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    Influence of Endwall Flow on Airfoil Suction Surface Midheight Boundary Layer Development in a Turbine Cascade 

    Source: Journal of Engineering for Gas Turbines and Power:;1983:;volume( 105 ):;issue: 001:;page 147
    Author(s): O. P. Sharma; R. A. Graziani
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents the results of an analysis to assess the influence of cascade passage endwall flow on the airfoil suction surface midheight boundary layer development in a turbine cascade. ...
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    Heat Transfer in Rotating Serpentine Passages With Trips Normal to the Flow 

    Source: Journal of Turbomachinery:;1992:;volume( 114 ):;issue: 004:;page 847
    Author(s): J. H. Wagner; R. A. Graziani; F. C. Yeh; B. V. Johnson
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Experiments were conducted to determine the effects of buoyancy and Coriolis forces on heat transfer in turbine blade internal coolant passages. The experiments were conducted with a large-scale, ...
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    An Experimental Study of Endwall and Airfoil Surface Heat Transfer in a Large Scale Turbine Blade Cascade 

    Source: Journal of Engineering for Gas Turbines and Power:;1980:;volume( 102 ):;issue: 002:;page 257
    Author(s): R. A. Graziani; M. F. Blair; J. R. Taylor; R. E. Mayle
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Local rates of heat transfer on the endwall, suction, and pressure surfaces of a large scale turbine blade cascade were measured for two inlet boundary layer thicknesses and for a Reynolds ...
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