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Proc. ASME. GT2021, Volume 2C: Turbomachinery — Design Methods and CFD Modeling for Turbomachinery; Ducts, Noise, and Component Interactions, V02CT34A013, June 7–11, 2021

Paper No: GT2021-59121

DOI: https://doi.org/10.1115/GT2021-59121

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Topics: Compressors, Topology, Design, Blades, Geometry, Computational fluid dynamics, Flow (Dynamics), Manufacturing, Noise (Sound), Optimization

Proceedings Papers

Transonic Relief in Fans and Compressors

Demetrios Lefas, Robert J. Miller

Proc. ASME. GT2020, Volume 2A: Turbomachinery, V02AT32A043, September 21–25, 2020

Paper No: GT2020-15064

DOI: https://doi.org/10.1115/GT2020-15064

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Topics: Compressors, Fans

Proceedings Papers

The Effect of Reaction on Compressor Performance

Krishan S. Chana, Robert J. Miller

Proc. ASME. GT2020, Volume 2A: Turbomachinery, V02AT32A047, September 21–25, 2020

Paper No: GT2020-15220

DOI: https://doi.org/10.1115/GT2020-15220

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Topics: Compressors, Boundary layers, Rotors, Stators, Centrifugal force, Design

Journal Articles

The Effect of Heat Transfer on Turbine Performance

Lachlan J. Jardine, Robert J. Miller

Mechanical Engineering. September 2020, 142(09): 56–57.

Paper No: ME-2020-SEP5

DOI: https://doi.org/10.1115/1.2020-SEP5

Published Online: September 1, 2020

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Topics: Heat transfer, Turbines, Blades, Temperature, Cooling

Journal Articles

The Impact of Combustor Turbulence on Turbine Loss Mechanisms

Masha Folk, Robert J. Miller, John D. Coull

J. Turbomach. September 2020, 142(9): 091009.

Paper No: TURBO-20-1040

DOI: https://doi.org/10.1115/1.4047615

Published Online: August 24, 2020

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Topics: Boundary layers, Combustion chambers, Turbulence, Turbines

Proceedings Papers

The Effect of Heat Transfer on Turbine Performance

Lachlan J. Jardine, Robert J. Miller

Proc. ASME. GT2019, Volume 5A: Heat Transfer, V05AT10A010, June 17–21, 2019

Paper No: GT2019-91556

DOI: https://doi.org/10.1115/GT2019-91556

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Topics: Heat transfer, Turbines, Blades, Heat, Cooling, Design, Flow (Dynamics), Brayton cycle, Compressors, Computational fluid dynamics

Proceedings Papers

The Impact of Combustor Turbulence on Turbine Loss Mechanisms

Masha Folk, Robert J. Miller, John D. Coull

Proc. ASME. GT2019, Volume 2B: Turbomachinery, V02BT40A002, June 17–21, 2019

Paper No: GT2019-90307

DOI: https://doi.org/10.1115/GT2019-90307

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Topics: Combustion chambers, Turbines, Turbulence, Blades, Cascades (Fluid dynamics), Anisotropy, Boundary layer turbulence, Boundary layers, Chords (Trusses), Cross-flow

Journal Articles

The Effect of Aspect Ratio on Compressor Performance

Ho-On To, Robert J. Miller

J. Turbomach. August 2019, 141(8): 081011.

Paper No: TURBO-19-1026

DOI: https://doi.org/10.1115/1.4043219

Published Online: April 15, 2019

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Topics: Blades, Compressors, Design, Flow (Dynamics), Pressure, Clearances (Engineering), Chords (Trusses), Computational fluid dynamics

Journal Articles

The Effect of Nonequilibrium Boundary Layers on Compressor Performance

Andrew P. S. Wheeler, Anthony M. J. Dickens, Robert J. Miller

J. Turbomach. October 2018, 140(10): 101003.

Paper No: TURBO-18-1057

DOI: https://doi.org/10.1115/1.4040094

Published Online: September 28, 2018

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Topics: Boundary layers, Compressors, Flow (Dynamics), Reynolds number, Shear (Mechanics), Simulation, Suction, Turbulence, Energy dissipation, Blades

Proceedings Papers

The Effect of Non-Equilibrium Boundary Layers on Compressor Performance

Andrew P. S. Wheeler, Anthony M. J. Dickens, Robert J. Miller

Proc. ASME. GT2017, Volume 2B: Turbomachinery, V02BT41A040, June 26–30, 2017

Paper No: GT2017-64635

DOI: https://doi.org/10.1115/GT2017-64635

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Topics: Boundary layers, Compressors, Equilibrium (Physics), Blades, Computer simulation, Reynolds number, Separation (Technology), Suction

Journal Articles

Design of Compressor Endwall Velocity Triangles

Kiran Auchoybur, Robert J. Miller

J. Turbomach. June 2017, 139(6): 061005.

Paper No: TURBO-16-1254

DOI: https://doi.org/10.1115/1.4035233

Published Online: February 1, 2017

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Topics: Blades, Compressors, Design, Flow (Dynamics), Pressure, Stators

Journal Articles

Competing Three-Dimensional Mechanisms in Compressor Flows

James V. Taylor, Robert J. Miller

J. Turbomach. February 2017, 139(2): 021009.

Paper No: TURBO-16-1210

DOI: https://doi.org/10.1115/1.4034685

Published Online: October 4, 2016

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Topics: Blades, Computational fluid dynamics, Corners (Structural elements), Design, Pressure gradient, Separation (Technology), Flow (Dynamics), Uncertainty, Compressors, Boundary layers

Proceedings Papers

Design of Compressor Endwall Velocity Triangles

Kiran Auchoybur, Robert J. Miller

Proc. ASME. GT2016, Volume 2A: Turbomachinery, V02AT37A038, June 13–17, 2016

Paper No: GT2016-57396

DOI: https://doi.org/10.1115/GT2016-57396

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Topics: Compressors, Design, Blades, Flow (Dynamics), Geometry, Degrees of freedom, Annulus, Boundary layers, Corners (Structural elements), Diffusion (Physics)

Journal Articles

The Limitations of Using “ R a ” to Describe Surface Roughness

Martin N. Goodhand, Karl Walton, Liam Blunt, Hang W. Lung, Robert J. Miller, Reg Marsden

J. Turbomach. October 2016, 138(10): 101003.

Paper No: TURBO-15-1210

DOI: https://doi.org/10.1115/1.4032280

Published Online: April 26, 2016

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Topics: Surface roughness, Reynolds number, Drag (Fluid dynamics)

Proceedings Papers

Competing 3D Mechanisms in Compressor Flows

James V. Taylor, Robert J. Miller

Proc. ASME. GT2015, Volume 2A: Turbomachinery, V02AT37A035, June 15–19, 2015

Paper No: GT2015-43322

DOI: https://doi.org/10.1115/GT2015-43322

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Topics: Compressors, Flow (Dynamics), Design, Pressure gradient, Blades, Aerodynamics, Chords (Trusses), Corners (Structural elements), Risk, Separation (Technology)

Proceedings Papers

The Effect of Aspect Ratio on Compressor Performance

Ho-On To, Robert J. Miller

Proc. ASME. GT2015, Volume 2A: Turbomachinery, V02AT37A030, June 15–19, 2015

Paper No: GT2015-43016

DOI: https://doi.org/10.1115/GT2015-43016

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Topics: Compressors, Flow (Dynamics), Blades, Cantilevers, Clearances (Engineering), Errors, Separation (Technology)

Proceedings Papers

The Limitations of “R a ” to Describe Surface Roughness

Martin N. Goodhand, Karl Walton, Liam Blunt, Hang W. Lung, Robert J. Miller, Reg Marsden

Proc. ASME. GT2015, Volume 5C: Heat Transfer, V05CT16A003, June 15–19, 2015

Paper No: GT2015-43329

DOI: https://doi.org/10.1115/GT2015-43329

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Topics: Surface roughness, Airfoils, Drag (Fluid dynamics), Blades, Polishing, Reynolds number, Skin friction (Fluid dynamics), Wakes

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Journal citation

NARROW

The Effect of Reaction on Compressor Performance

Designing With High Temperature Composites

Transonic Relief in Fans and Compressors

Selecting a Compressor Meridional Topology: Axial, Mixed, Radial

Transonic Relief in Fans and Compressors

The Effect of Reaction on Compressor Performance

The Effect of Heat Transfer on Turbine Performance

The Impact of Combustor Turbulence on Turbine Loss Mechanisms

The Effect of Heat Transfer on Turbine Performance

The Impact of Combustor Turbulence on Turbine Loss Mechanisms

The Effect of Aspect Ratio on Compressor Performance

The Effect of Nonequilibrium Boundary Layers on Compressor Performance

The Effect of Non-Equilibrium Boundary Layers on Compressor Performance

Design of Compressor Endwall Velocity Triangles

Competing Three-Dimensional Mechanisms in Compressor Flows

Design of Compressor Endwall Velocity Triangles

The Limitations of Using “ R a ” to Describe Surface Roughness

Competing 3D Mechanisms in Compressor Flows

The Effect of Aspect Ratio on Compressor Performance

The Limitations of “R a ” to Describe Surface Roughness

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