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    Controlling the Secondary Flow in a Turbine Cascade by Three-Dimensional Airfoil Design and Endwall Contouring 

    Source: Journal of Turbomachinery:;1999:;volume( 121 ):;issue: 002:;page 191
    Author(s): A. Duden; I. Raab; L. Fottner
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A highly loaded turbine cascade has been redesigned with the objective to reduce the secondary flow by applying endwall contouring and three-dimensional airfoil design in the endwall regions. ...
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    Improving Efficiency of a High Work Turbine Using Nonaxisymmetric Endwalls— Part I: Endwall Design and Performance 

    Source: Journal of Turbomachinery:;2010:;volume( 132 ):;issue: 002:;page 21007
    Author(s): T. Germain; P. Schüpbach; M. Rose; R. S. Abhari; M. Nagel; I. Raab
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper is the first part of a two part paper reporting the improvement of efficiency of a one-and-half stage high work axial flow turbine by nonaxisymmetric endwall contouring. In this ...
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    Improving Efficiency of a High Work Turbine Using Nonaxisymmetric Endwalls—Part II: Time-Resolved Flow Physics 

    Source: Journal of Turbomachinery:;2010:;volume( 132 ):;issue: 002:;page 21008
    Author(s): M. G. Rose; T. Germain; P. Schüpbach; R. S. Abhari; I. Raab; J. Gier
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper is the second part of a two part paper that reports on the improvement of efficiency of a one and a half stage high work axial flow turbine. The first part covered the design ...
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    Effects of Suction and Injection Purge-Flow on the Secondary Flow Structures of a High-Work Turbine 

    Source: Journal of Turbomachinery:;2010:;volume( 132 ):;issue: 002:;page 21021
    Author(s): M. G. Rose; T. Germain; P. Schuepbach; R. S. Abhari; I. Raab; J. Gier
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In high-pressure turbines, a small amount of air is ejected at the hub rim seal to cool and prevent the ingestion of hot gases into the cavity between the stator and the disk. This paper ...
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