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    Effect of Film Cooling on Turbine Capacity 

    Source: Journal of Engineering for Gas Turbines and Power:;2010:;volume( 132 ):;issue: 001:;page 11901
    Author(s): T. Povey
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes a method that allows the effect of film cooling on the capacity of a turbine to be computed. The model is based on fundamental cooling performance parameters and is ...
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    A Novel Technique for Assessing Turbine Cooling System Performance 

    Source: Journal of Turbomachinery:;2011:;volume( 133 ):;issue: 003:;page 31013
    Author(s): S. Luque; T. Povey
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A new experimental technique for the accurate measurement of steady-state metal temperature surface distributions of modern heavily film-cooled turbine vanes has been developed and is described ...
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    Experimental Measurements of Gas Turbine Flow Capacity Using a Novel Transient Technique 

    Source: Journal of Turbomachinery:;2011:;volume( 133 ):;issue: 001:;page 11005
    Author(s): T. Povey; M. Sharpe; A. Rawlinson
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Nozzle guide vane (NGV) flow capacity is perhaps the most important parameter for engine optimization. Inaccurate evaluation of capacity would lead to incorrect performance evaluation, and unmatched ...
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    On a Novel Annular Sector Cascade Technique 

    Source: Journal of Turbomachinery:;2007:;volume( 129 ):;issue: 001:;page 175
    Author(s): T. Povey; T. V. Jones; M. L. Oldfield
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An advanced technique for establishing pressure boundary conditions in annular sector cascade experiments has been developed. This novel technique represents an improvement over previous methods ...
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    The Effect of Hot-Streaks on HP Vane Surface and Endwall Heat Transfer: An Experimental and Numerical Study 

    Source: Journal of Turbomachinery:;2007:;volume( 129 ):;issue: 001:;page 32
    Author(s): T. Povey; K. S. Chana; T. V. Jones; J. Hurrion
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Pronounced nonuniformities in combustor exit flow temperature (hot-streaks), which arise because of discrete injection of fuel and dilution air jets within the combustor and because of endwall ...
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