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Volume 126, Issue 3

July 2004

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ISSN 0889-504X

EISSN 1528-8900

In this Issue

Technical Papers

Technical Papers

Performance of Strongly Bowed Stators in a Four-Stage High-Speed Compressor

Axel Fischer, Walter Riess, Joerg R. Seume

J. Turbomach. July 2004, 126(3): 333–338. doi: https://doi.org/10.1115/1.1649743

Abstract

View articletitled, Performance of Strongly Bowed Stators in a Four-Stage High-Speed Compressor

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

A Numerical Investigation of the Flow Mechanisms in a High Pressure Compressor Front Stage With Axial Slots

Ingo Wilke, Hans-Peter Kau

J. Turbomach. July 2004, 126(3): 339–349. doi: https://doi.org/10.1115/1.1731465

Abstract

View articletitled, A Numerical Investigation of the Flow Mechanisms in a High Pressure Compressor Front Stage With Axial Slots

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Topics: Blades , Compressors , Flow (Dynamics) , Vortices , Rotors , Leakage , Simulation , Leakage flows , Pressure

Advanced High Turning Compressor Airfoils for Low Reynolds Number Condition—Part I: Design and Optimization

Toyotaka Sonoda, Yoshihiro Yamaguchi, Toshiyuki Arima, Markus Olhofer, Bernhard Sendhoff, Heinz-Adolf Schreiber

J. Turbomach. July 2004, 126(3): 350–359. doi: https://doi.org/10.1115/1.1737780

Abstract

View articletitled, Advanced High Turning Compressor Airfoils for Low Reynolds Number Condition—Part I: Design and Optimization

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Topics: Airfoils , Blades , Boundary layers , Design , Optimization , Reynolds number , Flow (Dynamics) , Turbulence , Compressors

Experimental Investigation of Unsteady Flow Field in the Tip Region of an Axial Compressor Rotor Passage at Near Stall Condition With Stereoscopic Particle Image Velocimetry

Baojie Liu, Hongwei Wang, Huoxing Liu, Hongjun Yu, Haokang Jiang, Maozhang Chen

J. Turbomach. July 2004, 126(3): 360–374. doi: https://doi.org/10.1115/1.1748367

Abstract

View articletitled, Experimental Investigation of Unsteady Flow Field in the Tip Region of an Axial Compressor Rotor Passage at Near Stall Condition With Stereoscopic Particle Image Velocimetry

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Topics: Compressors , Corners (Structural elements) , Flow (Dynamics) , Leakage , Rotors , Suction , Vortices , Vorticity , Blades , Particulate matter

Numerical Investigation of Three-Dimensional Clocking Effects in a Low Pressure Turbine

Andrea Arnone, Michele Marconcini, Alberto Scotti Del Greco, Ennio Spano

J. Turbomach. July 2004, 126(3): 375–384. doi: https://doi.org/10.1115/1.1740780

Abstract

View articletitled, Numerical Investigation of Three-Dimensional Clocking Effects in a Low Pressure Turbine

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Topics: Blades , Pressure , Stators , Turbines , Wakes , Rotors , Flow (Dynamics) , Computation

The Effect of Real Turbine Roughness With Pressure Gradient on Heat Transfer

Jeffrey P. Bons, Stephen T. McClain

J. Turbomach. July 2004, 126(3): 385–394. doi: https://doi.org/10.1115/1.1738120

Abstract

View articletitled, The Effect of Real Turbine Roughness With Pressure Gradient on Heat Transfer

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Topics: Heat transfer , Pressure gradient , Surface roughness , Turbines , Boundary layers , Turbulence

Vortex Transport and Blade Interactions in High Pressure Turbines

V. S. P. Chaluvadi, A. I. Kalfas, H. P. Hodson

J. Turbomach. July 2004, 126(3): 395–405. doi: https://doi.org/10.1115/1.1773849

Abstract

View articletitled, Vortex Transport and Blade Interactions in High Pressure Turbines

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Topics: Blades , Flow (Dynamics) , Rotors , Stators , Vortices , Wings , Pressure , Computer simulation , Turbines

Aerodynamic Performance of a Very High Lift Low Pressure Turbine Blade With Emphasis on Separation Prediction

Re´gis Houtermans, Thomas Coton, Tony Arts

J. Turbomach. July 2004, 126(3): 406–413. doi: https://doi.org/10.1115/1.1748416

Abstract

View articletitled, Aerodynamic Performance of a Very High Lift Low Pressure Turbine Blade With Emphasis on Separation Prediction

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Topics: Bubbles , Flow (Dynamics) , Pressure , Reynolds number , Separation (Technology) , Turbulence , Blades , Turbine blades

Experimental Surface Heat Transfer and Flow Structure in a Curved Channel With Laminar, Transitional, and Turbulent Flows

P. M. Ligrani, C. R. Hedlund

J. Turbomach. July 2004, 126(3): 414–423. doi: https://doi.org/10.1115/1.1738119

Abstract

View articletitled, Experimental Surface Heat Transfer and Flow Structure in a Curved Channel With Laminar, Transitional, and Turbulent Flows

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Topics: Flow (Dynamics) , Heat transfer , Turbulence , Vortices , Flow visualization

Intermittency Transport Modeling of Separated Flow Transition

J. Vicedo, S. Vilmin, W. N. Dawes, A. M. Savill

J. Turbomach. July 2004, 126(3): 424–431. doi: https://doi.org/10.1115/1.1748393

Abstract

View articletitled, Intermittency Transport Modeling of Separated Flow Transition

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Topics: Boundary layers , Bubbles , Flow (Dynamics) , Modeling , Separation (Technology) , Turbulence

Acoustic Resonance in Aeroengine Intake Ducts

A. J. Cooper, A. B. Parry, N. Peake

J. Turbomach. July 2004, 126(3): 432–441. doi: https://doi.org/10.1115/1.1776586

Abstract

View articletitled, Acoustic Resonance in Aeroengine Intake Ducts

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Topics: Acoustics , Ducts , Flow (Dynamics) , Resonance , Rotors , Stators

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Optimization of Low-Pressure Turbine Blade by Means of Fine Inspection of Loss Production Mechanisms

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Unsteady Flow Structure of Rotating Instability in a 1.5-Stage Axial Compressor

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Performance of Rough-Ribbed Low-Pressure Turbine Blades Under Varying Loading and Operating Conditions

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CONTROL OF SHROUD LEAKAGE LOSS AND WINDAGE TORQUE IN A LOW-PRESSURE TURBINE STAGE

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Numerical implementation of electrostatic solver within OpenFOAM for GT intake filtration

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Technical Papers

Performance of Strongly Bowed Stators in a Four-Stage High-Speed Compressor

A Numerical Investigation of the Flow Mechanisms in a High Pressure Compressor Front Stage With Axial Slots

Advanced High Turning Compressor Airfoils for Low Reynolds Number Condition—Part I: Design and Optimization

Experimental Investigation of Unsteady Flow Field in the Tip Region of an Axial Compressor Rotor Passage at Near Stall Condition With Stereoscopic Particle Image Velocimetry

Numerical Investigation of Three-Dimensional Clocking Effects in a Low Pressure Turbine

The Effect of Real Turbine Roughness With Pressure Gradient on Heat Transfer

Vortex Transport and Blade Interactions in High Pressure Turbines

Aerodynamic Performance of a Very High Lift Low Pressure Turbine Blade With Emphasis on Separation Prediction

Experimental Surface Heat Transfer and Flow Structure in a Curved Channel With Laminar, Transitional, and Turbulent Flows

Intermittency Transport Modeling of Separated Flow Transition

Acoustic Resonance in Aeroengine Intake Ducts

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