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    A New Model for Boundary Layer Transition Using a Single-Point RANS Approach 

    Source: Journal of Turbomachinery:;2004:;volume( 126 ):;issue: 001:;page 193
    Author(s): D. Keith Walters; James H. Leylek
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents the development and implementation of a new model for bypass and natural transition prediction using Reynolds-averaged Navier-Stokes computational fluid dynamics (CFD), based ...
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    Computational Fluid Dynamics Study of Wake-Induced Transition on a Compressor-Like Flat Plate 

    Source: Journal of Turbomachinery:;2005:;volume( 127 ):;issue: 001:;page 52
    Author(s): D. Keith Walters; James H. Leylek
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Recent experimental work has documented the importance of wake passing on the behavior of transitional boundary layers on the suction surface of axial compressor blades. This paper documents ...
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    Impact of Film-Cooling Jets on Turbine Aerodynamic Losses 

    Source: Journal of Turbomachinery:;2000:;volume( 122 ):;issue: 003:;page 537
    Author(s): Dibbon K. Walters; James H. Leylek
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper documents a computational investigation of the aerodynamic impact of film cooling on a linear turbine airfoil cascade. The simulations were for single row injection on both the ...
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    Leading-Edge Film-Cooling Physics—Part III: Diffused Hole Effectiveness 

    Source: Journal of Turbomachinery:;2003:;volume( 125 ):;issue: 002:;page 252
    Author(s): William D. York; James H. Leylek
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A proven computational methodology was applied to investigate film cooling from diffused holes on the simulated leading edge of a turbine airfoil. The short film-hole diffuser section was conical ...
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