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    Numerical Investigation of Three-Dimensional Separation in an Axial Flow Compressor: The Influence of Freestream Turbulence Intensity and Endwall Boundary Layer State 

    Source: Journal of Turbomachinery:;2017:;volume( 139 ):;issue: 002:;page 21011
    Author(s): Scillitoe, Ashley D.; Tucker, Paul G.; Adami, Paolo
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Regions of three-dimensional separations are an inherent flow feature of the suction surface-endwall corner in axial compressors. These corner separations can cause a significant total pressure loss and reduce the compressor's ...
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    Large Eddy Simulation of Boundary Layer Transition Mechanisms in a Gas-Turbine Compressor Cascade 

    Source: Journal of Turbomachinery:;2019:;volume( 141 ):;issue: 006:;page 61008
    Author(s): Scillitoe, Ashley D.; Tucker, Paul G.; Adami, Paolo
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Large eddy simulation (LES) is used to explore the boundary layer transition mechanisms in two rectilinear compressor cascades. To reduce numerical dissipation, a novel locally adaptive smoothing (LAS) scheme is added to ...
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    Modification of Shear Stress Transport Turbulence Model Using Helicity for Predicting Corner Separation Flow in a Linear Compressor Cascade 

    Source: Journal of Turbomachinery:;2020:;volume( 142 ):;issue: 002
    Author(s): Liu, Yangwei; Tang, Yumeng; Scillitoe, Ashley D.; Tucker, Paul G.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Three-dimensional corner separation significantly affects compressor performance, but turbulence models struggle to predict it accurately. This paper assesses the capability of the original shear stress transport (SST) ...
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