a Turbine Convex Endwall	8
Numerical Assessment of an Aerodynamic Probe to Enable Short Focal Length Laser Diagnostics in High Temperature Supersonic Flows Based on Flow Disturbance	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
Impact of High-Pressure-Turbine Purge Flow on the Evolution of Turbulence in a Turbine Vane Frame	8
High-Fidelity Investigation of Vortex Shedding From a Highly Loaded Turbine Blade	8
Unsteady Flow Structure of Corner Separation in a Highly Loaded Compressor Cascade	8
Numerical Investigation on the Influence of Wet Compression Aerodynamic Performance of Multi-Stage Transonic Compressor	8
Flow Check and Adiabatic Effectiveness Measurements on Traditionally Versus Additively Manufactured Film-Cooling Holes	8
Performance and Secondary Flow Structures Characterization in a Highly Loaded Low-Pressure Compressor Under Distorted Inflow Conditions	8
Insights Into Turbocharger Centrifugal Compressor Stability Using High-Fidelity Computational Fluid Dynamics and a Novel Impeller Diffusion Factor	8
Blade Envelopes Part I: Concept and Methodology	8
Numerical Study of Crossflow Effects on Discharge Coefficient of the Converging Slot Hole	8
Noise Source Identification for the Unsteady Low-Pressure Turbine Flow Fields	7
The Influence of Deterministic Surface Roughness and Freestream Turbulence on Transitional Boundary Layers: Heat Transfer Distributions and a New Transition Onset Correlation	7
ANALYSIS OF AEROACOUSTIC PHENOMENA IN CENTRIFUGAL COMPRESSORS USING A LATTICE BOLTZMANN FLOW SIMULATION APPROACH	7
Comparative Investigation of HPT Blade Cooling Concepts in an Aerothermal Test Rig	7
Unsteadiness in the Secondary Flows of a High-Speed Low-Pressure Turbine Cascade With Unsteady Wakes and Purge Flow	7
Optimal Riblets Applied to Gas Turbine Compressor Blades Studied via Direct Numerical Simulation (GT2024–122305)	7
Influences of Particulate Deposition on Vane Trailing-Edge Film Cooling: Adiabatic and Overall Cooling Effectiveness	7
The Application of Fluidic Sealing in Shrouded Gas Turbine Blades	7
Sensitivity Analysis for Flow Stability of Axial Compressor Based on Meridional Flow	7
A Review of Secondary Combustion on the Turbine Blade Cooling	7
Film Superposition Characteristics With Laidback Fan-Shaped Holes Under the Influence of Internal Crossflow	7
Dissipation in Skewed Boundary Layers	7
Strategies for High-Accuracy Measurements of Stage Efficiency for a Cooled Turbine	7
Response of Separated Boundary Layers to Steady and Pulsated Flow Injection	7
A Three-Dimensional Actuator Disk Model for Fan Response to Inlet Distortion: Part I - Formulation	7
A Detailed Loss Analysis Methodology for Centrifugal Compressors	7
Compressor Stator Leading Edge Instrumentation	7
RANS Capabilities for Transonic Axial Compressor: A Perspective From GPPS Computational Fluid Dynamics Workshop	7
Morphing of Reversible Axial Fan Blade: A FSI-FEM Study	7
Investigation of Tip Leakage Vortex Breakdown in a High-Speed Multistage Axial Compressor	7
Advanced Design of a Transition Duct for Supersonic Inlet Turbines in Rotating Detonation Engines	7
Investigation of the Map Width Improvement in a Radially Reduced Diffuser Design Concept for a Centrifugal Compressor	7
Impacts of Material and Machine on the Variation of Additively Manufactured Cooling Channels	7
The Design of Aspirated Stators for Compressor Bleed	7
Numerical Investigation of the Fan Flutter Mechanism Related to Acoustic Propagation Characteristics	7
Equation-Oriented Meanline Method for Axial Turbine Performance Prediction Under Choking Conditions	6
Blade Vibration Analysis for Radial Turbine Featuring a Multi-Channel Casing Design	6
Characterizing Flow Instabilities During Transient Events in the Turbine Rim Seal Cavity	6
Effects of Ribbed Surfaces on Profile Losses of Low-Pressure Turbine Blades	6
Experimental and Numerical Investigation of High Load Turbine Blade Tip Cavity Structures	6
Optimization of a Tip Appendage for the Control of Tip Leakage Vortices in Axial Flow Fans	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
The Effect of Inlet Conditions on Turbine Endwall Loss	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
Collaborative Robust Design Optimization of Blade Geometry and Manufacturing Tolerance for a Transonic Centrifugal Impeller	6
Plume Model for Buoyancy-Induced Flow and Heat Transfer in Closed Rotating Cavities	6
Surge Inception Point Analysis Using the Greitzer Model for Centrifugal Compressor	6
Aft Fuselage Boundary Layer Ingesting Propulsion System Design	6
Investigating the Influence of Mainstream Turbulence and Large Vortices on Gas Turbine Trenched Film Cooling Flows Using Planar Temperature-Velocity Imaging	6
GPU-Accelerated Full-Wheel Large-Eddy Simulations of a Transonic Fan Stage	6
The Influence of Combustor Hot Streaks on the Aerodynamic Performance of a Turbine Center Frame	6
UHBR Open-Test Case Fan ECL5/CATANA: Non-Linear Analysis of Non-Synchronous Blade Vibration at Part-Speed Conditions	6
The Influence of Purge Flow Parameters on Heat Transfer and Film Cooling in Turbine Center Frames	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
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]	6
Data Assimilation of Transitional and Separated Turbomachinery Flows With Physics-Informed Neural Networks	6
Cooling Performance of Additively Manufactured Pin Fins in Stacked Microchannels for the Inside-Out Ceramic Turbine Shroud-Cooling Ring	6
Manufacturing a Ceramic Turbine Rotor for a Compact Jet Engine	6
Robustness Analysis on Aerothermal Performance of the Winglet Squealer Tip—Part 1: Aerodynamic Performance	6
A New Loss Generation Body Force Model for Fan/Compressor Blade Rows: Application to Uniform and Non-Uniform Inflow in Rotor 67	6
Effect of Solidity and Aspect Ratio on the Aerodynamic Performance of Axial-Flow Fans With 0.2 Hub-to-Tip Ratio	6
A Shock Loss Reduction Method Using a Concave Suction Side Profile for a Zero Inlet Swirl Turbine Rotor	6
Adaptation of von Karman Institute for Fluid Dynamics’ Isentropic Compression Tube Facility for High-Speed Low-Pressure Turbines Testing	6
Comparative Study of Tip Injection in a Transonic and Subsonic Compressor	6
Impact of Low Freestream Turbulence and Surface Roughness on the Flat-Plate Boundary Layer Transition Under a High-Lift Airfoil Pressure Gradient	6
Multiscale Data-Driven RANS Closure for Trailing Edge Cutback Film Cooling Flows	6
Highly Time Resolved, Combined Temperature, and Heat Flux Measurement Technique Based on ALTP Sensors	6
Heat Transfer in an Injector-Scaled Additively Manufactured Fuel Passage	6
Particle Bounce Stick Behavior in the Rotating Frame of Reference	6
Magnetic Resonance Velocimetry of a Turbine Blade With Engine-Representative Internal and Film Cooling Structures	6
Multidisciplinary Optimization of a Mixed-Flow Impeller With 140 Parameters and Its Shapley Additive Explanations	6
Experimental Research Into Aeroelastic Phenomena in Turbine Rotor Blades Inside ARIAS EU Project	6
IMPACT OF FAN AERODYNAMICS ON INLET DISTORTION AT CROSSWIND	6

The Effects of Incoming Vortex and Wake on the Aerodynamics of an Intermediate Turbine Duct	6
A Free Streamline Model for Fully Separated Turbomachine Flows	6
A New Nonlinear Time-Domain Flutter Analysis Approach for Distorted Flows	6
Effects of Water-to-Air Mass Ratio on Long-Term Washing Efficiency and Erosion Risk in an Axial Compressor Under Online Washing Conditions	5
Experimental Investigation of Mode-Frequency Scattering at Fan Stages	5
The Influence of Boundary Layer State and Trailing Edge Wedge Angle on the Aerodynamic Performance of Transonic Turbine Blades	5
Experimental and Numerical Analysis of Loss Characteristics of Cooled Transonic Nozzle Guide Vanes	5
Effects of Rotation on the Flow Structure in a Compressor Cascade	5
High-Fidelity Computational Assessment of Aero-Thermal Performance and the Reynolds’ Analogy for Additively Manufactured Anisotropic Surface Roughness	5
Inverse Design of Compressor/Fan Blade Profiles Based on Conditional Invertible Neural Networks	5
Wall-Modeled Large-Eddy Simulation of a Transonic Gas Turbine Vane—Part II: Mach Number Effect and Losses Prediction	5
Convergence Acceleration of Favre-Averaged Non-Linear Harmonic Method	5
Effects on Film Cooling Performance in the Showerhead From Geometric Parameterization of Shaped Hole Designs	5
Large Eddy Simulation of Laminar and Turbulent Shock/Boundary Layer Interactions in a Transonic Passage	5
Improved Prediction of Losses With Large Eddy Simulation in a Low-Pressure Turbine	5
Innovative Cavity Modeling for Centrifugal Compressors Aeromechanical Analysis	5
Development of Compact and Hermetic Organic Rankine Cycle Turbine Generator With Upgraded Cooling Capability	5
Efficient Aerodynamic Uncertainty Quantification for a Three-Dimensional Transonic Fan Rotor	5
An Active Turbulence Grid for Turbomachinery Flow Experiments	5
A Physics-Informed Neural Network for Solving the Inverse Heat Transfer Problem in Gas Turbine Rotating Cavities	5
The Unsteady Topology of Corner Separations	5
Wake–Separation Bubble Interaction Over an Experimentally Simulated Axial Compressor Blade Under Low Reynolds Number Flow	5
Improvements in the Prediction of Steady and Unsteady Transition and Mixing in Low-Pressure Turbines by Means of Machine-Learnt Closures	5
Pressure Characteristic Rollover of a Transonic Centrifugal Impeller	5
On the Secondary Flow System of an Aggressive Inter Compressor Duct	5
Scale-Resolving Simulations of Turbulent Flow Retaining the Exact Blade Count With the Time-Inclined Method	5
Low Reynolds Number Effects on the Endwall Flow Field in a High-Lift Turbine Passage	5
Loss Analysis in Radial Inflow Turbines for Supercritical CO2 Mixtures	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
A Test Facility for the Experimental Investigation of Labyrinth Seal Flutter and Early-Stage Validation of Prediction Techniques	5
Transient Temperature Field Inversion of Turbine Based on Physics-Encoded Neural Networks	5
Effective Clearance and Differential Gapping Impact on Seal Flutter Modeling and Validation	5
A High-Speed Disk Rotor Rig Design for Tip Aerothermal Research	5
Impact of the Purge Flow Density Ratio on the Rim Sealing Effectiveness in Hot Gas Ingestion Measurements	5
Heat Transfer and Flow Field Characteristics of Variable Aspect Ratio, Serpentine Passages	5
Turbine Nozzle Guide Vane Endwall Film Cooling and Vane Phantom Cooling Performances at Various Blocked Film Hole Configurations	5
Annular Dump Diffuser and Deswirl System for Back-Pressure Control in Engine-Scale Transonic Annular Cascade	5
Modeling of Combustor Non-Uniformities Evolution Through a High-Pressure Turbine Stage	5
Characterizing the Unsteady Flow Field in Low-Flow Turbine Operation	4
Data-Driven Radial Compressor Design Space Mapping	4
Considerations for Compressible Film Cooling: A Computational Study of the Effects of Transonic Flows and Varying Mainstream Mach Number	4
Using Data Assimilation to Improve Turbulence Modeling for Inclined Jets in Crossflow	4
Effect of Coolant Crossflow on Film Cooling Effectiveness of Diffusion Slot Hole With and Without Ribs	4
Numerical Investigation of the Effect of Trailing Edge Thickness of Simulated Ceramic Matrix Composite Blades on Loss Profiles	4
Large Eddy Simulation Analysis of Loss Anomaly of a Turbine Blade With Large Trailing Edge Radius	4
Analysis of Heat Transfer Within Buoyancy Dominated Rotating Cavities of High-Pressure Compressors	4
Impact of Temperature Ratio on Overall Cooling Effectiveness: Experimental Validation of a Scaling Theory	4
Scaling Heat Transfer and Pressure Losses of Novel Additively Manufactured Rib Designs	4
Boundary Layer Analysis of a Transonic High-Pressure Turbine Vane Using Ultra-Fast-Response Temperature-Sensitive Paint	4
Mitigation of Boundary Layer Ingestion Circumferential Distortion Using Nonaxisymmetric Fan Exit Guide Vanes	4
Mode Analysis for the Rotating Aerodynamic Disturbance of a Transonic Fan	4
Validation of Filtered Rayleigh Scattering Optical Rake Measurement Techniques in Turbomachinery Applications and Boundary Layers	4
Aero-Structural Coupling Strategy for a Morphing Blade Cascade Study	4
The Impact of Manufacturing Variations on the Aerothermal Performance of High-Pressure Turbine Blade Shrouds	4
Challenges in Aerodynamic Performance of Micro Gas Turbines and Design Inefficiencies	4
Experimental Study of Impact of In-Service Deterioration on Thermal Performance of High-Pressure Nozzle Guide Vanes	4
The Effect of Reaction on Compressor Performance	4
Impact of Blowing and Density Ratio on the Film Cooling and Heat Transfer in an Aggressive Turbine Center Frame	4
Investigation on Heat Transfer Distribution of Rotating Two-Pass Smooth and Ribbed Channels Under Aero-Engine Simulated Conditions	4
The Effect of Upstream Unsteadiness on the Unstarting of a Supersonic Inlet Turbine	4
A Resistive Model to Characterize Overall Effectiveness Influenced by Multiple Coolant Temperatures	4
The Role of Turbine Operating Conditions on Combustor–Turbine Interaction—Part II: Loading Effects	4
Hybrid RANS-LES Simulation of Rotor–Stator Interaction in a Compressor Stage Using a Grid-Adaptive Simulation Method	4
Computational and Experimental Study of Film-Cooling Effectiveness With and Without Downstream Vortex Generators	4
Unsteady Loss Mechanisms in Low-Pressure Turbines With Diverging End-Walls Studied Via High-Fidelity Simulation	4
Interaction Mechanism of Transonic Squealer Tip Cooling With the Effect of High-Speed Relative Casing Motion	4
Non-Intrusive Ground Force Decomposition Applied to Turbofans—Part II: Filtered Rayleigh Scattering Application	4
Analysis on the Effect of Cavity Flows on the Aerothermal Performance of a High-Pressure Turbine Stage	4
The Impact of Multi-Scale Ceramic Matrix Composite Roughness on Heat Transfer and Boundary Layer Behavior	4
Validation of Broadband Noise Prediction Methodology Based on Linearized Navier–Stokes Analyses	4
A New Axial Compressor Test Facility for the Investigation of Aerodynamic Damping Featuring an Electromagnetic Excitation System	4
Unsteady Investigation of Intermediate Turbine Ducts Under the Influence of Purge Flows	4
A Digital Engineering Analysis of an Additively-Manufactured Turbine Vane	4
Fan Stability Enhancement With Partial Casing Treatments	4
Experimental Investigation of Flame-Film Cooling Interactions With an Academic Test Rig and Optical Laser Diagnostics	4
Reynolds Number Effect on Transitional Delayed Detached-Eddy Simulation	4
Cavity Impact on the Base Flow Unsteadiness for a High-Speed Exhaust System	4
The Role of Turbine Operating Conditions on Combustor–Turbine Interaction—Part I: Change in Expansion Ratio	4
Unsteady Structure of Compressor Tip Leakage Flows	4
Influence of Casing Groove on Rotating Instabilities in a Low-Speed Axial Compressor	4
Experimental Investigation of the Pre-Stall and Stall Evolution in a Centrifugal Compressor With a Volute	4
High-Dimensional Uncertainty Quantification of High-Pressure Turbine Vane Based on Multifidelity Deep Neural Networks	4
Turbine Vane Passage Cooling Experiments With a Close-Coupled Combustor–Turbine Interface Geometry Part II: Describing the Coolant Coverage	4
Analysis of Averaging Methods for Nonuniform Total Pressure Fields	4
Effect of Geometry and Heat Flux on Turbine Over-Tip Flow Power Extraction	4
Quasi-Dynamic Approximation of Unsteady Pressure Distribution for Transonic Airfoils in Flutter	4
On Intake–Compressor Interactions Within an Integrated Propulsion System	4
Control of Shroud Leakage Loss and Windage Torque in a Low-Pressure Turbine Stage	3
Reconstruction and Reduction of Realistic Manufacturing Error Field for Uncertainty Quantification of Transonic Axial Compressor Rotor	3
PDA Laser Measurements of Droplet-Laden Flows in a Four-Stage Axial Compressor	3
Direct Numerical Simulation of a High-Pressure Turbine Stage: Unsteady Boundary Layer Transition and the Resulting Flow Structures	3
Roughness Related to Cooling Performance of Channels Made Through Additive Manufacturing	3
Multi-Objective Aerodynamic and Aeroelastic Coupled Design Optimization Using a Full Viscosity Discrete Adjoint Harmonic Balance Method	3
Effect of Blade Damage on Low Pressure Ratio Fan Windmill Aerodynamics	3
INVESTIGATION OF SHEAR LAYER INDUCED PRESSURE FLUCTUATIONS IN A LINEAR COMPRESSOR CASCADE	3