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    Cooling Air Flow Characteristics in Gas Turbine Components 

    Source: Journal of Engineering for Gas Turbines and Power:;1982:;volume( 104 ):;issue: 002:;page 275
    Author(s): H. F. Jen; J. B. Sobanik
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An analytical model for the prediction of cooling air flow characteristics (mass flow rate and internal pressure distribution) in gas turbine components is discussed. The model addresses a number ...
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    Cooling Airflow Studies at the Leading Edge of a Film-Cooled Airfoil 

    Source: Journal of Engineering for Gas Turbines and Power:;1984:;volume( 106 ):;issue: 001:;page 214
    Author(s): E. S. Tillman; H. F. Jen
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An experimental flow study on cooling holes in cylindrical models simulating the leading edge of a typical turbine airfoil is presented. The effect of external flow around the cylinder on the ...
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    The Prediction of Flow Through Leading Edge Holes in a Film Cooled Airfoil With and Without Inserts 

    Source: Journal of Engineering for Gas Turbines and Power:;1985:;volume( 107 ):;issue: 001:;page 92
    Author(s): E. S. Tillman; E. O. Hartel; H. F. Jen
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A method for predicting cooling air flow rates using tests on cylindrical models of typical turbine blade leading edges has been extended to include blades with inserts and blades with ...
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    Airfoil Heat Transfer Calculation Using a Low Reynolds Number Version of a Two-Equation Turbulence Model 

    Source: Journal of Engineering for Gas Turbines and Power:;1985:;volume( 107 ):;issue: 001:;page 60
    Author(s): J. H. Wang; H. F. Jen; E. O. Hartel
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A two-dimensional, boundary-layer program, STAN5, was modified to incorporate a low-Reynolds number version of the K-ε, two-equation turbulence model for the predictions of flow and heat transfer ...
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