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    Discussion: “The Additive Nature of Film Cooling From Rows of Holes” (Muska, J. F., Fish, R. W., Suo, M., 1976, ASME J. Eng. Power, 98, pp. 457–463) 

    Source: Journal of Engineering for Gas Turbines and Power:;1976:;volume( 098 ):;issue: 004:;page 464
    Author(s): D. A. Nealy
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Discussion: “An Experimental Study of Turbine Vane Heat Transfer With Water–Air Cooling” (Nirmalan, N. V., Weaver, J. A., and Hylton, L. D., 1998, ASME J. Turbomach., 120, pp. 50–60) 

    Source: Journal of Turbomachinery:;1998:;volume( 120 ):;issue: 001:;page 60
    Author(s): D. A. Nealy
    Publisher: The American Society of Mechanical Engineers (ASME)
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    A Note on Turbine Cooling Performance Characterization 

    Source: Journal of Turbomachinery:;1995:;volume( 117 ):;issue: 001:;page 203
    Author(s): D. A. Nealy
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Erratum: “Some Effects of Variable Surface Temperature on Heat Transfer to a Partially Porous Flat Plate” (Journal of Engineering for Power, 1973, 95, pp. 319–325) 

    Source: Journal of Engineering for Gas Turbines and Power:;1974:;volume( 096 ):;issue: 001:;page 65
    Author(s): D. A. Nealy
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Some Effects of Variable Surface Temperature on Heat Transfer to a Partially Porous Flat Plate 

    Source: Journal of Engineering for Gas Turbines and Power:;1973:;volume( 095 ):;issue: 004:;page 319
    Author(s): D. A. Nealy
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Based on a simple enthalpy thickness approach, results are presented for laminar and turbulent heat transfer to a partially porous, nonisothermal flat plate. The model employed accounts for ...
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    Experimental Simulation of Turbine Airfoil Leading Edge Film Cooling 

    Source: Journal of Turbomachinery:;1988:;volume( 110 ):;issue: 002:;page 226
    Author(s): A. R. Wadia; D. A. Nealy
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Leading edge showerhead cooling designs represent an important feature of certain classes of high-temperature turbine airfoils. This paper outlines a methodology for predicting the surface temperatures ...
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    Evaluation of Laminated Porous Wall Materials for Combustor Liner Cooling 

    Source: Journal of Engineering for Gas Turbines and Power:;1980:;volume( 102 ):;issue: 002:;page 268
    Author(s): D. A. Nealy; S. B. Reider
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Some of the work at Detroit Diesel Allison (DDA) that has been aimed at the synthesis, characterization, and evaluation of a promising porous wall combustor-cooling concept featuring electrochemically ...
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    Some Boundary Layer-Porous Wall Coupling Effects in Laminar Flows With Surface Injection 

    Source: Journal of Engineering for Gas Turbines and Power:;1970:;volume( 092 ):;issue: 003:;page 257
    Author(s): D. A. Nealy; P. W. McFadden
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Using the integral form of the laminar boundary layer thermal energy equation, a method is developed which permits calculation of thermal boundary layer development under more general conditions ...
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    Measurements of Heat Transfer Distribution Over the Surfaces of Highly Loaded Turbine Nozzle Guide Vanes 

    Source: Journal of Engineering for Gas Turbines and Power:;1984:;volume( 106 ):;issue: 001:;page 149
    Author(s): D. A. Nealy; H. J. Gladden; M. S. Mihelc; L. D. Hylton
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The results of an experimental study of aerodynamic (surface velocity) and heat transfer distributions over the surfaces of two different, highly loaded, low-solidity contemporary turbine vane ...
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