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    Limitations on Gas Turbine Performance Imposed by Large Turbine Cooling Flows 

    Source: Journal of Engineering for Gas Turbines and Power:;2001:;volume( 123 ):;issue: 003:;page 487
    Author(s): J. H. Horlock; D. T. Watson; T. V. Jones
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Calculations of the performance of modern gas turbines usually include allowance for cooling air flow rate; assumptions are made for the amount of the cooling air bled from the compressor, as ...
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