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    Effect of Blade Profile Contouring on Endwall Flow Structure in a High-Lift Low-Pressure Turbine Cascade 

    Source: Journal of Turbomachinery:;2017:;volume( 139 ):;issue: 002:;page 21006
    Author(s): Sangston, Keith; Little, Jesse; Eric Lyall, M.; Sondergaard, Rolf
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Previous work has shown that low-stagger contouring near the endwall of a nominally high-lift and high-stagger angle front-loaded low-pressure turbine (LPT) airfoil is successful in reducing endwall loss by limiting the ...
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    End Wall Loss Reduction of High Lift Low Pressure Turbine Airfoils Using Profile Contouring—Part II: Validation 

    Source: Journal of Turbomachinery:;2014:;volume( 136 ):;issue: 008:;page 81006
    Author(s): Sangston, Keith; Little, Jesse; Lyall, M. Eric; Sondergaard, Rolf
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The hypothesis, posed in Part I, that excessive end wall loss of high lift low pressure turbine (LPT) airfoils is due to the influence of high stagger angles on the end wall pressure distribution and not front loading is ...
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