Skip Nav Destination

Issues

Select Decade

Select Year

Issue

Volume 147, Issue 6

June 2025

In Progress

Previous Issue
Next Issue

ISSN 0889-504X

EISSN 1528-8900

In this Issue

Research Papers

Research Papers

Spectral Heat Transfer Coefficient for Thermal Design Analysis—Part 1: Augmenting the Cooling Law for Non-Isothermal Wall

L. He

J. Turbomach. June 2025, 147(6): 061001. doi: https://doi.org/10.1115/1.4066671

Abstracts

View articletitled, Spectral Heat Transfer Coefficient for Thermal Design Analysis—Part 1: Augmenting the Cooling Law for Non-Isothermal Wall

Open the PDF for in another window

Topics: Cooling , Temperature , Wall temperature , Fluids , Blades , Flow (Dynamics) , Design , Heat flux , Heat , Heat transfer coefficients

Spectral Heat Transfer Coefficient for Thermal Design Analysis—Part II: Leveraging Diabatic Wall Conditioning for Nonlinear Regime

L. He

J. Turbomach. June 2025, 147(6): 061002. doi: https://doi.org/10.1115/1.4066672

Abstracts

View articletitled, Spectral Heat Transfer Coefficient for Thermal Design Analysis—Part II: Leveraging Diabatic Wall Conditioning for Nonlinear Regime

Open the PDF for in another window

Topics: Cooling , Temperature , Blades , Heat transfer , Wall temperature , Heat flux , Design

Introduction of Axisymmetric Grooves as a Tip Seal Treatment for Small-Core Turbines

Connor J. Wiese, Reid A. Berdanier, Karen A. Thole

J. Turbomach. June 2025, 147(6): 061003. doi: https://doi.org/10.1115/1.4067034

Abstract

View articletitled, Introduction of Axisymmetric Grooves as a Tip Seal Treatment for Small-Core Turbines

Open the PDF for in another window

Topics: Blades , Flow (Dynamics) , Pressure , Rotors , Turbines , Design , Geometry , Vortices

Optimization of Tip Seal Grooves for Aerodynamic and Durability Improvements of Small-Core Turbines

Connor J. Wiese, Reid A. Berdanier, Karen A. Thole

J. Turbomach. June 2025, 147(6): 061004. doi: https://doi.org/10.1115/1.4067028

Abstract

View articletitled, Optimization of Tip Seal Grooves for Aerodynamic and Durability Improvements of Small-Core Turbines

Open the PDF for in another window

Topics: Blades , Clearances (Engineering) , Design , Flow (Dynamics) , Geometry , Heat transfer , Optimization , Rotors , Turbines , Stress

Understanding the Flow Field in a Highly Loaded Tandem Compressor Cascade

Thanh-Son Tran, Cedric Babin, Fabrizio Fontaneto, Gregory Coussement, Tom Verstraete

J. Turbomach. June 2025, 147(6): 061005. doi: https://doi.org/10.1115/1.4067029

Abstracts

View articletitled, Understanding the Flow Field in a Highly Loaded Tandem Compressor Cascade

Open the PDF for in another window

Topics: Blades , Flow (Dynamics) , Design , Cascades (Fluid dynamics)

Loss Breakdown in Axial Turbines: A New Method for Vortex Loss and Wake Detection From 3D RANS Simulations

Greta Raina, Yannick Bousquet, David Luquet, Eric Lippinois, Nicolas Binder

J. Turbomach. June 2025, 147(6): 061006. doi: https://doi.org/10.1115/1.4067033

Abstracts

View articletitled, Loss Breakdown in Axial Turbines: A New Method for Vortex Loss and Wake Detection From 3D RANS Simulations

Open the PDF for in another window

Topics: Boundary layers , Ducts , Entropy , Flow (Dynamics) , Turbines , Vortices , Wakes , Nozzle guide vanes , Simulation , Cascades (Fluid dynamics)

A Data-Driven Method for the Derivation of Explicit Algebraic Reynolds Stress Models Applied to the Wake Losses of Low-Pressure Turbine Cascades

Johannes Deutsch, Nima Fard Afshar, Stefan Henninger, Peter Jeschke

J. Turbomach. June 2025, 147(6): 061007. doi: https://doi.org/10.1115/1.4067032

Abstract

View articletitled, A Data-Driven Method for the Derivation of Explicit Algebraic Reynolds Stress Models Applied to the Wake Losses of Low-Pressure Turbine Cascades

Open the PDF for in another window

Topics: Kinetic energy , Optimization , Pressure , Reynolds stress , Simulation , Turbines , Turbulence , Wakes , Reynolds-averaged Navier–Stokes equations , Tensors

Multidisciplinary Optimization of a Mixed-Flow Impeller With 140 Parameters and Its Shapley Additive Explanations

Guang Xi, Yong Zhang, Cheng Ji, Chenqing Zhang

J. Turbomach. June 2025, 147(6): 061008. doi: https://doi.org/10.1115/1.4067030

Abstracts

View articletitled, Multidisciplinary Optimization of a Mixed-Flow Impeller With 140 Parameters and Its Shapley Additive Explanations

Open the PDF for in another window

Topics: Blades , Flow (Dynamics) , Impellers , Optimization , Design , Shapes

Robust Design Optimization of a Compressor Rotor Using Recursive Cokriging Based Multi-Fidelity Uncertainty Quantification and Multi-Fidelity Optimization

Marcus Wiegand, Andriy Prots, Marcus Meyer, Robin Schmidt, Matthias Voigt, Ronald Mailach

J. Turbomach. June 2025, 147(6): 061009. doi: https://doi.org/10.1115/1.4067076

Abstract

View articletitled, Robust Design Optimization of a Compressor Rotor Using Recursive Cokriging Based Multi-Fidelity Uncertainty Quantification and Multi-Fidelity Optimization

Open the PDF for in another window

Topics: Compressors , Design , Optimization , Uncertainty quantification

Integration of Cooling Holes Into a Turbine Vane Made Using Additive Manufacturing

Nicholas L. Gailey, Michael D. Barringer, Reid A. Berdanier, Karen A. Thole

J. Turbomach. June 2025, 147(6): 061010. doi: https://doi.org/10.1115/1.4067100

Abstracts

View articletitled, Integration of Cooling Holes Into a Turbine Vane Made Using Additive Manufacturing

Open the PDF for in another window

Topics: Cooling , Flow (Dynamics) , Film cooling

Numerical Investigation on the Influence of Wet Compression Aerodynamic Performance of Multi-Stage Transonic Compressor

Zihuan Zhu, Yadong Wu, Lele Ming, Xinze Zhang, Hua Ouyang

J. Turbomach. June 2025, 147(6): 061011. doi: https://doi.org/10.1115/1.4067101

Abstracts

View articletitled, Numerical Investigation on the Influence of Wet Compression Aerodynamic Performance of Multi-Stage Transonic Compressor

Open the PDF for in another window

Topics: Compression , Compressors , Drops , Plasma spraying , Spraying (Coating processes) , Wireless power transfer , Pressure , Temperature , Water

Scale Cooling—A Novel Fractal Cooling Structure for Turbine Vanes

Zhongran Chi, Longfei Wang

J. Turbomach. June 2025, 147(6): 061012. doi: https://doi.org/10.1115/1.4067099

Abstract

View articletitled, Scale Cooling—A Novel Fractal Cooling Structure for Turbine Vanes

Open the PDF for in another window

Topics: Cooling , Fractals , Design , Heat transfer , Computational fluid dynamics

All Issues

Email alerts

Accepted Manuscript Alert

New Issue Alert

RSS Feeds

Open Issues RSS Feed

Latest
Most Read
Most Cited

ON THE APPLICATION OF BACKGROUND ORIENTED SCHLIEREN TO A TRANSONIC LOW-REYNOLDS TURBINE CASCADE

J. Turbomach

NUMERICAL SIMULATIONS AND SENSITIVITY ANALYSIS OF ICE FORMATION ON FAN BLADES

J. Turbomach

UNSTEADY LOSS MECHANISMS IN LOW-PRESSURE TURBINES WITH DIVERGING END-WALLS STUDIED VIA HIGH-FIDELITY SIMULATION

J. Turbomach

EFFECT OF FLOW DISTORTIONS ON PIN FINS IN THE ENTRY REGION OF CIRCULAR CHANNELS

J. Turbomach

Unsteady Flow Mechanism of Corner Separation Control Using Blade End Slots in a Highly Loaded Compressor Cascade

J. Turbomach

Research Papers

Spectral Heat Transfer Coefficient for Thermal Design Analysis—Part 1: Augmenting the Cooling Law for Non-Isothermal Wall

Spectral Heat Transfer Coefficient for Thermal Design Analysis—Part II: Leveraging Diabatic Wall Conditioning for Nonlinear Regime

Introduction of Axisymmetric Grooves as a Tip Seal Treatment for Small-Core Turbines

Optimization of Tip Seal Grooves for Aerodynamic and Durability Improvements of Small-Core Turbines

Understanding the Flow Field in a Highly Loaded Tandem Compressor Cascade

Loss Breakdown in Axial Turbines: A New Method for Vortex Loss and Wake Detection From 3D RANS Simulations

A Data-Driven Method for the Derivation of Explicit Algebraic Reynolds Stress Models Applied to the Wake Losses of Low-Pressure Turbine Cascades

Multidisciplinary Optimization of a Mixed-Flow Impeller With 140 Parameters and Its Shapley Additive Explanations

Robust Design Optimization of a Compressor Rotor Using Recursive Cokriging Based Multi-Fidelity Uncertainty Quantification and Multi-Fidelity Optimization

Integration of Cooling Holes Into a Turbine Vane Made Using Additive Manufacturing

Numerical Investigation on the Influence of Wet Compression Aerodynamic Performance of Multi-Stage Transonic Compressor

Scale Cooling—A Novel Fractal Cooling Structure for Turbine Vanes

Email alerts

RSS Feeds

ASME Journals

ASME Conference Proceedings

ASME eBooks

Resources

Opportunities

Issues

Research Papers

Email alerts

RSS Feeds

ASME Journals

ASME Conference Proceedings

ASME eBooks

Resources

Opportunities

This Feature Is Available To Subscribers Only