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Volume 127, Issue 4

October 2005

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ISSN 0889-504X

EISSN 1528-8900

In this Issue

Technical Papers
Erratum

Technical Papers

Interaction of Shroud Leakage Flow and Main Flow in a Three-Stage LP Turbine

Jochen Gier, Bertram Stubert, Bernard Brouillet, Laurent de Vito

J. Turbomach. October 2005, 127(4): 649–658. doi: https://doi.org/10.1115/1.2006667

Abstract

View articletitled, Interaction of Shroud Leakage Flow and Main Flow in a Three-Stage LP Turbine

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Topics: Cavities , Flow (Dynamics) , Leakage flows , Turbines

Fluid Flow and Heat Transfer in Rotating Curved Duct at High Rotation and Density Ratios

A. K. Sleiti, J. S. Kapat

J. Turbomach. October 2005, 127(4): 659–667. doi: https://doi.org/10.1115/1.2019276

Abstract

View articletitled, Fluid Flow and Heat Transfer in Rotating Curved Duct at High Rotation and Density Ratios

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Topics: Density , Ducts , Flow (Dynamics) , Heat transfer , Rotation , Stress , Turbulence , Cooling , Buoyancy , Coriolis force

Fluid Dynamics and Performance of Partially and Fully Shrouded Axial Turbines

L. Porreca, T. Behr, J. Schlienger, A. I. Kalfas, R. S. Abhari, J. Ehrhard, E. Janke

J. Turbomach. October 2005, 127(4): 668–678. doi: https://doi.org/10.1115/1.2008972

Abstract

View articletitled, Fluid Dynamics and Performance of Partially and Fully Shrouded Axial Turbines

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Topics: Blades , Flow (Dynamics) , Pressure , Rotors , Stators , Turbines , Vortices , Leakage , Yaw

Unsteady Flow Interactions Within the Inlet Cavity of a Turbine Rotor Tip Labyrinth Seal

A. Pfau, J. Schlienger, D. Rusch, A. I. Kalfas, R. S. Abhari

J. Turbomach. October 2005, 127(4): 679–688. doi: https://doi.org/10.1115/1.2008973

Abstract

View articletitled, Unsteady Flow Interactions Within the Inlet Cavity of a Turbine Rotor Tip Labyrinth Seal

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Topics: Cavities , Flow (Dynamics) , Pressure , Rotors , Turbines , Vortices , Blades , Stators , Vorticity , Fluids

Design and Test of an Ultralow Solidity Flow-Controlled Compressor Stator

K. R. Kirtley, P. Graziosi, P. Wood, B. Beacher, H.-W. Shin

J. Turbomach. October 2005, 127(4): 689–698. doi: https://doi.org/10.1115/1.1860374

Abstract

View articletitled, Design and Test of an Ultralow Solidity Flow-Controlled Compressor Stator

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Topics: Compressors , Design , Flow (Dynamics) , Flow control , Stators , Pressure , Computational fluid dynamics , Boundary layers

Vortex-Wake-Blade Interaction in a Shrouded Axial Turbine

J. Schlienger, A. I. Kalfas, R. S. Abhari

J. Turbomach. October 2005, 127(4): 699–707. doi: https://doi.org/10.1115/1.1934263

Abstract

View articletitled, Vortex-Wake-Blade Interaction in a Shrouded Axial Turbine

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Topics: Blades , Flow (Dynamics) , Pressure , Rotors , Stators , Vortices , Wakes , Turbines , Probes , Unsteady flow

Flow Mechanism for Stall Margin Improvement due to Circumferential Casing Grooves on Axial Compressors

Aamir Shabbir, John J. Adamczyk

J. Turbomach. October 2005, 127(4): 708–717. doi: https://doi.org/10.1115/1.2008970

Abstract

View articletitled, Flow Mechanism for Stall Margin Improvement due to Circumferential Casing Grooves on Axial Compressors

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Topics: Compressors , Flow (Dynamics) , Momentum , Pressure , Rotors , Shear (Mechanics) , Simulation , Computational fluid dynamics

Effect of Hole Geometry on the Thermal Performance of Fan-Shaped Film Cooling Holes

Michael Gritsch, Will Colban, Heinz Schär, Klaus Döbbeling

J. Turbomach. October 2005, 127(4): 718–725. doi: https://doi.org/10.1115/1.2019315

Abstract

View articletitled, Effect of Hole Geometry on the Thermal Performance of Fan-Shaped Film Cooling Holes

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Topics: Film cooling , Discharge coefficient , Flow (Dynamics)

Development of an Experimental Capability to Produce Controlled Blade Tip∕Shroud Rubs at Engine Speed

Corso Padova, Jeffrey Barton, Michael G. Dunn, Steve Manwaring, Gamaliel Young, Maurice Adams, Jr., Michael Adams

J. Turbomach. October 2005, 127(4): 726–735. doi: https://doi.org/10.1115/1.1934429

Abstract

View articletitled, Development of an Experimental Capability to Produce Controlled Blade Tip∕Shroud Rubs at Engine Speed

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Topics: Blades , Engines , Stress

Averaged and Time-Dependent Aerodynamics of a High Pressure Turbine Blade Tip Cavity and Stationary Shroud: Comparison of Computational and Experimental Results

Brian R. Green, John W. Barter, Charles W. Haldeman, Michael G. Dunn

J. Turbomach. October 2005, 127(4): 736–746. doi: https://doi.org/10.1115/1.1934410

Abstract

View articletitled, Averaged and Time-Dependent Aerodynamics of a High Pressure Turbine Blade Tip Cavity and Stationary Shroud: Comparison of Computational and Experimental Results

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Topics: Blades , Computational fluid dynamics , Pressure , Turbines , Rotors , High pressure (Physics) , Cavities , Turbine blades

The Effects of a Trip Wire and Unsteadiness on a High-Speed Highly Loaded Low-Pressure Turbine Blade

M. Vera, H. P. Hodson, R. Vazquez

J. Turbomach. October 2005, 127(4): 747–754. doi: https://doi.org/10.1115/1.1934446

Abstract

View articletitled, The Effects of a Trip Wire and Unsteadiness on a High-Speed Highly Loaded Low-Pressure Turbine Blade

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Topics: Inflow , Mach number , Pressure , Wire , Boundary layers , Surface roughness , Wakes , Flow (Dynamics) , Bubbles , Separation (Technology)

Pump Performance Improvement by Restraining Back Flow in Screw-Type Centrifugal Pump

Yasushi Tatebayashi, Kazuhiro Tanaka, Toshio Kobayashi

J. Turbomach. October 2005, 127(4): 755–762. doi: https://doi.org/10.1115/1.2019217

Abstract

View articletitled, Pump Performance Improvement by Restraining Back Flow in Screw-Type Centrifugal Pump

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Topics: Flow (Dynamics) , Impellers , Pressure , Pumps , Screws , Centrifugal pumps

The Impact of Blade-to-Blade Flow Variability on Turbine Blade Cooling Performance

Vince Sidwell, David Darmofal

J. Turbomach. October 2005, 127(4): 763–770. doi: https://doi.org/10.1115/1.2019247

Abstract

View articletitled, The Impact of Blade-to-Blade Flow Variability on Turbine Blade Cooling Performance

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Topics: Blades , Cooling , Flow (Dynamics) , Turbine blades , Manufacturing

Erratum

Erratum: “The Transient Liquid Crystal Technique: Influence of Surface Curvature and Finite Wall Thickness” [Journal of Turbomachinery, 2005, 127(1), pp. 175–182]

G. Wagner, M. Kottula, P. Ott, B. Weigand, J. von Wolfersdorf

J. Turbomach. October 2005, 127(4): 771–772. doi: https://doi.org/10.1115/1.2019348

Extract

View articletitled, Erratum: “The Transient Liquid Crystal Technique: Influence of Surface Curvature and Finite Wall Thickness” [<span class="related-article">Journal of Turbomachinery, 2005, 127(1), pp. 175–182</span>]

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Topics: Liquid crystals , Transients (Dynamics) , Turbomachinery , Wall thickness , Plates (structures)

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Analysis of High-order Source Terms in Throughflow Solutions

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Conjugate Heat Transfer Validation of an Optimized Film Cooling Configuration for a Turbine Vane Endwall

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CONCEPTUAL ANALYSIS ON THE IMPACT OF ACOUSTIC LINERS IN FAN FLUTTER

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Equation-Oriented Meanline Method for Axial Turbine Performance Prediction Under Choking Conditions

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Insights Into Turbocharger Centrifugal Compressor Stability Using High-Fidelity CFD and a Novel Impeller Diffusion Factor

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Technical Papers

Interaction of Shroud Leakage Flow and Main Flow in a Three-Stage LP Turbine

Fluid Flow and Heat Transfer in Rotating Curved Duct at High Rotation and Density Ratios

Fluid Dynamics and Performance of Partially and Fully Shrouded Axial Turbines

Unsteady Flow Interactions Within the Inlet Cavity of a Turbine Rotor Tip Labyrinth Seal

Design and Test of an Ultralow Solidity Flow-Controlled Compressor Stator

Vortex-Wake-Blade Interaction in a Shrouded Axial Turbine

Flow Mechanism for Stall Margin Improvement due to Circumferential Casing Grooves on Axial Compressors

Effect of Hole Geometry on the Thermal Performance of Fan-Shaped Film Cooling Holes

Development of an Experimental Capability to Produce Controlled Blade Tip∕Shroud Rubs at Engine Speed

Averaged and Time-Dependent Aerodynamics of a High Pressure Turbine Blade Tip Cavity and Stationary Shroud: Comparison of Computational and Experimental Results

The Effects of a Trip Wire and Unsteadiness on a High-Speed Highly Loaded Low-Pressure Turbine Blade

Pump Performance Improvement by Restraining Back Flow in Screw-Type Centrifugal Pump

The Impact of Blade-to-Blade Flow Variability on Turbine Blade Cooling Performance

Erratum

Erratum: “The Transient Liquid Crystal Technique: Influence of Surface Curvature and Finite Wall Thickness” [Journal of Turbomachinery, 2005, 127(1), pp. 175–182]

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