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    Heat Transfer Measurements to a Gas Turbine Cooling Passage With Inclined Ribs 

    Source: Journal of Turbomachinery:;1998:;volume( 120 ):;issue: 001:;page 63
    Author(s): Z. Wang; P. T. Ireland; S. T. Kohler; J. W. Chew
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The local heat transfer coefficient distribution over all four walls of a large-scale model of a gas turbine cooling passage have been measured in great detail. A new method of determine the ...
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    Full Surface Local Heat Transfer Coefficient Measurements in a Model of an Integrally Cast Impingement Cooling Geometry 

    Source: Journal of Turbomachinery:;1998:;volume( 120 ):;issue: 001:;page 92
    Author(s): D. R. H. Gillespie; S. T. Kohler; Z. Wang; P. T. Ireland
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Cast impingement cooling geometries offer the gas turbine designer higher structural integrity and improved convective cooling when compared to traditional impingement cooling systems, which rely ...
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    Erratum: “Heat Transfer Measurements to a Gas Turbine Cooling Passage With Inclined Ribs” (1998, ASME Journal of Turbomachinery, 120, pp. 63–69) 

    Source: Journal of Turbomachinery:;1998:;volume( 120 ):;issue: 003:;page 445
    Author(s): Z. Wang; P. T. Ireland; S. T. Kohler; J. W. Chew
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Detailed Measurements of Local Heat Transfer Coefficient in the Entrance to Normal and Inclined Film Cooling Holes 

    Source: Journal of Turbomachinery:;1996:;volume( 118 ):;issue: 002:;page 285
    Author(s): D. R. H. Gillespie; S. T. Kohler; A. R. Byerley; P. T. Ireland; Z. Wang; T. V. Jones
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The local heat transfer inside the entrance to large-scale models of film cooling holes has been measured using the transient heat transfer technique. The method employs temperature-sensitive ...
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