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    M. J. Hartmann Memorial Session Paper: Turbulence Characteristics in a Supersonic Cascade Wake Flow 

    Source: Journal of Turbomachinery:;1994:;volume( 116 ):;issue: 004:;page 586
    Author(s): P. L. Andrew; Wing-fai Ng
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The turbulent character of the supersonic wake of a linear cascade of fan airfoils has been studied using a two-component laser-doppler anemometer. The cascade was tested in the Virginia ...
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    3D Numerical Investigation of Tandem Airfoils for a Core Compressor Rotor 

    Source: Journal of Turbomachinery:;2010:;volume( 132 ):;issue: 003:;page 31009
    Author(s): Jonathan McGlumphy; Steven R. Wellborn; Severin Kempf; Wing-Fai Ng
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The tandem airfoil has potential to do more work as a compressor blade than a single airfoil without incurring higher losses. The goal of this work is to evaluate the fluid mechanics of a ...
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    Showerhead Film Cooling Performance of a Turbine Vane at High Freestream Turbulence in a Transonic Cascade 

    Source: Journal of Turbomachinery:;2012:;volume( 134 ):;issue: 005:;page 51021
    Author(s): Shakeel Nasir; Trey Bolchoz; Luzeng J. Zhang; Richard J. Anthony; Hee Koo Moon; Wing-Fai Ng
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper experimentally investigates the effect of blowing ratio and exit Reynolds number/Mach number on the film cooling performance of a showerhead film cooled first stage turbine vane. The ...
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    Numerical Investigation of Tandem Airfoils for Subsonic Axial-Flow Compressor Blades 

    Source: Journal of Turbomachinery:;2009:;volume( 131 ):;issue: 002:;page 21018
    Author(s): Jonathan McGlumphy; Steven R. Wellborn; Severin Kempf; Wing-Fai Ng
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The tandem airfoil has potential to do more work as a compressor blade than a single airfoil without incurring significantly higher losses. Although tandem blades are sometimes employed as ...
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    Effects of Large Scale High Freestream Turbulence and Exit Reynolds Number on Turbine Vane Heat Transfer in a Transonic Cascade 

    Source: Journal of Turbomachinery:;2009:;volume( 131 ):;issue: 002:;page 21021
    Author(s): Shakeel Nasir; Luzeng J. Zhang; Hee Koo Moon; Jeffrey S. Carullo; Wing-Fai Ng; Karen A. Thole; Hong Wu
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper experimentally and numerically investigates the effects of large scale high freestream turbulence intensity and exit Reynolds number on the surface heat transfer distribution of a ...
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