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    An Improved Particle Impact Model by Accounting for Rate of Strain and Stochastic Rebound 

    Source: Journal of Turbomachinery:;2022:;volume( 145 ):;issue: 001:;page 11010-1
    Author(s): Whitaker, Steven M.; Bons, Jeffrey P.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A methodology for informing physics-based impact and deposition models through the use of novel experimental and analysis techniques is presented. Coefficient of restitution (CoR) data were obtained for Arizona Road Dust ...
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    Challenges Associated With Replicating Rotor Blade Deposition in a Non-Rotating Annular Cascade 

    Source: Journal of Turbomachinery:;2020:;volume( 142 ):;issue: 009:;page 091003-1
    Author(s): Bowen, Christopher P.; Ameri, Ali; Bons, Jeffrey P.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A computational analysis is performed to determine if particulate impact events on the external surfaces of gas turbine engine rotor blades can be faithfully replicated in an experimental rotor cascade. The general electric ...
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    Modeling Deposition in Gas Turbines With Conjugate Mesh-Morphing and Temperature Sensitivity 

    Source: Journal of Turbomachinery:;2026:;volume( 148 ):;issue:004:;page 2274
    Author(s): Jacobs, Bradley C.; Bons, Jeffrey P.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Abstract. A versatile procedure is presented for simulating the growth and thermal impact of deposition in representative gas turbine cooling circuits. The methodology comprises the following sequence: (1) employ computational ...
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    Deposition on a Cooled Nozzle Guide Vane With Nonuniform Inlet Temperatures 

    Source: Journal of Turbomachinery:;2016:;volume( 138 ):;issue: 010:;page 101005
    Author(s): Prenter, Robin; Ameri, Ali; Bons, Jeffrey P.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: External deposition on a slot film cooled nozzle guide vane, subjected to nonuniform inlet temperatures, was investigated experimentally and computationally. Experiments were conducted using a fourvane cascade, operating ...
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    A Global Approach to Turbomachinery Flow Control: Passage Vortex Control 

    Source: Journal of Turbomachinery:;2014:;volume( 136 ):;issue: 004:;page 41003
    Author(s): Bloxham, Matthew J.; Bons, Jeffrey P.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A flow control scheme was implemented in a lowpressure turbine cascade that simultaneously mitigated profile and endwall losses using midspan vortex generator jets (VGJs) and endwall suction. The combined system had an ...
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    Computational Simulation of Deposition in a Cooled High-Pressure Turbine Stage With Hot Streaks 

    Source: Journal of Turbomachinery:;2017:;volume( 139 ):;issue: 009:;page 91005
    Author(s): Prenter, Robin; Ameri, Ali; Bons, Jeffrey P.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Ash particle deposition in a high-pressure turbine stage was numerically investigated using steady Reynolds-averaged Navier-Stokes (RANS) and unsteady Reynolds-averaged Navie-Stokes (URANS) methods. An inlet temperature ...
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    The Effect of Training Data on Predicting Turbulent Flow Through a Linear Cascade Using Physics-Informed Neural Networks 

    Source: Journal of Turbomachinery:;2026:;volume( 148 ):;issue:003
    Author(s): McNichols, Ezra O.; Bons, Jeffrey P.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Abstract. This article investigates the effect of training data on the accuracy of turbulent flow predictions in the wake region of a linear turbine cascade using physics-informed neural networks (PINNs). While it is well ...
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    Experimental Investigation of Sweeping Jet Film Cooling in a Transonic Turbine Cascade 

    Source: Journal of Turbomachinery:;2020:;volume( 142 ):;issue: 004
    Author(s): Hossain, Mohammad A.; Asar, Munevver E.; Gregory, James W.; Bons, Jeffrey P.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The sweeping jet (SJ) film cooling hole has shown promising cooling performance compared to the standard shaped hole in low-speed conditions. The present work demonstrates the first attempt of SJ film cooling at an engine ...
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    A Simplified Injection Model for Variable Area Turbine Fluidic Throttling 

    Source: Journal of Turbomachinery:;2024:;volume( 147 ):;issue: 003:;page 31008-1
    Author(s): Spens, Alexander; McFadden, Evan J.; Westrick, Cole D.; Bons, Jeffrey P.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Previous studies have demonstrated the effectiveness of using fluidic actuators to throttle the flow through a nozzle guide vane, enabling a variable area turbine (VAT) with no moving parts. A simplified model was developed ...
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    Electrostatic Effects on Airborne Particle Deposition in Gas Turbine Engines 

    Source: Journal of Turbomachinery:;2026:;volume( 148 ):;issue:006
    Author(s): Sabau, Tanner J.; Frith, Kyle H.; Bons, Jeffrey P.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Abstract. The effects of electrostatics on the deposition of 0–5 µm Arizona Road Dust within a gas turbine hot section were studied. These experiments focused on different cooling methods found in turbine components: ...
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