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    St and cf Augmentation for Real Turbine Roughness With Elevated Freestream Turbulence 

    Source: Journal of Turbomachinery:;2002:;volume( 124 ):;issue: 004:;page 632
    Author(s): Jeffrey P. Bons
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Experimental measurements of skin friction (cf) and heat transfer (St) augmentation are reported for low speed flow over turbine roughness models. The models were scaled from surface measurements ...
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    Separated Flow Transition on an LP Turbine Blade With Pulsed Flow Control 

    Source: Journal of Turbomachinery:;2008:;volume( 130 ):;issue: 002:;page 21014
    Author(s): Jeffrey P. Bons; Daniel Reimann; Matthew Bloxham
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Flow measurements were made on a highly loaded low pressure turbine blade in a low-speed linear cascade facility. The blade has a design Zweifel coefficient of 1.34 with a peak pressure ...
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    The Effect of Real Turbine Roughness With Pressure Gradient on Heat Transfer 

    Source: Journal of Turbomachinery:;2004:;volume( 126 ):;issue: 003:;page 385
    Author(s): Jeffrey P. Bons; Stephen T. McClain
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Experimental measurements of heat transfer (St) are reported for low speed flow over scaled turbine roughness models at three different freestream pressure gradients: adverse, zero (nominally), ...
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    The Effect of Element Thermal Conductivity on Turbulent Convective Heat Transfer From Rough Surfaces 

    Source: Journal of Turbomachinery:;2011:;volume( 133 ):;issue: 002:;page 21024
    Author(s): Stephen T. McClain; B. Keith Hodge; Jeffrey P. Bons
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The discrete-element model for flows over rough surfaces considers the heat transferred from a rough surface to be the sum of the heat convected from the flat surface and the heat convected ...
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    Turbine Separation Control Using Pulsed Vortex Generator Jets 

    Source: Journal of Turbomachinery:;2001:;volume( 123 ):;issue: 002:;page 198
    Author(s): Jeffrey P. Bons; Rolf Sondergaard; Richard B. Rivir
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The application of pulsed vortex generator jets to control separation on the suction surface of a low-pressure turbine blade is reported. Blade Reynolds numbers in the experimental, linear turbine ...
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    The Fluid Dynamics of LPT Blade Separation Control Using Pulsed Jets 

    Source: Journal of Turbomachinery:;2002:;volume( 124 ):;issue: 001:;page 77
    Author(s): Jeffrey P. Bons; Rolf Sondergaard; Richard B. Rivir
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The effects of pulsed vortex generator jets on a naturally separating low-pressure turbine boundary layer have been investigated experimentally. Blade Reynolds numbers in the linear turbine cascade ...
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    The Application of Flow Control to an Aft-Loaded Low Pressure Turbine Cascade With Unsteady Wakes 

    Source: Journal of Turbomachinery:;2012:;volume( 134 ):;issue: 003:;page 31009
    Author(s): Jeffrey P. Bons; John P. Clark; Jon Pluim; Kyle Gompertz; Matthew Bloxham
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The synchronous application of flow control in the presence of unsteady wakes was studied on a highly loaded low pressure turbine blade. At low Reynolds numbers, the blade exhibits a nonreattaching ...
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    Deposition Near Film Cooling Holes on a High Pressure Turbine Vane 

    Source: Journal of Turbomachinery:;2012:;volume( 134 ):;issue: 004:;page 41013
    Author(s): Weiguo Ai; Spencer Harding; Scott Lewis; Jeffrey P. Bons; Nathan Murray; Thomas H. Fletcher
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Deposition on film-cooled turbine components was studied in an accelerated test facility. The accelerated deposition facility seeds a natural-gas burning combustor with finely ground coal ash ...
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    Effect of Hole Spacing on Deposition of Fine Coal Flyash Near Film Cooling Holes 

    Source: Journal of Turbomachinery:;2012:;volume( 134 ):;issue: 004:;page 41021
    Author(s): Weiguo Ai; Spencer Harding; Jeffrey P. Bons; Nathan Murray; Thomas H. Fletcher
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Particulate deposition experiments were performed in a turbine accelerated deposition facility to examine the nature of flyash deposits near film cooling holes. Deposition on both bare metal and ...
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    Evolution of Surface Deposits on a High-Pressure Turbine Blade—Part I: Physical Characteristics 

    Source: Journal of Turbomachinery:;2008:;volume( 130 ):;issue: 002:;page 21020
    Author(s): James E. Wammack; Thomas H. Fletcher; Jared Crosby; Daniel Fletcher; Jeffrey P. Bons
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Turbine blade coupons with three different surface treatments were exposed to deposition conditions in an accelerated deposition facility. The facility simulates the flow conditions at the inlet ...
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