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    Unsteady Analysis of Blade and Tip Heat Transfer as Influenced by the Upstream Momentum and Thermal Wakes 

    Source: Journal of Turbomachinery:;2010:;volume( 132 ):;issue: 004:;page 41007
    Author(s): Ali A. Ameri; David L. Rigby; Erlendur Steinthorsson; James Heidmann; John C. Fabian
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The effect of the upstream wake on the time averaged rotor blade heat transfer was numerically investigated. The geometry and flow conditions of the first stage turbine blade of GE’s E3 engine ...
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    Film Cooling From a Row of Holes Supplemented With Antivortex Holes 

    Source: Journal of Turbomachinery:;2009:;volume( 131 ):;issue: 002:;page 21007
    Author(s): Alok Dhungel; Srinath V. Ekkad; James Heidmann; Yiping Lu; Wynn Phillips
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: design was originally developed at NASA-Glenn Research Center by James Heidmann, coauthor of this paper. This “antivortex” design is unique in that it requires only easily machinable round holes, unlike shaped film cooling...
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