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    A Review of Surface Roughness Effects in Gas Turbines 

    Source: Journal of Turbomachinery:;2010:;volume( 132 ):;issue: 002:;page 21004
    Author(s): J. P. Bons
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The effects of surface roughness on gas turbine performance are reviewed based on publications in the open literature over the past 60 years. Empirical roughness correlations routinely employed ...
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    Flow Physics Leading to System Instability in a Centrifugal Pump 

    Source: Journal of Turbomachinery:;1994:;volume( 116 ):;issue: 004:;page 612
    Author(s): A. M. Wo; J. P. Bons
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The off-design performance in a centrifugal pump is investigated experimentally. The objective is to identify flow features that lead to the onset of surge as the fundamental pumping system ...
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    1998 Heat Transfer Committee Best Paper Award: Complementary Velocity and Heat Transfer Measurements in a Rotating Cooling Passage With Smooth Walls 

    Source: Journal of Turbomachinery:;1999:;volume( 121 ):;issue: 004:;page 651
    Author(s): J. P. Bons; J. L. Kerrebrock
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An experimental investigation was conducted on the internal flowfield of a simulated smooth-wall turbine blade cooling passage. The square cross-sectioned passage was manufactured from quartz for ...
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    Effects of a Realistically Rough Surface on Vane Heat Transfer Including the Influence of Turbulence Condition and Reynolds Number 

    Source: Journal of Turbomachinery:;2012:;volume( 134 ):;issue: 002:;page 21013
    Author(s): E. L. Erickson; F. E. Ames; J. P. Bons
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Heat transfer distributions are experimentally acquired and reported for a vane with both a smooth and a realistically rough surface. Surface heat transfer is investigated over a range of ...
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    The Effect of High Free-Stream Turbulence on Film Cooling Effectiveness 

    Source: Journal of Turbomachinery:;1996:;volume( 118 ):;issue: 004:;page 814
    Author(s): J. P. Bons; C. D. MacArthur; R. B. Rivir
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This study investigated the adiabatic wall cooling effectiveness of a single row of film cooling holes injecting into a turbulent flat plate boundary layer below a turbulent, zero pressure ...
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    A Comparison of Approximate Versus Exact Geometrical Representations of Roughness for CFD Calculations of cf and St 

    Source: Journal of Turbomachinery:;2008:;volume( 130 ):;issue: 002:;page 21024
    Author(s): J. P. Bons; S. T. McClain; Z. J. Wang; X. Chi; T. I. Shih
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Skin friction (cf) and heat transfer (St) predictions were made for a turbulent boundary layer over randomly rough surfaces at Reynolds number of 1×106. The rough surfaces are scaled models ...
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    Synchronizing Separation Flow Control With Unsteady Wakes in a Low-Pressure Turbine Cascade 

    Source: Journal of Turbomachinery:;2009:;volume( 131 ):;issue: 002:;page 21019
    Author(s): M. Bloxham; D. Reimann; K. Crapo; J. Pluim; J. P. Bons
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Particle image velocimetry (PIV) measurements were made on a highly loaded low-pressure turbine blade in a linear cascade. The Pack B blade has a design Zweifel coefficient of 1.15 and a peak ...
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    The Effect of Particle Size and Film Cooling on Nozzle Guide Vane Deposition 

    Source: Journal of Engineering for Gas Turbines and Power:;2012:;volume( 134 ):;issue: 010:;page 101901
    Author(s): C. Bonilla; J. Webb; C. Clum; B. Casaday; E. Brewer; J. P. Bons
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An accelerated deposition test facility is used to study the effect of particle size and film cooling on deposit roughness, spatial distribution, and thickness. Tests were run at gas turbine ...
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