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    Optimized Shroud Design for Axial Turbine Aerodynamic Performance 

    Source: Journal of Turbomachinery:;2008:;volume( 130 ):;issue: 003:;page 31016
    Author(s): L. Porreca; A. I. Kalfas; R. S. Abhari
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents a comprehensive study of the effect of shroud design in axial turbine aerodynamics. Experimental measurements and numerical simulations have been conducted on three different ...
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    Multistage Aspects and Unsteady Effects of Stator and Rotor Clocking in an Axial Turbine With Low Aspect Ratio Blading 

    Source: Journal of Turbomachinery:;2006:;volume( 128 ):;issue: 001:;page 11
    Author(s): T. Behr; L. Porreca; T. Mokulys; A. I. Kalfas; R. S. Abhari
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents the outcome of a recent study in clocking-related flow features and multistage effects occurring in high-pressure turbine blade geometries. The current investigation deals with ...
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    Fluid Dynamics and Performance of Partially and Fully Shrouded Axial Turbines 

    Source: Journal of Turbomachinery:;2005:;volume( 127 ):;issue: 004:;page 668
    Author(s): L. Porreca; T. Behr; J. Ehrhard; E. Janke; J. Schlienger; A. I. Kalfas; R. S. Abhari
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A unique comparative experimental and numerical investigation carried out on two test cases with shroud configurations, differing only in the labyrinth seal path, is presented in this paper. The ...
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    Interstage Flow Interactions and Loss Generation in a Two-Stage Shrouded Axial Turbine 

    Source: Journal of Turbomachinery:;2009:;volume( 131 ):;issue: 001:;page 11002
    Author(s): L. Porreca; Y. I. Yun; S. J. Song; A. I. Kalfas; R. S. Abhari
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The aerodynamics and kinematics of flow structures, including the loss generation mechanisms, in the interstage region of a two-stage partially shrouded axial turbine are examined. The nonaxisymmetric ...
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