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Journal Articles

Reconstruction and Reduction of Realistic Manufacturing Error Field for Uncertainty Quantification of Transonic Axial Compressor Rotor

Benrui Zhang, Yaping Ju, Zhen Li, Xiawen Zhang, Yiming Liu, Chuhua Zhang

Publisher: ASME

J. Turbomach.

Paper No: TURBO-25-1029

https://doi.org/10.1115/1.4069132

Published Online: July 9, 2025

... Turbine Institute (IGTI) of ASME for publication in the J ournal of T urbomachinery . 15 02 2025 03 07 2025 07 07 2025 09 07 2025 Fan, compressor, and turbine aerodynamic design Turbomachinery blading design Accepted Manuscript Not Copyedited Journal of Turbomachinery...

View Articletitled, Reconstruction and Reduction of Realistic Manufacturing Error Field for Uncertainty Quantification of Transonic Axial Compressor Rotor

Topics: Compressors, Design, Errors, Manufacturing, Rotors, Turbochargers, Uncertainty quantification

Journal Articles

Multi-Aeroelastic Phenomena Modelling Part II: Application for the Evaluation of Fan OGV Cyclic Pattern Designs

Davendu Kulkarni, Luca di Mare

Publisher: ASME

J. Turbomach.

Paper No: TURBO-24-1251

https://doi.org/10.1115/1.4068948

Published Online: June 16, 2025

... (CFD) Fan, compressor, and turbine aerodynamic design Turbomachinery blading design Rolls-Royce 10.13039/501100000767 10064212 Accepted Manuscript Not Copyedited Journal of Turbomachinery. Received August 16, 2024; Accepted manuscript posted June 16, 2025. doi:10.1115/1.4068948...

View Articletitled, Multi-Aeroelastic Phenomena Modelling Part II: Application for the Evaluation of Fan OGV Cyclic Pattern Designs

Topics: Architecture, Compressors, Computational fluid dynamics, Design, Engineering simulation, Engines, Flight, Geometry, Guide vanes, Modeling

Journal Articles

A Novel Design Concept for Highly-Loaded Compressor Airfoils

A. Hergt, O. Reutter, S. Grund

Publisher: ASME

J. Turbomach. December 2025, 147(12): 121002.

Paper No: TURBO-24-1378

https://doi.org/10.1115/1.4068689

Published Online: June 5, 2025

... = measurement plane 2 (exit) OP 1 = operating point 1 toward choke OP 2 = operating point 2 toward stability limit RANS = Reynolds-averaged Navier–Stokes fan axial compressor aerodynamic design turbomachinery blading design References [1] Herrig , L. J...

View Articletitled, A Novel Design Concept for Highly-Loaded Compressor Airfoils

Topics: Airfoils, Cascades (Fluid dynamics), Design, Compressors, Blades

Journal Articles

Compressor Blade Shaping and Optimization Through Design Features Based on Free-Form Deformation

Xin Li, Tongtong Meng, Ling Zhou, Lucheng Ji

Publisher: ASME

J. Turbomach. November 2025, 147(11): 111009.

Paper No: TURBO-24-1317

https://doi.org/10.1115/1.4068597

Published Online: May 20, 2025

... for compressor design was proposed. fan compressor and turbine aerodynamic design turbomachinery blading design In today’s competitive environment, the demand for improvements in gas turbine engines is still relentless, which is generally reflected in very high-pressure ratios while operating...

View Articletitled, Compressor Blade Shaping and Optimization Through Design Features Based on Free-Form Deformation

Topics: Blades, Deformation, Design, Optimization, Flow (Dynamics)

Journal Articles

Inverse Design of Compressor/Fan Blade Profiles Based on Conditional Invertible Neural Networks

Xinkai Jia, Xiuquan Huang, Shouyong Jiang, Dingxi Wang, Christian Maria Firrone

Publisher: ASME

J. Turbomach. October 2025, 147(10): 101014.

Paper No: TURBO-24-1150

https://doi.org/10.1115/1.4068386

Published Online: May 2, 2025

[email protected] 1 Corresponding author. Email: [email protected] Email: [email protected] Email: [email protected] Email: [email protected] fan compressor fan/compressor aerodynamic design turbomachinery blading design References [1] Gorla...

View Articletitled, Inverse Design of Compressor/Fan Blade Profiles Based on Conditional Invertible Neural Networks

Topics: Design, Artificial neural networks, Modeling, Blades, Compressors

Journal Articles

IMPACT OF TEMPERATURE RATIO ON OVERALL COOLING EFFECTIVENESS: EXPERIMENTAL VALIDATION OF A SCALING THEORY

James Cartlidge, Aravin Dass Naidu, Nafiz Chowdhury, Thomas Povey

Publisher: ASME

J. Turbomach.

Paper No: TURBO-24-1271

https://doi.org/10.1115/1.4068460

Published Online: April 16, 2025

... transfer and film cooling Measurement techniques turbine blade and measurement advancements Turbomachinery blading design Journal of Turbomachinery. Received August 20, 2024; Accepted manuscript posted April 16, 2025. doi:10.1115/1.4068460 Copyright © 2025 by ASME; reuse license CC-BY 4.0 IMPACT...

View Articletitled, IMPACT OF TEMPERATURE RATIO ON OVERALL COOLING EFFECTIVENESS: EXPERIMENTAL VALIDATION OF A SCALING THEORY

Topics: Cooling, Temperature, Turbochargers, Coolants, Heat transfer, Heat transfer coefficients, Boundary-value problems, Compressors, Design, Engines

Journal Articles

An Unsteady Deposition Model for Evaluating CMAS Nonuniform Deposition Behavior and Aerodynamic Performance Degradation Under Hot Streak Clocking Effect

Li Shi, Xiao Tan, Rongli Deng, Liang Su, Jinfeng Peng, Jiasheng Song, Junjie Chen

Publisher: ASME

J. Turbomach. October 2025, 147(10): 101012.

Paper No: TURBO-24-1282

https://doi.org/10.1115/1.4068227

Published Online: April 8, 2025

... 03 2025 08 04 2025 gas turbines cooling computational fluid dynamics (CFD) thermodynamics two-phase fluid dynamics and heat transfer phenomena in compressor and turbine components of gas turbine engines turbomachinery blading design During the operation of land-based...

View Articletitled, An Unsteady Deposition Model for Evaluating CMAS Nonuniform Deposition Behavior and Aerodynamic Performance Degradation Under Hot Streak Clocking Effect

Topics: Particulate matter, Temperature, Pressure, Suction

Journal Articles

Nature of Transonic Compressor Flow and Its 3D Design Implications

Demetrios Lefas

Publisher: ASME

J. Turbomach. October 2025, 147(10): 101008.

Paper No: TURBO-24-1341

https://doi.org/10.1115/1.4067994

Published Online: April 1, 2025

... fan and compressor aerodynamic design computational fluid dynamics (CFD) turbomachinery blading design References [1] Lieblein , S. , and Johnsen , I. A. , 1961 , “ Resume of Transonic Compressor Research at NACA Lewis Laboratory ,” ASME J. Eng. Power , 83 ( 3...

View Articletitled, Nature of Transonic Compressor Flow and Its 3D Design Implications

Topics: Blades, Compressors, Design, Flow (Dynamics), Mach number, Shock (Mechanics), Computational fluid dynamics, Pressure

Journal Articles

Impact of Trailing Edge Damage on Nozzle Guide Vane Aerodynamic Performance

Zelimhan Raduev, Dougal Jackson, Nafiz Chowdhury, Thomas Povey

Publisher: ASME

J. Turbomach. October 2025, 147(10): 101007.

Paper No: TURBO-24-1291

https://doi.org/10.1115/1.4067930

Published Online: March 20, 2025

... turbine blade and measurement advancements turbomachinery blading design vortex shedding turbine component erosion In operational engines, transonic high-pressure (HP) nozzle guide vanes (NGVs) are subject to trailing edge (TE) erosion and oxidation damage (or, so-called, burn-back ). Loss...

View Articletitled, Impact of Trailing Edge Damage on Nozzle Guide Vane Aerodynamic Performance

Topics: Computational fluid dynamics, Flow (Dynamics), Geometry, Pressure, Coolants, Damage, Nozzle guide vanes, Mach number, Boundary layers, Vortices

Journal Articles

Gradient-Free Aerodynamic Optimization With Structural Constraints and Surge Line Control for Radial Compressor Stage

Robert Schaffrath, Eberhard Nicke, Nicolai Forsthofer, Oliver Kunc, Christian Voß

Publisher: ASME

J. Turbomach. September 2025, 147(9): 091018.

Paper No: TURBO-23-1121

https://doi.org/10.1115/1.4067687

Published Online: February 18, 2025

... for publication in the J ournal of T urbomachinery . 11 07 2023 27 03 2024 27 03 2024 18 02 2025 radial compressor aero-structure optimization water steam centrifugal compressors and pumps computational fluid dynamics (CFD) turbomachinery blading design Global warming...

View Articletitled, Gradient-Free Aerodynamic Optimization With Structural Constraints and Surge Line Control for Radial Compressor Stage

Topics: Compressors, Computational fluid dynamics, Geometry, Optimization, Blades, Parametrization, Surges, Simulation, Impellers, Pressure

Journal Articles

Design and Analysis of a Liftfan for eVTOL Aircraft

R. D. Hine, D. R. Cousins, L. Maden, S. J. Walker, N. R. Atkins, S. D. Grimshaw, J. V. Taylor

Publisher: ASME

J. Turbomach. September 2025, 147(9): 091016.

Paper No: TURBO-24-1308

https://doi.org/10.1115/1.4067673

Published Online: February 17, 2025

... fluid dynamics (CFD) fan compressor aerodynamic design fluid dynamics and heat transfer phenomena in compressor turbomachinery blading design electric vertical take-off and landing aircraft The increasing demand for emission free air transport is driving a global market for electrified...

View Articletitled, Design and Analysis of a Liftfan for eVTOL Aircraft

Topics: Cooling, Design, Engines, Flight, Flow (Dynamics), Motors, Pressure, Engineering prototypes, Simulation, Computational fluid dynamics

Journal Articles

Effect of Blade Damage on Low Pressure Ratio Fan Windmill Aerodynamics

Sofía I. Medina Cassillas, Alejandro Castillo Pardo, Cesare A. Hall, Ben Mohankumar

Publisher: ASME

J. Turbomach. September 2025, 147(9): 091008.

Paper No: TURBO-24-1320

https://doi.org/10.1115/1.4067518

Published Online: February 14, 2025

... design measurement techniques turbomachinery blading design The windmill condition occurs after the in-flight shutdown of a turbofan when the ram pressure of the oncoming air causes the fan to freewheel. Fan windmill often follows damage to the fan due to foreign object ingestion, birdstrike...

View Articletitled, Effect of Blade Damage on Low Pressure Ratio Fan Windmill Aerodynamics

Topics: Blades, Damage, Flow (Dynamics), Pressure, Rotors, Wire, Probes

Journal Articles

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

Yangwei Liu, Weibo Zhong, Yumeng Tang

Publisher: ASME

J. Turbomach. June 2025, 147(6): 061016.

Paper No: TURBO-24-1240

https://doi.org/10.1115/1.4067295

Published Online: January 13, 2025

.../compressor and turbine aerodynamic design turbomachinery blading design High efficiency and high-loading compressors are the key components of advanced modern aero-engines [ 1 ]. However, the aerodynamic design, aeroelastic problems, and numerical prediction of compressors are permanent challenges...

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

Topics: Blades, Corners (Structural elements), Flow (Dynamics), Separation (Technology), Vortices, Unsteady flow, Pressure

Journal Articles

Experimental and Numerical Comparison of Two Turbine Vane Frame Designs

Nicolas Krajnc, Asim Hafizovic, Lukas Wiesinger, Francesco Mangini, Patrick Zeno Sterzinger, Marios Patinios, Emil Göttlich

Publisher: ASME

J. Turbomach. August 2025, 147(8): 081005.

Paper No: TURBO-24-1212

https://doi.org/10.1115/1.4067321

Published Online: January 13, 2025

... TVF1 and TVF2, (b) purge derivatives of TVF1, and (c) purge derivatives of TVF2 01 08 2024 28 10 2024 28 10 2024 13 01 2025 Graphical Abstract Figure TTTF scheme TTTF scheme computational fluid dynamics (CFD) turbomachinery blading design...

View Articletitled, Experimental and Numerical Comparison of Two Turbine Vane Frame Designs

Topics: Flow (Dynamics), Pressure, Turbines, Design, Ducts, Vortices

Journal Articles

Film Cooling and Thermal Performances of a Blade Tip Winglet Operated in an Annular Test Rig and a Test Gas Turbine Power Plant

Shailendra Naik, Marc Henze, Manuel Wilhelm, Heinz-Peter Schiffer

Publisher: ASME

J. Turbomach. February 2025, 147(2): 021013.

Paper No: TURBO-24-1243

https://doi.org/10.1115/1.4067237

Published Online: December 17, 2024

... in the J ournal of T urbomachinery . 15 08 2024 16 10 2024 16 10 2024 17 12 2024 Graphical Abstract Figure heat transfer and film cooling measurement techniques turbomachinery blading design Bundesministerium für Wirtschaft und Energie 10.13039...

View Articletitled, Film Cooling and Thermal Performances of a Blade Tip Winglet Operated in an Annular Test Rig and a Test Gas Turbine Power Plant

Topics: Blades, Coolants, Cooling, Film cooling, Gas turbines, Temperature, Pressure, Power stations, Flow (Dynamics), Cavities

Journal Articles

Targeting Full-Hydrogen Operation on Industrial-Scale Gas Turbines: Impact of Unconventional Fuels on Turbine Module Performance and Aeromechanics

Alberto Bandini, Claudio Bettini, Lorenzo Peruzzi, Mauro Carretta, Claudio Canelli, Michele Marconcini, Lorenzo Pinelli, Andrea Arnone

Publisher: ASME

J. Turbomach. July 2025, 147(7): 071008.

Paper No: TURBO-24-1277

https://doi.org/10.1115/1.4067127

Published Online: December 11, 2024

... computational fluid dynamics (CFD) turbomachinery blading design variation of the flowrate at the turbine inlet, which, in turn, affects the turbine/compressor coupling variation of the enthalpy drop during the expansion variation of the heat transfer coefficient on the turbine blades, which...

View Articletitled, Targeting Full-Hydrogen Operation on Industrial-Scale Gas Turbines: Impact of Unconventional Fuels on Turbine Module Performance and Aeromechanics

Topics: Computational fluid dynamics, Fuels, Gas turbines, Hydrogen, Temperature, Turbines, Aeroelasticity, Blades, Design, Methane

Journal Articles

MULTI-AEROELASTIC PHENOMENA MODELLING PART I: THE DEVELOPMENT OF WHOLE LPC MODEL FOR CIVIL TURBOFAN ENGINE

Davendu Kulkarni, Bharat Lad, Luca di Mare

Publisher: ASME

J. Turbomach.

Paper No: TURBO-24-1250

https://doi.org/10.1115/1.4067353

Published Online: December 6, 2024

... (CFD) Fan, compressor, and turbine aerodynamic design Turbomachinery blading design Accepted Manuscript Not Copyedited Journal of Turbomachinery. Received August 16, 2024; Accepted manuscript posted December 6, 2024. doi:10.1115/1.4067353 Copyright © 2024 bAy SRMollEs-RJooyucrenpallcof...

View Articletitled, MULTI-AEROELASTIC PHENOMENA MODELLING PART I: THE DEVELOPMENT OF WHOLE LPC MODEL FOR CIVIL TURBOFAN ENGINE

Topics: Computational fluid dynamics, Design, Engines, Modeling, Turbochargers, Turbofans, Simulation, Compression, High cycle fatigue, Pressure

Journal Articles

Understanding the Flow Field in a Highly Loaded Tandem Compressor Cascade

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

Publisher: ASME

J. Turbomach. June 2025, 147(6): 061005.

Paper No: TURBO-24-1180

https://doi.org/10.1115/1.4067029

Published Online: November 22, 2024

... the diffusion taking place in the blade passage. An alternative approach consists of distributing the load over two subsequent airfoils, using a so-called tandem blade configuration to restart the boundary layer before flow separation occurs [ 3 ]. boundary layer development turbomachinery blading...

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

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

Journal Articles

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

Publisher: ASME

J. Turbomach. June 2025, 147(6): 061006.

Paper No: TURBO-24-1184

https://doi.org/10.1115/1.4067033

Published Online: November 22, 2024

... for publication in the J ournal of T urbomachinery . 24 07 2024 18 10 2024 18 10 2024 22 11 2024 Graphical Abstract Figure computational fluid dynamics (CFD) turbine aerodynamic design turbomachinery blading design entropy loss loss audit vortices, wakes...

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

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

Journal Articles

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

Publisher: ASME

J. Turbomach. June 2025, 147(6): 061009.

Paper No: TURBO-24-1192

https://doi.org/10.1115/1.4067076

Published Online: November 22, 2024

... fluid dynamics (CFD) compressor and turbine aerodynamic design turbomachinery blading design uncertainty quantification optimization robust optimization multi-fidelity To reduce climate-damaging emissions and to enhance the cost-effectiveness of jet engines, the efficiency of engine...

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

Topics: Compressors, Design, Optimization, Uncertainty quantification

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Reconstruction and Reduction of Realistic Manufacturing Error Field for Uncertainty Quantification of Transonic Axial Compressor Rotor

Multi-Aeroelastic Phenomena Modelling Part II: Application for the Evaluation of Fan OGV Cyclic Pattern Designs

A Novel Design Concept for Highly-Loaded Compressor Airfoils

Compressor Blade Shaping and Optimization Through Design Features Based on Free-Form Deformation

Inverse Design of Compressor/Fan Blade Profiles Based on Conditional Invertible Neural Networks

IMPACT OF TEMPERATURE RATIO ON OVERALL COOLING EFFECTIVENESS: EXPERIMENTAL VALIDATION OF A SCALING THEORY

An Unsteady Deposition Model for Evaluating CMAS Nonuniform Deposition Behavior and Aerodynamic Performance Degradation Under Hot Streak Clocking Effect

Nature of Transonic Compressor Flow and Its 3D Design Implications

Impact of Trailing Edge Damage on Nozzle Guide Vane Aerodynamic Performance

Gradient-Free Aerodynamic Optimization With Structural Constraints and Surge Line Control for Radial Compressor Stage

Design and Analysis of a Liftfan for eVTOL Aircraft

Effect of Blade Damage on Low Pressure Ratio Fan Windmill Aerodynamics

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

Experimental and Numerical Comparison of Two Turbine Vane Frame Designs

Film Cooling and Thermal Performances of a Blade Tip Winglet Operated in an Annular Test Rig and a Test Gas Turbine Power Plant

Targeting Full-Hydrogen Operation on Industrial-Scale Gas Turbines: Impact of Unconventional Fuels on Turbine Module Performance and Aeromechanics

MULTI-AEROELASTIC PHENOMENA MODELLING PART I: THE DEVELOPMENT OF WHOLE LPC MODEL FOR CIVIL TURBOFAN ENGINE

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

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

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