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    Overall Effectiveness for a Film Cooled Turbine Blade Leading Edge With Varying Hole Pitch 

    Source: Journal of Turbomachinery:;2013:;volume( 135 ):;issue: 003:;page 31011
    Author(s): Dyson, Thomas E.; Bogard, David G.; Piggush, Justin D.; Kohli, Atul
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Overall effectiveness, د†, for a simulated turbine blade leading edge was experimentally measured using a model constructed with a relatively high conductivity material selected so that the Biot number of the model matched ...
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