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    A Turbomachinery Design Tool for Teaching Design Concepts for Axial-Flow Fans, Compressors, and Turbines 

    Source: Journal of Turbomachinery:;2011:;volume( 133 ):;issue: 003:;page 31017
    Author(s): Mark G. Turner; Ali Merchant; Dario Bruna
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A new turbomachinery design system, T-AXI, is described and demonstrated. It is intended primarily for use by educators and students, although it is sophisticated enough for actual designs. The ...
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    Radial Migration of Shed Vortices in a Transonic Rotor Following a Wake Generator: A Comparison Between Time Accurate and Average Passage Approaches 

    Source: Journal of Turbomachinery:;2011:;volume( 133 ):;issue: 003:;page 31018
    Author(s): Mark G. Turner; Steven E. Gorrell; David Car
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper shows a comparison of an unsteady simulation using turbo and an average passage simulation for a two blade row configuration consisting of a wake generator followed by a transonic ...
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    An Educational Software Suite for Teaching Design Strategies for Multistage Axial Flow Compressors 

    Source: Journal of Turbomachinery:;2012:;volume( 134 ):;issue: 005:;page 51010
    Author(s): Dario Bruna; Carlo Cravero; Mark G. Turner; Ali Merchant
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The T-AXI turbomachinery design system, an axisymmetric methodology recently developed with an educational purpose, has shown great capabilities in the redesign of existing axial flow gas turbine ...
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    Investigation of Loss Generation in an Embedded Transonic Fan Stage at Several Gaps Using High-Fidelity, Time-Accurate Computational Fluid Dynamics 

    Source: Journal of Turbomachinery:;2010:;volume( 132 ):;issue: 001:;page 11014
    Author(s): Michael G. List; Steven E. Gorrell; Mark G. Turner
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The blade-row interaction (BRI) rig at the Air Force Research Laboratory, Compressor Aero Research Laboratory, has been simulated at three axial gaps between the highly loaded upstream stator ...
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    DSpace software copyright © 2002-2015  DuraSpace
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