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    Blockage Effects From Simulated Thermal Barrier Coatings for Cylindrical and Shaped Cooling Holes 

    Source: Journal of Turbomachinery:;2015:;volume( 137 ):;issue: 009:;page 91004
    Author(s): Whitfield, Christopher A.; Schroeder, Robert P.; Thole, Karen A.; Lewis, Scott D.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Film cooling and sprayed thermal barrier coatings (TBCs) protect gas turbine components from the hot combustion gas temperatures. As gas turbine designers pursue higher turbine inlet temperatures, film cooling and TBCs are ...
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