Volume 128 Issue 1 | J. Turbomach. | ASME Digital Collection

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Volume 128, Issue 1

January 2006

ISSN 0889-504X

EISSN 1528-8900

Technical Papers

A Unified Correlation for Slip Factor in Centrifugal Impellers

Theodor W. von Backström

J. Turbomach. January 2006, 128(1): 1–10. doi: https://doi.org/10.1115/1.2101853

Abstract

View articletitled, A Unified Correlation for Slip Factor in Centrifugal Impellers

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Topics: Blades , Eddies (Fluid dynamics) , Impellers , Rotors

Multistage Aspects and Unsteady Effects of Stator and Rotor Clocking in an Axial Turbine With Low Aspect Ratio Blading

T. Behr, L. Porreca, T. Mokulys, A. I. Kalfas, R. S. Abhari

J. Turbomach. January 2006, 128(1): 11–22. doi: https://doi.org/10.1115/1.2101855

Abstract

View articletitled, Multistage Aspects and Unsteady Effects of Stator and Rotor Clocking in an Axial Turbine With Low Aspect Ratio Blading

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Topics: Blades , Flow (Dynamics) , Rotors , Stators , Turbines

Design and Testing of a Transonic Linear Cascade Tunnel With Optimized Slotted Walls

Aldo Rona, Renato Paciorri, Marco Geron

J. Turbomach. January 2006, 128(1): 23–34. doi: https://doi.org/10.1115/1.2101856

Abstract

View articletitled, Design and Testing of a Transonic Linear Cascade Tunnel With Optimized Slotted Walls

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Topics: Blades , Cascades (Fluid dynamics) , Flow (Dynamics) , Pressure , Wind tunnels , Tunnels , Design , Waves

Unsteady Aerodynamics and Interactions Between a High-Pressure Turbine Vane and Rotor

Ryan M. Urbassik, J. Mitch Wolff, Marc D. Polanka

J. Turbomach. January 2006, 128(1): 35–42. doi: https://doi.org/10.1115/1.2098752

Abstract

View articletitled, Unsteady Aerodynamics and Interactions Between a High-Pressure Turbine Vane and Rotor

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Topics: Blades , Pressure , Rotors , Turbines , Aerodynamics , High pressure (Physics) , Reynolds number

Fan-Shaped Hole Effects on the Aero-Thermal Performance of a Film-Cooled Endwall

Giovanna Barigozzi, Giuseppe Benzoni, Giuseppe Franchini, Antonio Perdichizzi

J. Turbomach. January 2006, 128(1): 43–52. doi: https://doi.org/10.1115/1.2098788

Abstract

View articletitled, Fan-Shaped Hole Effects on the Aero-Thermal Performance of a Film-Cooled Endwall

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Topics: Cooling , Flow (Dynamics) , Geometry , Jets , Vortices , Cross-flow , Coolants , Pressure , Cascades (Fluid dynamics) , Film cooling

Heat Transfer and Film-Cooling Measurements on a Stator Vane With Fan-Shaped Cooling Holes

W. Colban, A. Gratton, K. A. Thole, M. Haendler

J. Turbomach. January 2006, 128(1): 53–61. doi: https://doi.org/10.1115/1.2098789

Abstract

View articletitled, Heat Transfer and Film-Cooling Measurements on a Stator Vane With Fan-Shaped Cooling Holes

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Topics: Cooling , Film cooling , Heat transfer , Pressure , Suction , Engines , Boundary layers

Effect of Midpassage Gap, Endwall Misalignment, and Roughness on Endwall Film-Cooling

N. D. Cardwell, N. Sundaram, K. A. Thole

J. Turbomach. January 2006, 128(1): 62–70. doi: https://doi.org/10.1115/1.2098791

Abstract

View articletitled, Effect of Midpassage Gap, Endwall Misalignment, and Roughness on Endwall Film-Cooling

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Topics: Coolants , Film cooling , Flow (Dynamics) , Pressure , Surface roughness , Cooling , Turbines , Cascades (Fluid dynamics) , Suction

Turbulent Transport in Pin Fin Arrays: Experimental Data and Predictions

F. E. Ames, L. A. Dvorak

J. Turbomach. January 2006, 128(1): 71–81. doi: https://doi.org/10.1115/1.2098792

Abstract

View articletitled, Turbulent Transport in Pin Fin Arrays: Experimental Data and Predictions

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Topics: Flow (Dynamics) , Heat transfer , Pressure , Reynolds number , Turbulence , Wire , Spectra (Spectroscopy)

The Effect of Inlet Guide Vanes Wake Impingement on the Flow Structure and Turbulence Around a Rotor Blade

Francesco Soranna, Yi-Chih Chow, Oguz Uzol, Joseph Katz

J. Turbomach. January 2006, 128(1): 82–95. doi: https://doi.org/10.1115/1.2098755

Abstract

View articletitled, The Effect of Inlet Guide Vanes Wake Impingement on the Flow Structure and Turbulence Around a Rotor Blade

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Topics: Blades , Flow (Dynamics) , Inlet guide vanes , Rotors , Turbulence , Wakes , Suction

Local Heat/Mass Transfer Characteristics on a Rotating Blade With Flat Tip in Low-Speed Annular Cascade—Part I: Near-Tip Surface

Dong-Ho Rhee, Hyung Hee Cho

J. Turbomach. January 2006, 128(1): 96–109. doi: https://doi.org/10.1115/1.2098756

Abstract

View articletitled, Local Heat/Mass Transfer Characteristics on a Rotating Blade With Flat Tip in Low-Speed Annular Cascade—Part I: Near-Tip Surface

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Topics: Blades , Flow (Dynamics) , Heat , Mass transfer , Heat transfer , Rotating blades , Pressure , Design

Local Heat/Mass Transfer Characteristics on a Rotating Blade With Flat Tip in a Low-Speed Annular Cascade—Part II: Tip and Shroud

Dong-Ho Rhee, Hyung Hee Cho

J. Turbomach. January 2006, 128(1): 110–119. doi: https://doi.org/10.1115/1.2098767

Abstract

View articletitled, Local Heat/Mass Transfer Characteristics on a Rotating Blade With Flat Tip in a Low-Speed Annular Cascade—Part II: Tip and Shroud

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Topics: Blades , Flow (Dynamics) , Heat , Heat transfer , Mass transfer , Rotating blades , Design

Averaging Nonuniform Flow for a Purpose

N. A. Cumpsty, J. H. Horlock

J. Turbomach. January 2006, 128(1): 120–129. doi: https://doi.org/10.1115/1.2098807

Abstract

View articletitled, Averaging Nonuniform Flow for a Purpose

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Topics: Flow (Dynamics) , Nozzles , Pressure , Temperature , Turbines , Enthalpy

Long-to-Short Length-Scale Transition: A Stall Inception Phenomenon in an Axial Compressor With Inlet Distortion

Feng Lin, Meilin Li, Jingyi Chen

J. Turbomach. January 2006, 128(1): 130–140. doi: https://doi.org/10.1115/1.2098808

Abstract

View articletitled, Long-to-Short Length-Scale Transition: A Stall Inception Phenomenon in an Axial Compressor With Inlet Distortion

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Topics: Compressors , Flow (Dynamics) , Stall inception , Blades , Rotors , Probes

Modeling of Film Cooling—Part I: Experimental Study of Flow Structure

Stefan Bernsdorf, Martin G. Rose, Reza S. Abhari

J. Turbomach. January 2006, 128(1): 141–149. doi: https://doi.org/10.1115/1.2098768

Abstract

View articletitled, Modeling of Film Cooling—Part I: Experimental Study of Flow Structure

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Topics: Film cooling , Flow (Dynamics) , Cooling , Density

The Influence of Turbulence on Wake Dispersion and Blade Row Interaction in an Axial Compressor

Alan D. Henderson, Gregory J. Walker, Jeremy D. Hughes

J. Turbomach. January 2006, 128(1): 150–157. doi: https://doi.org/10.1115/1.2098809

Abstract

View articletitled, The Influence of Turbulence on Wake Dispersion and Blade Row Interaction in an Axial Compressor

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Topics: Blades , Compressors , Rotors , Stators , Turbulence , Wakes , Flow (Dynamics) , Inlet guide vanes

Heat Transfer on Internal Surfaces of a Duct Subjected to Impingement of a Jet Array with Varying Jet Hole-Size and Spacing

U. Uysal, P.-W. Li, M. K. Chyu, F. J. Cunha

J. Turbomach. January 2006, 128(1): 158–165. doi: https://doi.org/10.1115/1.2101859

Abstract

View articletitled, Heat Transfer on Internal Surfaces of a Duct Subjected to Impingement of a Jet Array with Varying Jet Hole-Size and Spacing

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Topics: Cooling , Heat transfer , Heat transfer coefficients , Jets , Ducts , Flow (Dynamics) , Convection

Effects of Reynolds Number and Freestream Turbulence on Turbine Tip Clearance Flow

Takayuki Matsunuma

J. Turbomach. January 2006, 128(1): 166–177. doi: https://doi.org/10.1115/1.2103091

Abstract

View articletitled, Effects of Reynolds Number and Freestream Turbulence on Turbine Tip Clearance Flow

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Topics: Clearances (Engineering) , Flow (Dynamics) , Pressure , Reynolds number , Turbines , Turbulence , Cascades (Fluid dynamics)

Investigation of Vortex Shedding and Wake-Wake Interaction in a Transonic Turbine Stage Using Laser-Doppler-Velocimetry and Particle-Image-Velocimetry

E. Göttlich, J. Woisetschläger, P. Pieringer, B. Hampel, F. Heitmeir

J. Turbomach. January 2006, 128(1): 178–187. doi: https://doi.org/10.1115/1.2103092

Abstract

View articletitled, Investigation of Vortex Shedding and Wake-Wake Interaction in a Transonic Turbine Stage Using Laser-Doppler-Velocimetry and Particle-Image-Velocimetry

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Topics: Blades , Flow (Dynamics) , Particulate matter , Rotors , Stators , Turbines , Vortex shedding , Vortices , Wakes , Nozzles

Combined Three-Dimensional Fluid Dynamics and Mechanical Modeling of Brush Seals

Diego Lelli, John W. Chew, Paul Cooper

J. Turbomach. January 2006, 128(1): 188–195. doi: https://doi.org/10.1115/1.2103093

Abstract

View articletitled, Combined Three-Dimensional Fluid Dynamics and Mechanical Modeling of Brush Seals

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Topics: Aerodynamics , Computational fluid dynamics , Flow (Dynamics) , Geometry , Modeling , Pressure , Fluid-dynamic forces , Fluid dynamics , Rotors , Deflection

Film Cooling Effectiveness and Heat Transfer on the Trailing Edge Cutback of Gas Turbine Airfoils With Various Internal Cooling Designs

P. Martini, A. Schulz, H.-J. Bauer

J. Turbomach. January 2006, 128(1): 196–205. doi: https://doi.org/10.1115/1.2103094

Abstract

View articletitled, Film Cooling Effectiveness and Heat Transfer on the Trailing Edge Cutback of Gas Turbine Airfoils With Various Internal Cooling Designs

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Topics: Coolants , Cooling , Film cooling , Flow (Dynamics) , Heat transfer , Heat transfer coefficients , Turbulence , Gas turbines , Pressure , Discharge coefficient

Technical Brief

Predicting Blade Stress Levels Directly From Reduced-Order Vibration Models of Mistuned Bladed Disks

Sang-Ho Lim, Christophe Pierre, Matthew P. Castanier

J. Turbomach. January 2006, 128(1): 206–210. doi: https://doi.org/10.1115/1.2098754

Abstract

View articletitled, Predicting Blade Stress Levels Directly From Reduced-Order Vibration Models of Mistuned Bladed Disks

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Topics: Blades , Disks , Stress , Vibration , Finite element analysis , Displacement

Errata

Erratum: “Development and Experimental Validation of a Compressor Dynamic Model” [Journal of Turbomachinery, 2005, 127(3), pp. 599–608]

M. Venturini

J. Turbomach. January 2006, 128(1): 211. doi: https://doi.org/10.1115/1.2098706

Extract

View articletitled, Erratum: “Development and Experimental Validation of a Compressor Dynamic Model” [<span class="related-article">Journal of Turbomachinery, 2005, 127(3), pp. 599–608</span>]

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Topics: Compressors , Dynamic models , Turbomachinery

Technical Papers

A Unified Correlation for Slip Factor in Centrifugal Impellers

Multistage Aspects and Unsteady Effects of Stator and Rotor Clocking in an Axial Turbine With Low Aspect Ratio Blading

Design and Testing of a Transonic Linear Cascade Tunnel With Optimized Slotted Walls

Unsteady Aerodynamics and Interactions Between a High-Pressure Turbine Vane and Rotor

Fan-Shaped Hole Effects on the Aero-Thermal Performance of a Film-Cooled Endwall

Heat Transfer and Film-Cooling Measurements on a Stator Vane With Fan-Shaped Cooling Holes

Effect of Midpassage Gap, Endwall Misalignment, and Roughness on Endwall Film-Cooling

Turbulent Transport in Pin Fin Arrays: Experimental Data and Predictions

The Effect of Inlet Guide Vanes Wake Impingement on the Flow Structure and Turbulence Around a Rotor Blade

Local Heat/Mass Transfer Characteristics on a Rotating Blade With Flat Tip in Low-Speed Annular Cascade—Part I: Near-Tip Surface

Local Heat/Mass Transfer Characteristics on a Rotating Blade With Flat Tip in a Low-Speed Annular Cascade—Part II: Tip and Shroud

Averaging Nonuniform Flow for a Purpose

Long-to-Short Length-Scale Transition: A Stall Inception Phenomenon in an Axial Compressor With Inlet Distortion

Modeling of Film Cooling—Part I: Experimental Study of Flow Structure

The Influence of Turbulence on Wake Dispersion and Blade Row Interaction in an Axial Compressor

Heat Transfer on Internal Surfaces of a Duct Subjected to Impingement of a Jet Array with Varying Jet Hole-Size and Spacing

Effects of Reynolds Number and Freestream Turbulence on Turbine Tip Clearance Flow

Investigation of Vortex Shedding and Wake-Wake Interaction in a Transonic Turbine Stage Using Laser-Doppler-Velocimetry and Particle-Image-Velocimetry

Combined Three-Dimensional Fluid Dynamics and Mechanical Modeling of Brush Seals

Film Cooling Effectiveness and Heat Transfer on the Trailing Edge Cutback of Gas Turbine Airfoils With Various Internal Cooling Designs

Technical Brief

Predicting Blade Stress Levels Directly From Reduced-Order Vibration Models of Mistuned Bladed Disks

Errata

Erratum: “Development and Experimental Validation of a Compressor Dynamic Model” [Journal of Turbomachinery, 2005, 127(3), pp. 599–608]

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