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    A Study of Mesh-Fed Slot Film Cooling 

    Source: Journal of Turbomachinery:;2011:;volume( 133 ):;issue: 001:;page 11022
    Author(s): R. S. Bunker
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This investigation demonstrates the potential improvement in adiabatic film effectiveness that can be achieved through the use of mesh-fed surface slot film cooling. Mesh, or in-wall network, ...
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    Electronics Packaging Cooling: Technologies From Gas Turbine Engine Cooling 

    Source: Journal of Electronic Packaging:;2006:;volume( 128 ):;issue: 003:;page 215
    Author(s): M. Arik; R. S. Bunker
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Heat transfer in turbomachinery has been well established due to the long history of research in the field. A vast amount of research has been devoted to obtain flow fields and regimes, heat ...
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    Local Heat Transfer in Internally Cooled Turbine Airfoil Leading Edge Regions: Part I—Impingement Cooling Without Film Coolant Extraction 

    Source: Journal of Turbomachinery:;1990:;volume( 112 ):;issue: 003:;page 451
    Author(s): R. S. Bunker; D. E. Metzger
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An experimental study has been designed and performed to measure very localized internal heat transfer characteristics in large-scale models of turbine blade impingement-cooled leading edge regions. ...
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    Local Heat Transfer in Internally Cooled Turbine Airfoil Leading Edge Regions: Part II—Impingement Cooling With Film Coolant Extraction 

    Source: Journal of Turbomachinery:;1990:;volume( 112 ):;issue: 003:;page 459
    Author(s): D. E. Metzger; R. S. Bunker
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An experimental study has been designed and performed to measure very localized internal heat transfer characteristics in large-scale models of turbine blade impingement-cooled leading edge regions ...
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    Heat Transfer and Flow on the First-Stage Blade Tip of a Power Generation Gas Turbine: Part 2—Simulation Results 

    Source: Journal of Turbomachinery:;2000:;volume( 122 ):;issue: 002:;page 272
    Author(s): A. A. Ameri; R. S. Bunker
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A combined experimental and computational study has been performed to investigate the detailed distribution of convective heat transfer coefficients on the first-stage blade tip surface for a ...
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    Local Heat Transfer in Turbine Disk Cavities: Part I—Rotor and Stator Cooling With Hub Injection of Coolant 

    Source: Journal of Turbomachinery:;1992:;volume( 114 ):;issue: 001:;page 211
    Author(s): R. S. Bunker; D. E. Metzger; S. Wittig
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Results are presented from an experimental study designed to obtain detailed radial heat transfer coefficient distributions applicable to the cooling of disk-cavity regions of gas turbines. An ...
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    Local Heat Transfer in Turbine Disk Cavities: Part II—Rotor Cooling With Radial Location Injection of Coolant 

    Source: Journal of Turbomachinery:;1992:;volume( 114 ):;issue: 001:;page 221
    Author(s): R. S. Bunker; D. E. Metzger; S. Wittig
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Detailed radial distributions of rotor heat transfer coefficients are presented for three basic disk-cavity geometries applicable to gas turbines. The experimental apparatus has been designed to ...
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    Effects of Surface Roughness on Heat Transfer and Aerodynamic Performance of Turbine Airfoils 

    Source: Journal of Turbomachinery:;1998:;volume( 120 ):;issue: 003:;page 522
    Author(s): N. Abuaf; C. P. Lee; R. S. Bunker
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Aerodynamic flow path losses and turbine airfoil gas side heat transfer are strongly affected by the gas side surface finish. For high aero efficiencies and reduced cooling requirements, airfoil ...
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    Transient Liquid Crystal Measurement of Local Heat Transfer on a Rotating Disk With Jet Impingement 

    Source: Journal of Turbomachinery:;1991:;volume( 113 ):;issue: 001:;page 52
    Author(s): D. E. Metzger; R. S. Bunker; G. Bosch
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An experimental technique has been developed for measurement of local convection heat transfer characteristics on rotating surfaces, utilizing thin liquid crystal surface coatings in a thermal ...
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    Latticework (Vortex) Cooling Effectiveness: Rotating Channel Experiments 

    Source: Journal of Turbomachinery:;2005:;volume( 127 ):;issue: 003:;page 471
    Author(s): S. Acharya; R. S. Bunker; F. Zhou; J. Lagrone; G. Mahmood
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The heat transfer and pressure drop characteristics of latticework coolant blade passages have been investigated experimentally under conditions of rotation. Stationary studies with the latticework ...
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