Volume 123 Issue 4 | J. Turbomach. | ASME Digital Collection

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Technical Papers

Convective Heat Transfer and Aerodynamics in Axial Flow Turbines

Michael G. Dunn

J. Turbomach. October 2001, 123(4): 637–686. doi: https://doi.org/10.1115/1.1397776

Abstract

View articletitled, Convective Heat Transfer and Aerodynamics in Axial Flow Turbines

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Topics: Blades , Heat transfer , Pressure , Turbines , Turbulence , Flow (Dynamics) , Film cooling

Mainstream Aerodynamic Effects Due to Wheelspace Coolant Injection in a High-Pressure Turbine Stage: Part I—Aerodynamic Measurements in the Stationary Frame

Christopher McLean, Cengiz Camci, Professor of Aerospace Engineering, Boris Glezer

J. Turbomach. October 2001, 123(4): 687–696. doi: https://doi.org/10.1115/1.1401026

Abstract

View articletitled, Mainstream Aerodynamic Effects Due to Wheelspace Coolant Injection in a High-Pressure Turbine Stage: Part I—Aerodynamic Measurements in the Stationary Frame

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Topics: Coolants , Cooling , Flow (Dynamics) , Pressure , Rotors , Turbines , Uncertainty , Impingement cooling , High pressure (Physics)

Mainstream Aerodynamic Effects Due to Wheelspace Coolant Injection in a High-Pressure Turbine Stage: Part II—Aerodynamic Measurements in the Rotational Frame

Christopher McLean, Cengiz Camci, Professor of Aerospace Engineering, Boris Glezer

J. Turbomach. October 2001, 123(4): 697–703. doi: https://doi.org/10.1115/1.1397303

Abstract

View articletitled, Mainstream Aerodynamic Effects Due to Wheelspace Coolant Injection in a High-Pressure Turbine Stage: Part II—Aerodynamic Measurements in the Rotational Frame

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Topics: Coolants , Cooling , Flow (Dynamics) , High pressure (Physics) , Pressure , Rotors , Turbines , Wakes , Impingement cooling , Probes

Heat Transfer and Flow on the Blade Tip of a Gas Turbine Equipped With a Mean-Camberline Strip

A. A. Ameri

J. Turbomach. October 2001, 123(4): 704–708. doi: https://doi.org/10.1115/1.1400114

Abstract

View articletitled, Heat Transfer and Flow on the Blade Tip of a Gas Turbine Equipped With a Mean-Camberline Strip

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Topics: Blades , Flow (Dynamics) , Heat transfer , Strips , Leakage , Gas turbines , Geometry

Film-Cooled Turbine Endwall in a Transonic Flow Field: Part I—Aerodynamic Measurements

Friedrich Kost, Martin Nicklas

J. Turbomach. October 2001, 123(4): 709–719. doi: https://doi.org/10.1115/1.1400112

Abstract

View articletitled, Film-Cooled Turbine Endwall in a Transonic Flow Field: Part I—Aerodynamic Measurements

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Topics: Coolants , Flow (Dynamics) , Pressure

Film-Cooled Turbine Endwall in a Transonic Flow Field: Part II—Heat Transfer and Film-Cooling Effectiveness

Martin Nicklas

J. Turbomach. October 2001, 123(4): 720–729. doi: https://doi.org/10.1115/1.1397308

Abstract

View articletitled, Film-Cooled Turbine Endwall in a Transonic Flow Field: Part II—Heat Transfer and Film-Cooling Effectiveness

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Topics: Coolants , Film cooling , Flow (Dynamics) , Heat transfer , Cooling , Turbines , Heat transfer coefficients , Temperature

Turbine Nozzle Endwall Film Cooling Study Using Pressure-Sensitive Paint

Luzeng J. Zhang, Ruchira Sharma Jaiswal

J. Turbomach. October 2001, 123(4): 730–738. doi: https://doi.org/10.1115/1.1400113

Abstract

View articletitled, Turbine Nozzle Endwall Film Cooling Study Using Pressure-Sensitive Paint

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Topics: Cooling , Film cooling , Flow (Dynamics) , Nozzles , Pressure , Turbines , Nitrogen , Paints , Oxygen , Turbulence

The Many Faces of Turbine Surface Roughness

Jeffrey P. Bons, Robert P. Taylor, Stephen T. McClain, Richard B. Rivir

J. Turbomach. October 2001, 123(4): 739–748. doi: https://doi.org/10.1115/1.1400115

Abstract

View articletitled, The Many Faces of Turbine Surface Roughness

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Topics: Surface roughness , Turbines , Spallation (Nuclear physics)

High-Resolution Measurements of Local Heat Transfer Coefficients From Discrete Hole Film Cooling

S. Baldauf, A. Schulz, S. Wittig

J. Turbomach. October 2001, 123(4): 749–757. doi: https://doi.org/10.1115/1.1387245

Abstract

View articletitled, High-Resolution Measurements of Local Heat Transfer Coefficients From Discrete Hole Film Cooling

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Topics: Coolants , Density , Film cooling , Flow (Dynamics) , Heat flux , Heat transfer , Heat transfer coefficients , Resolution (Optics) , Temperature , Vortices

High-Resolution Measurements of Local Effectiveness From Discrete Hole Film Cooling

S. Baldauf, A. Schulz, S. Wittig

J. Turbomach. October 2001, 123(4): 758–765. doi: https://doi.org/10.1115/1.1371778

Abstract

View articletitled, High-Resolution Measurements of Local Effectiveness From Discrete Hole Film Cooling

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Topics: Coolants , Cooling , Density , Film cooling , Finite element analysis , Flow (Dynamics) , Heat flux , Jets , Momentum , Resolution (Optics)

An Experimental Study of Impingement on Roughened Airfoil Leading-Edge Walls With Film Holes

M. E. Taslim, Y. Pan, S. D. Spring

J. Turbomach. October 2001, 123(4): 766–773. doi: https://doi.org/10.1115/1.1401035

Abstract

View articletitled, An Experimental Study of Impingement on Roughened Airfoil Leading-Edge Walls With Film Holes

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Topics: Airfoils , Flow (Dynamics) , Geometry , Heat transfer , Heat transfer coefficients , Reynolds number , Cooling , Pressure , Jets

Film Cooling Discharge Coefficient Measurements in a Turbulated Passage With Internal Crossflow

Ronald S. Bunker, Jeremy C. Bailey

J. Turbomach. October 2001, 123(4): 774–780. doi: https://doi.org/10.1115/1.1397307

Abstract

View articletitled, Film Cooling Discharge Coefficient Measurements in a Turbulated Passage With Internal Crossflow

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

Effect of Crossflows on the Discharge Coefficient of Film Cooling Holes With Varying Angles of Inclination and Orientation

Michael Gritsch, Achmed Schulz, Sigmar Wittig

J. Turbomach. October 2001, 123(4): 781–787. doi: https://doi.org/10.1115/1.1397306

Abstract

View articletitled, Effect of Crossflows on the Discharge Coefficient of Film Cooling Holes With Varying Angles of Inclination and Orientation

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Topics: Discharge coefficient , Film cooling , Mach number , Pressure , Flow (Dynamics)

Shock Wave–Film Cooling Interactions in Transonic Flows

P. M. Ligrani, Fellow ASME, Professor, C. Saumweber, A. Schulz, S. Wittig

J. Turbomach. October 2001, 123(4): 788–797. doi: https://doi.org/10.1115/1.1397305

Abstract

View articletitled, Shock Wave–Film Cooling Interactions in Transonic Flows

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Topics: Film cooling , Mach number , Shock waves , Flow (Dynamics)

Full-Coverage Film Cooling With Short Normal Injection Holes

Mark K. Harrington, Marcus A. McWaters, David G. Bogard, Christopher A. Lemmon, Karen A. Thole

J. Turbomach. October 2001, 123(4): 798–805. doi: https://doi.org/10.1115/1.1400111

Abstract

View articletitled, Full-Coverage Film Cooling With Short Normal Injection Holes

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Topics: Coolants , Film cooling , Turbulence , Jets

Heat/Mass Transfer Measurement Within a Film Cooling Hole of Square and Rectangular Cross Section

Hyung Hee Cho, Seung Goo Kang, Dong Ho Rhee

J. Turbomach. October 2001, 123(4): 806–814. doi: https://doi.org/10.1115/1.1400109

Abstract

View articletitled, Heat/Mass Transfer Measurement Within a Film Cooling Hole of Square and Rectangular Cross Section

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Topics: Film cooling , Flow (Dynamics) , Heat , Mass transfer , Reynolds number , Vortices

Effects of Reynolds Number and Pressure Ratio on Leakage Loss and Heat Transfer in a Stepped Labyrinth Seal

K. Willenborg, S. Kim, S. Wittig

J. Turbomach. October 2001, 123(4): 815–822. doi: https://doi.org/10.1115/1.1397304

Abstract

View articletitled, Effects of Reynolds Number and Pressure Ratio on Leakage Loss and Heat Transfer in a Stepped Labyrinth Seal

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Topics: Discharge coefficient , Heat transfer , Leakage , Pressure , Reynolds number , Flow (Dynamics) , Geometry , Stators

The Application of Pressure- and Temperature-Sensitive Paints to an Advanced Compressor

Kelly R. Navarra, Douglas C. Rabe, Sergey D. Fonov, Larry P. Goss, Chunill Hah

J. Turbomach. October 2001, 123(4): 823–829. doi: https://doi.org/10.1115/1.1400116

Abstract

View articletitled, The Application of Pressure- and Temperature-Sensitive Paints to an Advanced Compressor

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Topics: Compressors , Paints , Pressure , Temperature , Computational fluid dynamics , Pressure measurement , Blades

Technical Papers

Convective Heat Transfer and Aerodynamics in Axial Flow Turbines

Mainstream Aerodynamic Effects Due to Wheelspace Coolant Injection in a High-Pressure Turbine Stage: Part I—Aerodynamic Measurements in the Stationary Frame

Mainstream Aerodynamic Effects Due to Wheelspace Coolant Injection in a High-Pressure Turbine Stage: Part II—Aerodynamic Measurements in the Rotational Frame

Heat Transfer and Flow on the Blade Tip of a Gas Turbine Equipped With a Mean-Camberline Strip

Film-Cooled Turbine Endwall in a Transonic Flow Field: Part I—Aerodynamic Measurements

Film-Cooled Turbine Endwall in a Transonic Flow Field: Part II—Heat Transfer and Film-Cooling Effectiveness

Turbine Nozzle Endwall Film Cooling Study Using Pressure-Sensitive Paint

The Many Faces of Turbine Surface Roughness

High-Resolution Measurements of Local Heat Transfer Coefficients From Discrete Hole Film Cooling

High-Resolution Measurements of Local Effectiveness From Discrete Hole Film Cooling

An Experimental Study of Impingement on Roughened Airfoil Leading-Edge Walls With Film Holes

Film Cooling Discharge Coefficient Measurements in a Turbulated Passage With Internal Crossflow

Effect of Crossflows on the Discharge Coefficient of Film Cooling Holes With Varying Angles of Inclination and Orientation

Shock Wave–Film Cooling Interactions in Transonic Flows

Full-Coverage Film Cooling With Short Normal Injection Holes

Heat/Mass Transfer Measurement Within a Film Cooling Hole of Square and Rectangular Cross Section

Effects of Reynolds Number and Pressure Ratio on Leakage Loss and Heat Transfer in a Stepped Labyrinth Seal

The Application of Pressure- and Temperature-Sensitive Paints to an Advanced Compressor

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