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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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    Investigation of the Three-Dimensional Flow Field Within a Transonic Fan Rotor: Experiment and Analysis 

    Source: Journal of Engineering for Gas Turbines and Power:;1985:;volume( 107 ):;issue: 002:;page 436
    Author(s): M. J. Pierzga; J. R. Wood
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An experimental investigation of the three-dimensional flow field through a low aspect ratio, transonic, axial-flow fan rotor has been conducted using an advanced laser anemometer (LA) system. ...
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    Effect of Area Ratio on the Performance of a 5.5:1 Pressure Ratio Centrifugal Impeller 

    Source: Journal of Turbomachinery:;1987:;volume( 109 ):;issue: 001:;page 10
    Author(s): L. F. Schumann; J. R. Wood; D. A. Clark
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A centrifugal impeller which was initially designed for a pressure ratio of approximately 5.5 and a mass flow rate of 0.959 kg/s was tested with a vaneless diffuser for a range of design ...
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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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    Application of Advanced Computational Codes in the Design of an Experiment for a Supersonic Throughflow Fan Rotor 

    Source: Journal of Turbomachinery:;1988:;volume( 110 ):;issue: 002:;page 270
    Author(s): J. R. Wood; J. F. Schmidt; R. J. Steinke; R. V. Chima; W. G. Kunik
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Increased emphasis on sustained supersonic or hypersonic cruise has revived interest in the supersonic throughflow fan as a possible component in advanced propulsion systems. Use of a fan that ...
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    On Flowfield Periodicity in the NASA Transonic Flutter Cascade 

    Source: Journal of Turbomachinery:;2001:;volume( 123 ):;issue: 003:;page 501
    Author(s): J. Lepicovsky; R. V. Chima; E. R. McFarland; J. R. Wood
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A combined experimental and numerical program was carried out to improve the flow uniformity and periodicity in the NASA transonic flutter cascade. The objectives of the program were to improve ...
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