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    Application of a Multi-Block CFD Code to Investigate the Impact of Geometry Modeling on Centrifugal Compressor Flow Field Predictions 

    Source: Journal of Turbomachinery:;1997:;volume( 119 ):;issue: 004:;page 820
    Author(s): M. D. Hathaway; J. R. Wood
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: CFD codes capable of utilizing multi-block grids provide the capability to analyze the complete geometry of centrifugal compressors including, among others, multiple splitter rows, tip clearance, ...
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    A Note on Blade Wake Interaction Influence on Compressor Stator Row Aerodynamic Performance 

    Source: Journal of Engineering for Gas Turbines and Power:;1985:;volume( 107 ):;issue: 002:;page 549
    Author(s): T. H. Okiishi; M. D. Hathaway; J. L. Hansen
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Stator Endwall Leading-Edge Sweep and Hub Shroud Influence on Compressor Performance 

    Source: Journal of Turbomachinery:;1986:;volume( 108 ):;issue: 002:;page 224
    Author(s): D. L. Tweedt; M. D. Hathaway; T. H. Okiishi
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The use of stator endwall leading-edge sweep to improve axial-flow compressor stator row performance was examined experimentally. The aerodynamics of three stator hub (inner diameter) conditions, ...
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    NASA Low-Speed Centrifugal Compressor for Three-Dimensional Viscous Code Assessment and Fundamental Flow Physics Research 

    Source: Journal of Turbomachinery:;1992:;volume( 114 ):;issue: 002:;page 295
    Author(s): M. D. Hathaway; J. R. Wood; C. A. Wasserbauer
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A low-speed centrifugal compressor facility recently built by the NASA Lewis Research Center is described. The purpose of this facility is to obtain detailed flow field measurements for computational ...
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    Experimental and Computational Results From the NASA Lewis Low-Speed Centrifugal Impeller at Design and Part-Flow Conditions 

    Source: Journal of Turbomachinery:;1996:;volume( 118 ):;issue: 001:;page 55
    Author(s): R. M. Chriss; M. D. Hathaway; J. R. Wood
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The NASA Lewis Low-Speed Centrifugal Compressor (LSCC) has been investigated with laser anemometry and computational analysis at two flow conditions: the design condition as well as a lower mass ...
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    Closure to “Discussion of ‘Experimental and Computational Investigation of the NASA Low-Speed Centrifugal Compressor Flow Field’” (1993, ASME J. Turbomach., 115, pp. 541–542) 

    Source: Journal of Turbomachinery:;1993:;volume( 115 ):;issue: 003:;page 542
    Author(s): M. D. Hathaway; R. M. Chriss; J. R. Wood; A. J. Strazisar
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Experimental and Computational Investigation of the NASA Low-Speed Centrifugal Compressor Flow Field 

    Source: Journal of Turbomachinery:;1993:;volume( 115 ):;issue: 003:;page 527
    Author(s): M. D. Hathaway; R. M. Chriss; J. R. Wood; A. J. Strazisar
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An experimental and computational investigation of the NASA Low-Speed Centrifugal Compressor (LSCC) flow field has been conducted using laser anemometry and Dawes’ three dimensional viscous code. ...
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