Journal of Turbomachinery-Transactions of the Asme

Papers
(The TQCC of Journal of Turbomachinery-Transactions of the Asme is 4. The table below lists those papers that are above that threshold based on CrossRef citation counts [max. 250 papers]. The publications cover those that have been published in the past four years, i.e., from 2021-04-01 to 2025-04-01.)
ArticleCitations
Enhancing Turbine Deposition Prediction Capability With Conjugate Mesh Morphing29
Heat Transfer in an Injector-Scaled Additively Manufactured Fuel Passage27
Internal Heat Transfer Measurement on Metal-Based Additively Manufactured Channels Using a Transient Technique22
Analyzing Unsteady Turbomachinery Flow Simulations With Mixing Entropy21
Unsteady Flow Development and Reynolds Stress Measurements in a Centrifugal Compressor Vaned Diffuser21
UHBR Open-Test Case Fan ECL5/CATANA: Non-Linear Analysis of Non-Synchronous Blade Vibration at Part-Speed Conditions21
Impact of Flow Unsteadiness on Turbine Airfoil Heat Transfer via Streaming21
Rotating Instabilities in Shrouded Low Pressure Turbine at Design and Off-Design Conditions18
Analysis of Measured and Predicted Turbine Maps From Start-Up to Design Point18
Effect of Boundary Layer Suction on the Corner Separation in a Highly Loaded Axial Compressor Cascade18
Theoretical Considerations for Scaling Convection in Overall Effectiveness Experiments18
Quantitative Evaluation and Optimization of Feeding-Back Previous Cycles Information for Computational Fluid Dynamics Periodic Convergence18
On the Use of Pressure-Sensitive Paint to Determine the Rim Sealing Effectiveness18
Analysis of the Instantaneous Film Cooling Effectiveness on Showerhead Film Cooling Using Fast Response Pressure Sensitive Paint17
Optimal Riblets Applied to Gas Turbine Compressor Blades Studied via Direct Numerical Simulation (GT2024–122305)17
Understanding the Effect of Three-Dimensional Design in Tandem Blade17
Effect of Leading Edge Erosion on the Tip Leakage Flow in a Compressor Cascade16
Assimilation of Disparate Data for Improving the Performance Prediction of Body-Force Model15
Action Mechanism of Film Extraction on Channel Impingement Cooling for Blade Leading Edge Using Large Eddy Simulation15
Corner Separation Control Using Sweeping Jet Actuator in a Compressor Cascade15
An Improved Particle Impact Model by Accounting for Rate of Strain and Stochastic Rebound15
A Machine-Learnt Wall Function for Rotating Diffusers15
Stall Warning and Adaptive Control Subjected to Rotating Inlet Distortion in Axial Flow Compressor14
Aero-Thermal Aspects of Film Cooled Nozzle Guide Vane Endwall—Part 1: Aerodynamics14
Detecting Multidimensional Pareto Fronts During the Optimization of a Return Channel Within a Centrifugal Compressor13
Aerodynamic Influence of a Bleed on the Last Stage of a Low-Pressure Compressor and S-Duct13
The Effect of Heat Transfer on Turbine Performance13
Amplitude and Wavelength Effects for Wavy Channels13
Bayesian Mass Averaging in Rigs and Engines13
Acoustic Resonance in an Axial Multistage Compressor Leading to Non-Synchronous Blade Vibration13
Applying Infrared Thermography as a Method for Online Monitoring of Turbine Blade Coolant Flow13
Impact of Turbine-Strut Clocking on the Performance of a Turbine Center Frame13
On the Probabilistic Endurance Prediction Approach for Turbomachinery Blades and Vanes12
The Effect of Thermal Cycling on Deposition in an Impingement/Effusion Cooling Geometry12
Effect of Reynolds Number on Five-Hole Probe Performance: Experimental Study of the Open-Access Oxford Probe12
A Simplified Injection Model for Variable Area Turbine Fluidic Throttling12
Turbine Vane Passage Cooling Experiments With a Close-Coupled Combustor-Turbine Interface Geometry—Part I: Describing the Flow12
Modeling of Axial Compressor With Large Tip Clearances12
Modeling Stochastical Particle Rebound Based on High-Velocity Experiments12
Active Fluidic Control of a Nozzle Guide Vane Throat11
Evaluation of Cooling Requirements for Rotating Detonation Combustors11
A Robust Implementation of a Reynolds Stress Model for Turbomachinery Applications in a Coupled Solver Environment11
LES MODELING OF HIGH-LIFT HIGH-WORK LPT BLADES: PART II—VALIDATION AND APPLICATION11
An Investigation of Non-Linear Surge Characteristic in a High-Speed Centrifugal Compressor11
Heat Transfer Coefficient and Adiabatic Effectiveness Measurements on a Nozzle Guide Vane With a Single Row of Cylindrical Holes11
Experimental and Numerical Comparison of Two Turbine Vane Frame Designs11
The Effect of Inlet Conditions on Turbine Endwall Loss11
Study on Additive Effect of Film Cooling Effectiveness in Two Rows of Fan-Shaped Holes11
GPU-Accelerated Full-Wheel Large-Eddy Simulations of a Transonic Fan Stage11
A Free Streamline Model for Fully Separated Turbomachine Flows10
Experimental Investigation of Tip Design Effects on the Unsteady Aerodynamics and Heat Transfer of a High-Speed Turbine10
NATURE OF TRANSONIC COMPRESSOR FLOW AND ITS 3D DESIGN IMPLICATIONS10
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 10
The Role of Turbine Operating Conditions on Combustor–Turbine Interaction—Part I: Change in Expansion Ratio10
Design and Analysis of a Liftfan for eVTOL Aircraft10
Influence of Propagation Velocity and Peak Pressure of the Rotating Pressure Wave on the Flow Characteristics of a Centrifugal Compressor10
Modelling Particulate Deposition in Gas Turbines Part I: a Non-Spherical Bounce Stick Model10
Lean-Burn Combustor Simulator for an Engine-Component Test Facility: An Experimental and Computational Study10
Influences of Particulate Deposition on Vane Trailing-Edge Film Cooling: Adiabatic and Overall Cooling Effectiveness10
Heat Transfer Coefficient and Adiabatic Wall Temperature Measurements on High-Pressure Turbine Nozzle Guide Vanes With Representative Inlet Swirl and Temperature Distortions9
Coupled Time and Passage Spectral Method for an Efficient Resolution of Turbomachinery Far Upstream Wakes9
Phantom Cooling Effects on Rotor Blade Surface Heat Flux in a Transonic Full Scale 1 + 1/2 Stage Rotating Turbine9
Aerothermal Effect of Cavity Welding Beads on a Transonic Squealer Tip9
Machine Learning for the Development of Data-Driven Turbulence Closures in Coolant Systems9
On the Divergence Mechanisms Analysis of a Vibrating Blade Subjected to Repetitive Rubs With an Abradable Coating9
The Role of Turbine Operating Conditions on Combustor–Turbine Interaction—Part II: Loading Effects9
Experimental Analysis of the Time-Wise Compressor Fouling Phenomenon9
Heat Transfer Measurements Using Multiple Thermochromic Liquid Crystals in Symmetric Cooling Channels9
A Data-Driven Approach for Generalizing the Laminar Kinetic Energy Model for Separation and Bypass Transition in Low- and High-Pressure Turbines8
Application of a Distributed Element Roughness Model to Additively Manufactured Internal Cooling Channels8
Magnetic Resonance Velocimetry of a Turbine Blade With Engine-Representative Internal and Film Cooling Structures8
Numerical Characterization of Prestall Disturbances in a Compressor Stage8
Profile Loss Reduction of High-Lift Turbine Blades With Rough and Ribbed Surfaces8
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]8
Purge–Mainstream Interactions in a Turbine Stage With Rotor Endwall Contouring8
Adaptive Batch Sampling Strategy for the Hundreds-Dimensional Aerodynamic Optimization of the Centrifugal Impeller8
Design and Testing of a Multi-Stage Intermediate Pressure Turbine for Future Geared Turbofans8
Effect of the Key Geometry and Flow Parameters on Discharge Coefficient of Laidback Fan-Shaped Hole Under Coolant Crossflow Condition8
Particle Bounce Stick Behavior in the Rotating Frame of Reference8
Unsteady Structure of Compressor Tip Leakage Flows8
An Investigation of Secondary Cooling Effect on the Endwall Surface With Vane Trailing Edge Coolant Injection8
Evolution of Turbulence and Its Modification by Axial Casing Grooves in a Multi-Stage Axial Compressor8
Characterizing Flow Instabilities During Transient Events in the Turbine Rim Seal Cavity8
Experimental Investigation of Transient Flow Phenomena in Rotating Compressor Cavities8
Attenuation of Inlet Distortion Effects on Fans Using Asymmetric Inlet Guide Vanes8
A Turbo-Oriented Data-Driven Modification to the Spalart–Allmaras Turbulence Model8
Three-Dimensional Unsteady Aerodynamic Optimization of a Transonic Compressor Stage Using an Implicit Discrete Adjoint Harmonic Balance Method8
Effects of Radially Variable Sweep Vanes on Rotor–Stator Interaction Noise8
A Novel Multi-Fidelity Surrogate for Efficient Turbine Design Optimization7
Analysis of the Bifurcating Duct of an Inlet Particle Separator in Transonic Flow Conditions7
Comparative Study of Tip Injection in a Transonic and Subsonic Compressor7
Interpretation of Stall Precursor Signatures7
Experimental Study of Turbulent Flow and Heat Transfer Behaviors Over a Micro-Rib-Dimple-Structured Surface7
Enhanced Antideposition Performance of Film Cooling With a Shaped Sweeping Jet Hole7
Experimental and Numerical Study of an Open Impeller Centrifugal Compressor Stage Utilizing Three-Dimensional (3D) Diffuser End Wall Contouring for Operating Range Extension7
Cooling Performance of Additively Manufactured Pin Fins in Stacked Microchannels for the Inside-Out Ceramic Turbine Shroud-Cooling Ring7
Physical Mechanisms Investigation of Sharkskin-Inspired Compressor Cascade Based on Large Eddy Simulations7
Effect of Axial Casing Groove Geometry on Rotor-Groove Interactions in the Tip Region of a Compressor7
Optimization of a Tip Appendage for the Control of Tip Leakage Vortices in Axial Flow Fans7
Uncertainty Quantification of Aero-Thermal Performance of a Blade Endwall Considering Slot Geometry Deviation and Mainstream Fluctuation7
Analysis Method of Nonsynchronous Vibration and Influence of Tip Clearance Flow Instabilities on Nonsynchronous Vibration in an Axial Transonic Compressor Rotor7
Aerodynamic Effects of an Incoming Vortex on Turbines With Different Tip Geometries7
Investigation of the Discharge Coefficient for Laidback Fan-Shaped Holes on Turbine Blades Under Internal Crossflow Condition7
Vortex Tracking of Purge-Mainstream Interactions in a Rotating Turbine Stage7
Comparing Gradient-Free and Gradient-Based Multi-Objective Optimization Methodologies on the VKI-LS89 Turbine Vane Test Case7
Multidisciplinary Design of an Electrically Powered High-Lift System7
Experimental and Numerical Investigation of High Load Turbine Blade Tip Cavity Structures7
Global Optimization of a Transonic Fan Blade Through AI-Enabled Active Subspaces7
On the Correlation Between Spanwise Inducer Incidence and Impeller Diffusion for Ruled Surface and Barreled Sweep-Bow Impeller Design at Inlet Guide Vane-Off-Design7
Computational Aeroacoustics for a Cold, Non-Ideally Expanded Aerospike Nozzle7
Heat Transfer Coefficient Augmentation for a Shaped Film Cooling Hole at a Range of Compound Angles7
Effects of Inlet Guide Vanes on the Performance and Stability of an Aeronautical Centrifugal Compressor7
Impact of Ceramic Matrix Composite Topology on Friction Factor and Heat Transfer7
Effect of a Ceramic Matrix Composite Surface on Film Cooling6
Investigation of a Novel Turbine Housing to Produce a Nonuniform Spanwise Flow Field at the Inlet to a Mixed Flow Turbine and Provide Variable Geometry Capabilities6
Statistical Error Estimation Methods for Engineering-Relevant Quantities From Scale-Resolving Simulations6
Transonic Compressor Darmstadt Open Test Case: Experimental Investigation of Stator Secondary Flows and Hub Leakage6
Automatic Design Optimization of a Transonic Compressor Rotor for Improving Aeroacoustic and Aerodynamic Performance6
Reviewer’s Recognition6
A Data-Driven Method for the Derivation of Explicit Algebraic Reynolds Stress Models Applied to the Wake Losses of Low-Pressure Turbine Cascades6
Reconstructing Compressor Non-Uniform Circumferential Flow Field From Spatially Undersampled Data—Part 1: Methodology and Sensitivity Analysis6
Optimization of Three-Dimensional Blade and Variable Stators for Efficiency and Stability Enhancement of Multistage Axial Flow Compressor at Variable Speeds6
The Dynamic Calibration Uncertainty of Fast Response Pressure Probes6
Mode Analysis for the Rotating Aerodynamic Disturbance of a Transonic Fan6
Frequency Lock-In Phenomenon of Vortex Induced Vibration of a Rotating Blade Considering Bending-Torsion Coupling Effect6
Fan Flutter Mechanisms Related to Blade Mode Shape and Acoustic Properties6
Scaling Flat Plate Overall Effectiveness Measurements6
A New Loss Generation Body Force Model for Fan/Compressor Blade Rows: Application to Uniform and Non-Uniform Inflow in Rotor 676
Novel Strategy for Thermal Evaluation of Film-Cooled Blades Using Thermographic Phosphors at Simulated Engine Conditions6
Low Reynolds Number Effects on the Separation and Wake of a Compressor Blade6
Erratum: “Scaling Roughness Effects on Pressure Loss and Heat Transfer of Additively Manufactured Channels” [J. Turbomach. 139(2), p. 021003; DOI: 10.1115/1.4034555]6
Heat Transfer Measurements for Array Jet Impingement With Castellated Wall6
An Analytical Study on the Effects of Non-Uniform Vane Spacing on Forced Response Reduction in a Mistuned Blisk Rotor in a Multistage Axial Compressor6
Extending Highly Loaded Axial Fan Operability Range Through Novel Blade Design6
Numerical Implementation of Electrostatic Solver Within OpenFOAM for Gas Turbine Intake Filtration6
The Impact of the Off-Design Conditions on the Entropy Wave Interaction With a High-Pressure Turbine Stage6
Numerical Study on the Effects of Re on the Unsteady Behaviors in a Transonic Axial-Fan Under Inlet Distortion6
Vane–Probe Interactions in Transonic Flows6
The Effects of Casing Profile on the Aerodynamics of Integrated Intermediate Turbine Ducts6
Influence of Purge Flow Injection on the Performance of an Axial Turbine With Three-Dimensional Airfoils and Non-Axisymmetric Endwall Contouring6
Heat Transfer in Rotating, Trailing Edge, Converging Channels With Partial Length Pin-Fins6
Erratum: “Secondary Flows, Endwall Effects, and Stall Detection in Axial Compressor Design” [ASME J. Turbomach. 2015, 137(5), p. 051004; DOI: 10.1115/1.4028648]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 Blade6
Impacts of Material and Machine on the Variation of Additively Manufactured Cooling Channels6
Exploring Topology Optimization for High Pressure Turbine Blade Tips6
A Data-Centric Approach to Loss Mechanisms6
Investigation on Mode Characteristics of Rotating Instability and Rotating Stall in an Axial Compressor5
Non-Dimensional Parameters for Comparing Conventional and Counter-Rotating Turbomachines5
A Superposition Technique for Predicting Overall Effectiveness With Multiple Sources of Individually Characterized Internal and External Coolant Flows5
Experimental and Computational Investigation of Integrated Internal and Film Cooling Designs Incorporating a Thermal Barrier Coating5
Effects of Ribbed Surfaces on Profile Losses of Low-Pressure Turbine Blades5
Physics and Instantaneous Performance of Radial Turbines in Unsteady Flows: Validity of the Quasi-Steady Assumption for the Rotor5
Multi-Objective Numerical Optimization of Radial Turbines5
Unsteady Pre-Stall Behavior in a Centrifugal Compressor With Vaned Diffuser5
Blade Envelopes Part II: Multiple Objectives and Inverse Design5
Zonal Detached Eddy Simulation of the Fan-Outlet Guide Vanes Stage of a Turbofan Engine: Part I—Methodology, Numerical Setup, and Aerodynamic Analysis5
Impact of Swirling Entropy Waves on a High Pressure Turbine5
Numerical Investigation of Unsteady Combustor Turbine Interaction for Flexible Power Generation5
A High-Speed Disk Rotor Rig Design for Tip Aerothermal Research5
Nonlinear Flutter Analysis of Labyrinth Seals5
Aerothermal Performance of Slashface Leakage With Double Surface Angle Under Realistic Swirling Inflow5
Leakage Flow Impact on Shrouded Stator Cavity Flow Topology and Associated High-Speed Axial Compressor Stage Performance5
Aerodynamic Impact of Secondary Air Injection Flowrates on the Main Annulus Flow Field for a Transonic High-Pressure Turbine Stage5
Experimental Research Into Aeroelastic Phenomena in Turbine Rotor Blades Inside ARIAS EU Project5
Roughness Investigations on In-Service High-Pressure Compressor Blades—Part II: Roughness Parameterization and Computational Fluid Dynamics-Based Modeling of Its Impact on Turbulent Flows5
Influence of Supersonic Nozzle Design Parameters on the Unsteady Stator–Rotor Interaction in Radial-Inflow Turbines for Organic Rankine Cycles5
Rapid Algorithmic Blade Design Applying Machine Learning From Shape Optimization to Satisfy Multidisciplinary Constraints5
Impact of Temperature Ratio on Overall Cooling Performance: Low-Order-Model-Based Analysis of Experiment Design5
Endwall Contouring for Improving Aerodynamic Performance in a High-Pressure Turbine Cascade5
Fan Non-Synchronous Forced Vibration Under Crosswind5
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 Misalignment5
Robust Design Optimization of a Compressor Rotor Using Recursive Cokriging Based Multi-Fidelity Uncertainty Quantification and Multi-Fidelity Optimization5
High-Resolution Thermal Profiling of a Combustor in a Non-Dedicated Test Using Thermal History Coatings5
Deposition of Fuel Impurities Within Thermal Barrier Coatings in Gas Turbine Hot Gas Paths5
Computational Fluid Dynamics Simulations of the Unsteady-State Flow Through a 1.5-Stage High-Work Turbine5
On the Origin of “Rotating Instabilities”—Stability and Frequency Studies of Channel Flows5
Experimental Investigation of a High-Speed Turbine With Rainbow Rotor and Rim Seal Purge Flow5
Modeling and Simulation of Sand Particle Trajectories and Erosion in a Transonic Fan Stage5
Investigation of Surge in a Transonic Centrifugal Compressor With Vaned Diffuser: Part II—Correlation With Subcomponent Characteristics5
Extension and Validation of the Turbomachinery Capabilities of SU2 Open Source Computational Fluid Dynamic Code5
Blade Vibration Analysis for Radial Turbine Featuring a Multi-Channel Casing Design5
EXTENDING A VAN DER POL BASED REDUCED-ORDER MODEL FOR FLUID-STRUCTURE INTERACTION APPLIED TO NON-SYNCHRONOUS VIBRATIONS IN TURBOMACHINERY5
Unique High-Resolution Temperature Mapping of Stage 1 Turbine Vane in a Long-Term Engine Test5
The Development of Machine Learning Models for Radial Compressor Monitoring With Instability Detection5
Design Guidelines for Inertial Particle Separators5
Investigation on Flow Characteristics and Its Effect on Heat Transfer Enhancement in a Wide Channel With Staggered Diamond-S Pin Fins5
Effect of Solidity and Aspect Ratio on the Aerodynamic Performance of Axial-Flow Fans With 0.2 Hub-to-Tip Ratio5
Measurements of Turbulence in Compressible Low-Density Flows at the Inlet of a Transonic Linear Cascade With and Without Unsteady Wakes5
A New Multi-Stage Turbine Stator Design for Improved Performance Retention4
An Analysis of the Secondary Flow Around a Tandem Blade Under the Presence of a Tip Gap in a High-Speed Linear Compressor Cascade4
A Shock Loss Reduction Method Using a Concave Suction Side Profile for a Zero Inlet Swirl Turbine Rotor4
Impact of Low Freestream Turbulence and Surface Roughness on the Flat-Plate Boundary Layer Transition Under a High-Lift Airfoil Pressure Gradient4
Impact of Operating Conditions and Axial Casing Grooves on the Evolution of Flow Structure Across Blade Rows in an Axial Compressor4
Multidisciplinary Optimization of a Mixed-Flow Impeller With 140 Parameters and Its Shapley Additive Explanations4
Vortex Unsteadiness in the Endwall Region of a High-Lift Low-Pressure Turbine Passage4
Resolvent Analysis for Subsonic Compressor With Impedance Boundary Condition Casing Treatment4
Robustness Analysis on Aerothermal Performance of the Winglet Squealer Tip—Part 1: Aerodynamic Performance4
High-Fidelity Simulation Study of the Unsteady Flow Effects on High-Pressure Turbine Blade Performance4
A Physics-Informed Neural Network for Solving the Inverse Heat Transfer Problem in Gas Turbine Rotating Cavities4
The Effects of Incoming Vortex and Wake on the Aerodynamics of an Intermediate Turbine Duct4
A New Nonlinear Time-Domain Flutter Analysis Approach for Distorted Flows4
Direct Numerical Simulation of Transitional and Turbulent Flows Over Multi-Scale Surface Roughness—Part I: Methodology and Challenges4
Reassessment of the Conventional: Numerical Validation of a One-Dimensional Model for the Prediction of Volute Losses4
Use of Multiple Tracer Gases to Quantify Vane Trailing Edge Flow Into Turbine Rim Seals4
Aerodynamic Performance and Leakage Flow in Turbine Cascades With Sweeping Jet Actuators4
The Influence of Element Thermal Conductivity, Shape, and Density on Heat Transfer in a Rough Wall Turbulent Boundary Layer With Strong Pressure Gradients4
Unsteady Flow Structure of Rotating Instability in a 1.5-Stage Axial Compressor4
Highly Time Resolved, Combined Temperature, and Heat Flux Measurement Technique Based on ALTP Sensors4
Adaptation of von Karman Institute for Fluid Dynamics’ Isentropic Compression Tube Facility for High-Speed Low-Pressure Turbines Testing4
The Influence of Purge Flow Parameters on Heat Transfer and Film Cooling in Turbine Center Frames4
Introduction of Axisymmetric Grooves as a Tip Seal Treatment for Small-Core Turbines4
Improved Spatiotemporal Distributions of Sweeping Jet Film Cooling With a Shaped Exit Design4
Exploring Physics of Acoustic Flow Control Over Airfoils Toward Potential Application to High Work and Lift Turbines4
Effect of Differential Tip Clearance on the Performance of a Tandem Rotor4
The Influence of Combustor Hot Streaks on the Aerodynamic Performance of a Turbine Center Frame4
Numerical and Experimental Investigation of Boundary Layer of a High-Lift Low-Pressure Turbine Cascade Under Periodic Wakes With Different Flow Coefficients4
Prediction of Steady and Unsteady Flow Quantities Using Multiscale Graph Neural Networks4
Modelling Particulate Deposition in Gas Turbines Part II: Prediction and Validation of Deposition Distributions4
Collaborative Robust Design Optimization of Blade Geometry and Manufacturing Tolerance for a Transonic Centrifugal Impeller4
A Fluid–Structure Interaction Tool Using a Van der Pol-Based Reduced-Order Model for Buffet and Nonsynchronous Vibrations4
Thermohydraulic Performance and Flow Structures of Diamond Pyramid Arrays4
Investigating the Influence of Mainstream Turbulence and Large Vortices on Gas Turbine Trenched Film Cooling Flows Using Planar Temperature-Velocity Imaging4
A Data-Driven Tip Flow Loss Prediction Method for a Transonic Fan Under Boundary Layer Ingesting Inflow Distortion4
Assessment of Low Engine Order Excitation of a Contaminated Turbocharger Radial Turbine Stage Using a Nozzle Ring Only Computational Model4
Impact of the Wall-Parallel Length Scale of Roughness on the Development of Turbulent Boundary Layers in Turbines4
Equation-Oriented Meanline Method for Axial Turbine Performance Prediction Under Choking Conditions4
Experimental Investigations on the Effects of Surface Roughness for Compressor Cascades With Different Roughness Magnitude and Location4
A Method for Preliminary Design of Variable Geometry Vaned Diffuser for Centrifugal Compressor4
Free-Stream Turbulence-Induced Boundary-Layer Transition in Low-Pressure Turbines4
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 Configurations4
Investigation of an Inter-Compressor S-Duct Using the Lattice Boltzmann Method4
The Unsteady Shock–Boundary Layer Interaction in a Compressor Cascade—Part II: High-Fidelity Simulation4
Numerical Investigations on the Rotating Stall in an Axial Compressor and Its Control by Flow Injection at Casing4
Unsteady Flow Mechanism of Impeller Stall Inception in a High-Pressure Ratio Centrifugal Compressor With Bleed Slots4
Manufacturing a Ceramic Turbine Rotor for a Compact Jet Engine4
Numerical Study on the Effect of Back Cavity on the Aerodynamic Behavior of a Non-Axisymmetric Casing Treatment for Transonic Axial Compressors4
The Effects of Swirling Flows in Entropy Wave Convection Through High-Pressure Turbine Stage4
Plume Model for Buoyancy-Induced Flow and Heat Transfer in Closed Rotating Cavities4
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