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Journal Articles

An Insight into Quasi-Two-Dimensional Flow Features Over Turbine Blading From the Works of Jonathan Paul Gostelow

Aldo Rona, David S. Adebayo, Jonathan Paul Gostelow

J. Turbomach. September 2023, 145(9): 090801.

Paper No: TURBO-22-1290

https://doi.org/10.1115/1.4062552

Published Online: June 9, 2023

View Article titled, An Insight into Quasi-Two-Dimensional Flow Features Over Turbine Blading From the Works of Jonathan Paul Gostelow

Topics: Blades, Boundary layers, Flow (Dynamics), Separation (Technology), Turbomachinery, Turbulence, Vortex shedding, Pressure, Vorticity, Shock (Mechanics)

Journal Articles

The Role of Endwall Shape Optimization in the Design of Supersonic Turbines for Rotating Detonation Engines

Noraiz Mushtaq, Giacomo Persico, Paolo Gaetani

J. Turbomach. August 2023, 145(8): 081015.

Paper No: TURBO-22-1161

https://doi.org/10.1115/1.4062277

Published Online: May 22, 2023

View Article titled, The Role of Endwall Shape Optimization in the Design of Supersonic Turbines for Rotating Detonation Engines

Topics: Blades, Design, Flow (Dynamics), Rotors, Shape optimization, Stators, Turbines, Optimization, Explosions, Mach number

Journal Articles

Investigation of Surge in a Transonic Centrifugal Compressor With Vaned Diffuser: Part II—Correlation With Subcomponent Characteristics

Fangyuan Lou, Herbert M. Harrison, William J. Brown, Nicole L. Key

J. Turbomach. May 2023, 145(5): 051004.

Paper No: TURBO-22-1147

https://doi.org/10.1115/1.4055865

Published Online: November 8, 2022

View Article titled, Investigation of Surge in a Transonic Centrifugal Compressor With Vaned Diffuser: Part II—Correlation With Subcomponent Characteristics

Topics: Compressors, Diffusers, Flow (Dynamics), Impellers, Pressure, Stability, Surges, Mach number, Shock (Mechanics)

Journal Articles

A Data-Driven Tip Flow Loss Prediction Method for a Transonic Fan Under Boundary Layer Ingesting Inflow Distortion

Zhe Yang, Hanan Lu, Tianyu Pan, Qiushi Li

J. Turbomach. January 2023, 145(1): 011001.

Paper No: TURBO-21-1236

https://doi.org/10.1115/1.4055439

Published Online: October 3, 2022

View Article titled, A Data-Driven Tip Flow Loss Prediction Method for a Transonic Fan Under Boundary Layer Ingesting Inflow Distortion

Topics: Annulus, Blades, Design, Flow (Dynamics), Inflow, Physics, Rotors, Computational fluid dynamics, Boundary layers, Errors

Journal Articles

A Shock Loss Reduction Method Using a Concave Suction Side Profile for a Zero Inlet Swirl Turbine Rotor

Qinghui Zhou, Wei Zhao, Xiuming Sui, Qingjun Zhao, Jianzhong Xu

J. Turbomach. November 2022, 144(11): 111010.

Paper No: TURBO-21-1270

https://doi.org/10.1115/1.4055067

Published Online: September 13, 2022

View Article titled, A Shock Loss Reduction Method Using a Concave Suction Side Profile for a Zero Inlet Swirl Turbine Rotor

Topics: Blades, Flow (Dynamics), Shock (Mechanics), Suction, Turbines, Design, Rotors, Pressure

Journal Articles

A Detailed Loss Analysis Methodology for Centrifugal Compressors

Luying Zhang, Loukia Kritioti, Peng Wang, Jiangnan Zhang, Mehrdad Zangeneh

J. Turbomach. May 2022, 144(5): 051013.

Paper No: TURBO-21-1214

https://doi.org/10.1115/1.4054065

Published Online: March 31, 2022

View Article titled, A Detailed Loss Analysis Methodology for Centrifugal Compressors

Topics: Blades, Compressors, Design, Entropy, Flow (Dynamics), Impellers, Computational fluid dynamics, Optimization, Pressure, Shock (Mechanics)

Journal Articles

Automatic Design Optimization of a Transonic Compressor Rotor for Improving Aeroacoustic and Aerodynamic Performance

Long Wu, Jae-Wook Kim, Alexander George Wilson, Shahrokh Shahpar

J. Turbomach. August 2022, 144(8): 081016.

Paper No: TURBO-21-1084

https://doi.org/10.1115/1.4053916

Published Online: March 16, 2022

View Article titled, Automatic Design Optimization of a Transonic Compressor Rotor for Improving Aeroacoustic and Aerodynamic Performance

Topics: Blades, Design, Flow (Dynamics), Noise (Sound), Optimization, Rotors, Pressure, Shock (Mechanics), Simulation

Journal Articles

A Comprehensive Analytical Shock Loss Model for Axial Compressor Cascades

Milan Banjac, Teodora Savanovic, Djordje Petkovic, Milan V. Petrovic

J. Turbomach. September 2022, 144(9): 091003.

Paper No: TURBO-22-1012

https://doi.org/10.1115/1.4053852

Published Online: March 4, 2022

View Article titled, A Comprehensive Analytical Shock Loss Model for Axial Compressor Cascades

Topics: Flow (Dynamics), Geometry, Mach number, Pressure, Shock (Mechanics), Blades, Cascades (Fluid dynamics), Airfoils, Compressors

Journal Articles

Transonic Relief in Fans and Compressors

Demetrios Lefas, Robert J. Miller

J. Turbomach. May 2022, 144(5): 051001.

Paper No: TURBO-21-1183

https://doi.org/10.1115/1.4052755

Published Online: November 15, 2021

View Article titled, Transonic Relief in Fans and Compressors

Topics: Blades, Design, Mach number, Compressors, Shock (Mechanics), Suction

Journal Articles

Impacts of Tandem Configurations on the Aerodynamic Performance of an Axial Supersonic Through-Flow Fan Cascade

Shijun Sun, Jiaqi Hao, Jutao Yang, Ling Zhou, Lucheng Ji

J. Turbomach. April 2022, 144(4): 041009.

Paper No: TURBO-21-1035

https://doi.org/10.1115/1.4052689

Published Online: November 11, 2021

View Article titled, Impacts of Tandem Configurations on the Aerodynamic Performance of an Axial Supersonic Through-Flow Fan Cascade

Topics: Blades, Cascades (Fluid dynamics), Chords (Trusses), Design, Flow (Dynamics), Pressure, Shock (Mechanics), Wakes, Mach number

Journal Articles

High-Fidelity Simulations of a High-Pressure Turbine Vane Subject to Large Disturbances: Effect of Exit Mach Number on Losses

Yaomin Zhao, Richard D. Sandberg

J. Turbomach. September 2021, 143(9): 091002.

Paper No: TURBO-20-1392

https://doi.org/10.1115/1.4050453

Published Online: May 3, 2021

View Article titled, High-Fidelity Simulations of a High-Pressure Turbine Vane Subject to Large Disturbances: Effect of Exit Mach Number on Losses

Topics: Blades, Boundary layers, Entropy, Flow (Dynamics), Mach number, Shock (Mechanics), Simulation, Turbulence, Turbines, Pressure

Journal Articles

Single and Multiple Circumferential Casing Groove for Stall Margin Improvement in a Transonic Axial Compressor

A. F. Mustaffa, V. Kanjirakkad

J. Turbomach. July 2021, 143(7): 071010.

Paper No: TURBO-20-1375

https://doi.org/10.1115/1.4050444

Published Online: April 19, 2021

View Article titled, Single and Multiple Circumferential Casing Groove for Stall Margin Improvement in a Transonic Axial Compressor

Topics: Compressors, Design, Shock (Mechanics), Vortices, Leakage, Blades, Rotors, Pressure

Journal Articles

Dynamics of Shock Waves Interacting With Laminar Separated Transonic Turbine Flow Investigated by High-Speed Schlieren and Surface Hot-Film Sensors

Marcel Börner, Reinhard Niehuis

J. Turbomach. May 2021, 143(5): 051010.

Paper No: TURBO-20-1249

https://doi.org/10.1115/1.4050330

Published Online: April 13, 2021

View Article titled, Dynamics of Shock Waves Interacting With Laminar Separated Transonic Turbine Flow Investigated by High-Speed Schlieren and Surface Hot-Film Sensors

Topics: Boundary layers, Flow (Dynamics), Mach number, Sensors, Separation (Technology), Shock waves, Turbines, Suction, Cascades (Fluid dynamics), Bubbles

Journal Articles

On the Importance of Transition Control at Transonic Compressor Blades

Alexander Hergt, J. Klinner, S. Grund, C. Willert, W. Steinert, M. Beversdorff

J. Turbomach. March 2021, 143(3): 031007.

Paper No: TURBO-20-1102

https://doi.org/10.1115/1.4049783

Published Online: March 1, 2021

View Article titled, On the Importance of Transition Control at Transonic Compressor Blades

Topics: Blades, Boundary layers, Cascades (Fluid dynamics), Compressors, Oscillations, Shock (Mechanics), Flow (Dynamics), Separation (Technology), Suction, Flow control

Journal Articles

New Supersonic Loss Model for the Preliminary Design of Transonic Turbine Blades and the Influence of Pitch

Luis Teia

J. Turbomach. April 2020, 142(4): 041008.

Paper No: TURBO-19-1007

https://doi.org/10.1115/1.4045983

Published Online: March 17, 2020

View Article titled, New Supersonic Loss Model for the Preliminary Design of Transonic Turbine Blades and the Influence of Pitch

Topics: Design, Mach number, Shock (Mechanics), Blades, Chords (Trusses), Turbines, Turbine blades, Pressure

Journal Articles

Flutter in Started and Unstarted Transonic Linear Cascades: Simultaneous Measurements of Unsteady Loads and Shock Dynamics

Prahallada Jutur, Raghuraman N. Govardhan

J. Turbomach. December 2019, 141(12): 121004.

Paper No: TURBO-19-1085

https://doi.org/10.1115/1.4045105

Published Online: November 8, 2019

View Article titled, Flutter in Started and Unstarted Transonic Linear Cascades: Simultaneous Measurements of Unsteady Loads and Shock Dynamics

Topics: Blades, Cascades (Fluid dynamics), Flutter (Aerodynamics), Shock (Mechanics), Excitation, Dynamics (Mechanics), Oscillations, Stress, Pressure, Suction

Journal Articles

Application of the Quantitative Monochrome Calibrated Schlieren Technique in a Highly Loaded Turbine Cascade Test

Zhihong Zhou, Haotian Wang, Huoxing Liu

J. Turbomach. November 2019, 141(11): 111007.

Paper No: TURBO-19-1179

https://doi.org/10.1115/1.4045088

Published Online: October 22, 2019

View Article titled, Application of the Quantitative Monochrome Calibrated Schlieren Technique in a Highly Loaded Turbine Cascade Test

Topics: Cascades (Fluid dynamics), Density, Flow (Dynamics), Pressure, Schlieren methods, Shock (Mechanics), Turbines, Blades, Boundary-value problems, Shock waves

Journal Articles

Toward Future Installations: Mutual Interactions of Short Intakes With Modern High Bypass Fans

Nagabhushana Rao Vadlamani, Teng Cao, Rob Watson, Paul G. Tucker

J. Turbomach. August 2019, 141(8): 081013.

Paper No: TURBO-19-1024

https://doi.org/10.1115/1.4044080

Published Online: July 26, 2019

View Article titled, Toward Future Installations: Mutual Interactions of Short Intakes With Modern High Bypass Fans

Topics: Blades, Design, Flow (Dynamics), Pressure, Rotors, Separation (Technology), Shock (Mechanics), Simulation, Mach number, Engines

Journal Articles

The Present Challenge of Transonic Compressor Blade Design

Alexander Hergt, J. Klinner, J. Wellner, C. Willert, S. Grund, W. Steinert, M. Beversdorff

J. Turbomach. September 2019, 141(9): 091004.

Paper No: TURBO-18-1244

https://doi.org/10.1115/1.4043329

Published Online: May 30, 2019

View Article titled, The Present Challenge of Transonic Compressor Blade Design

Topics: Blades, Boundary layers, Cascades (Fluid dynamics), Compressors, Design, Flow (Dynamics), Shock (Mechanics), Shock waves, Turbulence, Suction

Journal Articles

Using Shock Control Bumps to Improve Transonic Fan/Compressor Blade Performance

Alistair John, Ning Qin, Shahrokh Shahpar

J. Turbomach. August 2019, 141(8): 081003.

Paper No: TURBO-18-1271

https://doi.org/10.1115/1.4042891

Published Online: March 2, 2019

View Article titled, Using Shock Control Bumps to Improve Transonic Fan/Compressor Blade Performance

Topics: Blades, Design, Flow (Dynamics), Geometry, Optimization, Shock (Mechanics), Separation (Technology), Rotors, Compressors

Journal citation

NARROW

An Insight into Quasi-Two-Dimensional Flow Features Over Turbine Blading From the Works of Jonathan Paul Gostelow

The Role of Endwall Shape Optimization in the Design of Supersonic Turbines for Rotating Detonation Engines

Investigation of Surge in a Transonic Centrifugal Compressor With Vaned Diffuser: Part II—Correlation With Subcomponent Characteristics

A Data-Driven Tip Flow Loss Prediction Method for a Transonic Fan Under Boundary Layer Ingesting Inflow Distortion

A Shock Loss Reduction Method Using a Concave Suction Side Profile for a Zero Inlet Swirl Turbine Rotor

A Detailed Loss Analysis Methodology for Centrifugal Compressors

Automatic Design Optimization of a Transonic Compressor Rotor for Improving Aeroacoustic and Aerodynamic Performance

A Comprehensive Analytical Shock Loss Model for Axial Compressor Cascades

Transonic Relief in Fans and Compressors

Impacts of Tandem Configurations on the Aerodynamic Performance of an Axial Supersonic Through-Flow Fan Cascade

High-Fidelity Simulations of a High-Pressure Turbine Vane Subject to Large Disturbances: Effect of Exit Mach Number on Losses

Single and Multiple Circumferential Casing Groove for Stall Margin Improvement in a Transonic Axial Compressor

Dynamics of Shock Waves Interacting With Laminar Separated Transonic Turbine Flow Investigated by High-Speed Schlieren and Surface Hot-Film Sensors

On the Importance of Transition Control at Transonic Compressor Blades

New Supersonic Loss Model for the Preliminary Design of Transonic Turbine Blades and the Influence of Pitch

Flutter in Started and Unstarted Transonic Linear Cascades: Simultaneous Measurements of Unsteady Loads and Shock Dynamics

Application of the Quantitative Monochrome Calibrated Schlieren Technique in a Highly Loaded Turbine Cascade Test

Toward Future Installations: Mutual Interactions of Short Intakes With Modern High Bypass Fans

The Present Challenge of Transonic Compressor Blade Design

Using Shock Control Bumps to Improve Transonic Fan/Compressor Blade Performance

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