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    Unsteady Losses in Transonic Compressors 

    Source: Journal of Engineering for Gas Turbines and Power:;1985:;volume( 107 ):;issue: 002:;page 345
    Author(s): W. F. Ng; A. H. Epstein
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A newly developed probe has been used to measure the time-resolved total temperature and pressure in a transonic compressor. The investigation revealed the presence of large fluctuations in the ...
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    Fan Noise Reduction From a Supersonic Inlet During Simulated Aircraft Approach 

    Source: Journal of Engineering for Gas Turbines and Power:;1995:;volume( 117 ):;issue: 002:;page 237
    Author(s): W. E. Nuckolls; W. F. Ng
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A series of experiments was conducted to investigate the radiation of fan noise from a supersonic inlet during a simulated aircraft approach. A scaled-down model of an axisymmetric, mixed-compression, ...
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    Experimental Measurements and Modeling of the Effects of Large-Scale Freestream Turbulence on Heat Transfer 

    Source: Journal of Turbomachinery:;2007:;volume( 129 ):;issue: 003:;page 542
    Author(s): A. C. Nix; T. E. Diller; W. F. Ng
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The influence of freestream turbulence representative of the flow downstream of a modern gas turbine combustor and first stage vane on turbine blade heat transfer has been measured and analytically ...
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    Numerical Simulations of Nonreacting Flows for Industrial Gas Turbine Combustor Geometries 

    Source: Journal of Engineering for Gas Turbines and Power:;1998:;volume( 120 ):;issue: 003:;page 460
    Author(s): H. L. Relation; W. F. Ng; J. L. Battaglioli
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This study evaluates the application of the computational fluid dynamics (CFD) to calculate the flowfields in industrial combustors. Two-burner test cases, which contain the elemental flow ...
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    Profile Synthesis and Kinematic Analysis of Pure Rolling Contact Gears 

    Source: Journal of Mechanical Design:;1992:;volume( 114 ):;issue: 002:;page 326
    Author(s): M. J. Wagner; W. F. Ng; S. G. Dhande
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The kinematic analysis of a type of gearing which allows for power transmission between shafts with pure rolling contact is presented. This proposed gearing is helical and exhibits theoretical ...
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    The Effects of Freestream Turbulence, Turbulence Length Scale, and Exit Reynolds Number on Turbine Blade Heat Transfer in a Transonic Cascade 

    Source: Journal of Turbomachinery:;2011:;volume( 133 ):;issue: 001:;page 11030
    Author(s): J. S. Carullo; K. A. Thole; L. J. Zhang; H. K. Moon; S. Nasir; R. D. Cress; W. F. Ng
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper experimentally investigates the effect of high freestream turbulence intensity, turbulence length scale, and exit Reynolds number on the surface heat transfer distribution of a turbine ...
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    Transonic and Low Supersonic Flow Losses of Two Steam Turbine Blades at Large Incidences 

    Source: Journal of Fluids Engineering:;2004:;volume( 126 ):;issue: 006:;page 966
    Author(s): S.-M. Li; Research Associate; T.-L. Chu; Graduate Student Research Assistant; Y.-S. Yoo; Research Associate; W. F. Ng; Endowed Professor
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A linear cascade experiment was conducted to investigate transonic and low supersonic flow losses of two nozzle blades for the steam turbines. In the experiment, flow incidences were changed ...
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