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    Endwall Losses and Flow Unsteadiness in a Turbine Blade Cascade 

    Source: Journal of Turbomachinery:;1992:;volume( 114 ):;issue: 001:;page 191
    Author(s): L. Adjlout; S. L. Dixon
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The purpose of this paper is to describe an investigation of the flow within and downstream of a turbine blade cascade of high aspect ratio. A detailed experimental investigation into the ...
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    Discussion: “Annulus Wall Boundary Layers in Axial Compressors” (Horlock, J. H., 1963, ASME J. Basic Eng., 85, pp. 55–61) 

    Source: Journal of Fluids Engineering:;1967:;volume( 089 ):;issue: 001:;page 239
    Author(s): J. H. Horlock; S. L. Dixon
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Pressure Losses in Combining Subsonic Flows Through Branched Ducts 

    Source: Journal of Turbomachinery:;1992:;volume( 114 ):;issue: 001:;page 264
    Author(s): N. I. Abou-Haidar; S. L. Dixon
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An investigation of the “additional” total pressure losses occurring in combining flow through several sharp-edged three-leg junctions has been made. Experimental results covering a wide speed ...
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    Measurement of Compressible Flow Pressure Losses in Wye-Junctions 

    Source: Journal of Turbomachinery:;1994:;volume( 116 ):;issue: 003:;page 535
    Author(s): N. I. Abou-Haidar; S. L. Dixon
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper considers the compressible flow pressure losses in sharp-cornered wye-junctions with symmetric branches under dividing and combining flow conditions. Determination of the additional total ...
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    Growth of Secondary Flow Losses Downstream of a Turbine Blade Cascade 

    Source: Journal of Engineering for Gas Turbines and Power:;1986:;volume( 108 ):;issue: 002:;page 270
    Author(s): L. D. Chen; S. L. Dixon
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Endwall total pressure losses downstream of a low-speed turbine cascade have been measured at several planes in order to determine the changes in secondary flow loss coefficients and the growth ...
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