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    Closure to “Discussion of ‘Prediction of Cascade Performance Using an Incompressible Navier–Stokes Technique’” (1991, ASME J. Turbomach., 113, pp. 571–572) 

    Source: Journal of Turbomachinery:;1991:;volume( 113 ):;issue: 004:;page 572
    Author(s): G. V. Hobson; B. Lakshminarayana
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Prediction of Cascade Performance Using an Incompressible Navier–Stokes Technique 

    Source: Journal of Turbomachinery:;1991:;volume( 113 ):;issue: 004:;page 561
    Author(s): G. V. Hobson; B. Lakshminarayana
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A fully elliptic, control volume solution of the two-dimensional incompressible Navier–Stokes equations for the prediction of cascade performance over a wide range is presented in this paper. The ...
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    Pre-Stall Instability Distribution Over a Transonic Compressor Rotor 

    Source: Journal of Fluids Engineering:;2009:;volume( 131 ):;issue: 005:;page 51106
    Author(s): A. J. Gannon; G. V. Hobson
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An investigation of the behavior of a transonic compressor rotor when operating close to stall is presented. The specific areas of interest are the behavior and location of low-frequency ...
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    Three-Component LDV Measurements in the Wake of a Compressor Cascade With Flow Separation 

    Source: Journal of Turbomachinery:;2008:;volume( 130 ):;issue: 001:;page 11008
    Author(s): G. V. Hobson; T. M. Caruso; J. R. Carlson
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Measurements were taken of the vortex system and turbulent flow that resulted from the interaction between a stator blade and the approaching endwall boundary layer in a linear cascade of ...
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    Laser-Doppler-Velocimetry Measurements in a Cascade of Compressor Blades at Stall 

    Source: Journal of Turbomachinery:;1998:;volume( 120 ):;issue: 001:;page 170
    Author(s): G. V. Hobson; A. J. H. Williams; H. J. Ganaim Rickel
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Compressor stall was simulated in the Low-Speed Cascade Wind Tunnel at the Turbopropulsion Laboratory of the Naval Postgraduate School. The test blades were of controlled-diffusion design with a ...
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