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    An Experimental Study of Turbine Vane Heat Transfer With Leading Edge and Downstream Film Cooling 

    Source: Journal of Turbomachinery:;1990:;volume( 112 ):;issue: 003:;page 477
    Author(s): N. V. Nirmalan; L. D. Hylton
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents the effects of downstream film cooling, with and without leading edge showerhead film cooling, on turbine vane external heat transfer. Steady-state experimental measurements ...
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    An Experimental Study of Turbine Vane Heat Transfer With Water–Air Cooling 

    Source: Journal of Turbomachinery:;1998:;volume( 120 ):;issue: 001:;page 50
    Author(s): N. V. Nirmalan; J. A. Weaver; L. D. Hylton
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents data showing the improvement in cooling effectiveness of turbine vanes through the application of water–air cooling technology in an industrial/utility engine application. The ...
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    Closure to “Discussion of ‘An Experimental Study of Turbine Vane Heat Transfer With Water–Air Cooling’” (1998, ASME J. Turbomach., 120, pp. 60–61) 

    Source: Journal of Turbomachinery:;1998:;volume( 120 ):;issue: 001:;page 61
    Author(s): N. V. Nirmalan; J. A. Weaver; L. D. Hylton
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Experimental and Numerical Study of Heat Transfer in a Gas Turbine Combustor Liner 

    Source: Journal of Engineering for Gas Turbines and Power:;2003:;volume( 125 ):;issue: 004:;page 994
    Author(s): J. C. Bailey; J. Intile; A. K. Tolpadi; N. V. Nirmalan; R. S. Bunker; T. F. Fric
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Experiments and numerical simulations were conducted to understand the heat transfer characteristics of a stationary gas turbine combustor liner cooled by impingement jets and cross flow between ...
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