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Volume 142, Issue 9

September 2020

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ISSN 0889-504X

EISSN 1528-8900

In this Issue

Research Papers

Research Papers

Comparison of Thin Film Heat Flux Gauge Technologies Emphasizing Continuous-Duration Operation

Shawn Siroka, Reid A. Berdanier, Karen A. Thole, Kam Chana, Charles W. Haldeman, Richard J. Anthony

J. Turbomach. September 2020, 142(9): 091001. doi: https://doi.org/10.1115/1.4045991

Abstract

View articletitled, Comparison of Thin Film Heat Flux Gauge Technologies Emphasizing Continuous-Duration Operation

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Topics: Calibration , Gages , Heat flux , Temperature , Thermal properties , Thin films , Sensors , Errors

Secondary Flows in the Return System of a Centrifugal Compressor Stage

T. Rossbach, J. Bisping, D. R. Grates, P. Jeschke, A. Hildebrandt, H. Franz

J. Turbomach. September 2020, 142(9): 091002. doi: https://doi.org/10.1115/1.4046686

Abstract

View articletitled, Secondary Flows in the Return System of a Centrifugal Compressor Stage

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Topics: Compressors , Flow (Dynamics) , Pressure

Challenges Associated With Replicating Rotor Blade Deposition in a Non-Rotating Annular Cascade

Christopher P. Bowen, Ali Ameri, Jeffrey P. Bons

J. Turbomach. September 2020, 142(9): 091003. doi: https://doi.org/10.1115/1.4047399

Abstract

View articletitled, Challenges Associated With Replicating Rotor Blade Deposition in a Non-Rotating Annular Cascade

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Topics: Blades , Cascades (Fluid dynamics) , Flow (Dynamics) , Particulate matter , Rotors , Pressure

A Deep Insight Into the Transonic Flow of an Advanced Centrifugal Compressor Design

David Wittrock, Martin Junker, Manfred Beversdorff, Andreas Peters, Eberhard Nicke

J. Turbomach. September 2020, 142(9): 091004. doi: https://doi.org/10.1115/1.4047609

Abstract

View articletitled, A Deep Insight Into the Transonic Flow of an Advanced Centrifugal Compressor Design

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Topics: Blades , Compressors , Design , Flow (Dynamics) , Impellers , Outflow , Inflow , Pressure

Improving Steady Computational Fluid Dynamics to Capture the Effects of Radial Mixing in Axial Compressors

Lorenzo Cozzi, Filippo Rubechini, Andrea Arnone, Andrea Schneider, Pio Astrua

J. Turbomach. September 2020, 142(9): 091005. doi: https://doi.org/10.1115/1.4047394

Abstract

View articletitled, Improving Steady Computational Fluid Dynamics to Capture the Effects of Radial Mixing in Axial Compressors

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Topics: Compressors , Flow (Dynamics) , Simulation , Calibration , Reynolds-averaged Navier–Stokes equations , Computational fluid dynamics , Steady state , Blades , Clearances (Engineering) , Design

Reducing Instrumentation Errors Caused by Circumferential Flow-Field Variations in Multistage Axial Compressors

M. Chilla, G. Pullan, S. Gallimore

J. Turbomach. September 2020, 142(9): 091006. doi: https://doi.org/10.1115/1.4047610

Abstract

View articletitled, Reducing Instrumentation Errors Caused by Circumferential Flow-Field Variations in Multistage Axial Compressors

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Topics: Compressors , Errors , Flow (Dynamics) , Pressure , Probes , Signals , Stators , Temperature , Wakes , Computational fluid dynamics

Coolant Jets Interaction in Effusion Cooling System: Experimental and Numerical Study

Y. Jiang, A. V. Murray, P.T. Ireland, L. di Mare

J. Turbomach. September 2020, 142(9): 091007. doi: https://doi.org/10.1115/1.4047612

Abstract

View articletitled, Coolant Jets Interaction in Effusion Cooling System: Experimental and Numerical Study

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Topics: Boundary layers , Computational fluid dynamics , Coolants , Cooling , Film cooling , Flow (Dynamics) , Jets , Temperature , Heat transfer , Cooling systems

Loss in Axial Compressor Bleed Systems

S. D. Grimshaw, J. Brind, G. Pullan, R. Seki

J. Turbomach. September 2020, 142(9): 091008. doi: https://doi.org/10.1115/1.4047614

Abstract

View articletitled, Loss in Axial Compressor Bleed Systems

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Topics: Compressors , Flow (Dynamics) , Turbines , Industrial gases , Pressure , Design , Ducts

The Impact of Combustor Turbulence on Turbine Loss Mechanisms

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

J. Turbomach. September 2020, 142(9): 091009. doi: https://doi.org/10.1115/1.4047615

Abstract

View articletitled, The Impact of Combustor Turbulence on Turbine Loss Mechanisms

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Topics: Boundary layers , Combustion chambers , Turbulence , Turbines

Modeling Axisymmetric Centrifugal Compressor Characteristics From First Principles

Katherine H. Powers, Chris J. Brace, Chris J. Budd, Colin D. Copeland, Paul A. Milewski

J. Turbomach. September 2020, 142(9): 091010. doi: https://doi.org/10.1115/1.4047616

Abstract

View articletitled, Modeling Axisymmetric Centrifugal Compressor Characteristics From First Principles

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Topics: Compressors , Flow (Dynamics) , Impellers , Surges , Diffusers

Effect of Blade Row Interaction on Rotor Film Cooling

J. Brind, G. Pullan

J. Turbomach. September 2020, 142(9): 091011. doi: https://doi.org/10.1115/1.4047617

Abstract

View articletitled, Effect of Blade Row Interaction on Rotor Film Cooling

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Topics: Blades , Boundary-value problems , Coolants , Cooling , Film cooling , Momentum , Pressure , Rotors , Turbines , Wakes

Investigations Into Heat Transfer and Aerodynamic Performance of a Worn Squealer Tipped Turbine Stage

Xin Yan, Mingliang Ye, Kun He

J. Turbomach. September 2020, 142(9): 091012. doi: https://doi.org/10.1115/1.4047632

Abstract

View articletitled, Investigations Into Heat Transfer and Aerodynamic Performance of a Worn Squealer Tipped Turbine Stage

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Topics: Blades , Cavities , Design , Flow (Dynamics) , Heat transfer , Heat transfer coefficients , Turbines , Wear , Damage , Vortices

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Research Papers

Comparison of Thin Film Heat Flux Gauge Technologies Emphasizing Continuous-Duration Operation

Secondary Flows in the Return System of a Centrifugal Compressor Stage

Challenges Associated With Replicating Rotor Blade Deposition in a Non-Rotating Annular Cascade

A Deep Insight Into the Transonic Flow of an Advanced Centrifugal Compressor Design

Improving Steady Computational Fluid Dynamics to Capture the Effects of Radial Mixing in Axial Compressors

Reducing Instrumentation Errors Caused by Circumferential Flow-Field Variations in Multistage Axial Compressors

Coolant Jets Interaction in Effusion Cooling System: Experimental and Numerical Study

Loss in Axial Compressor Bleed Systems

The Impact of Combustor Turbulence on Turbine Loss Mechanisms

Modeling Axisymmetric Centrifugal Compressor Characteristics From First Principles

Effect of Blade Row Interaction on Rotor Film Cooling

Investigations Into Heat Transfer and Aerodynamic Performance of a Worn Squealer Tipped Turbine Stage

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