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    Effects of Reynolds Number and Freestream Turbulence Intensity on the Unsteady Boundary Layer Development on an Ultra-High-Lift Low Pressure Turbine Airfoil 

    Source: Journal of Turbomachinery:;2010:;volume( 132 ):;issue: 001:;page 11016
    Author(s): Xue Feng Zhang; Howard Hodson
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The effects of Reynolds numbers and the freestream turbulence intensities (FSTIs) on the unsteady boundary layer development on an ultra-high-lift low-pressure turbine airfoil, so-called T106C, are ...
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    Combined Effects of Surface Trips and Unsteady Wakes on the Boundary Layer Development of an Ultra-High-Lift LP Turbine Blade 

    Source: Journal of Turbomachinery:;2005:;volume( 127 ):;issue: 003:;page 479
    Author(s): Xue Feng Zhang; Howard Hodson
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An experimental investigation of the combined effects of upstream unsteady wakes and surface trips on the boundary layer development on an ultra-high-lift low-pressure turbine blade, known as ...
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    Separation and Transition Control on an Aft-Loaded Ultra-High-Lift LP Turbine Blade at Low Reynolds Numbers: High-Speed Validation 

    Source: Journal of Turbomachinery:;2007:;volume( 129 ):;issue: 002:;page 340
    Author(s): Maria Vera; Neil Harvey; Xue Feng Zhang; Howard Hodson
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents the second part of an investigation of the combined effects of unsteadiness and surface roughness on an aft-loaded ultra-high-lift low-pressure turbine (LPT) profile at low ...
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    Separation and Transition Control on an Aft-Loaded Ultra-High-Lift LP Turbine Blade at Low Reynolds Numbers: Low-Speed Investigation 

    Source: Journal of Turbomachinery:;2006:;volume( 128 ):;issue: 003:;page 517
    Author(s): Xue Feng Zhang; Neil Harvey; Maria Vera; Howard Hodson
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An experimental study was conducted to improve the performance of an aft-loaded ultra-high-lift low-pressure turbine blade known as U2 at low Reynolds numbers. This was achieved by manipulation ...
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