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    Film Cooling of the Gas Turbine Endwall by Discrete-Hole Injection 

    Source: Journal of Turbomachinery:;1996:;volume( 118 ):;issue: 002:;page 278
    Author(s): M. Y. Jabbari; K. C. Marston; E. R. G. Eckert; R. J. Goldstein
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Film cooling performance for injection through discrete holes in the endwall of a turbine blade is investigated. The effectiveness is measured at 60 locations in the region covered by injection. ...
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