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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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    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 Freestream Turbulence on Deposition for Nozzle Guide Vanes 

    Source: Journal of Turbomachinery:;2015:;volume( 137 ):;issue: 012:;page 121001
    Author(s): Whitaker, Steven M.; Prenter, Robin; Bons, Jeffrey P.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An evaluation of the effect of freestream turbulence intensity on the rate of deposit accumulation for nozzle guide vanes (NGVs) was performed using the turbine reacting flow rig (TuRFR) accelerated deposition facility. ...
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    Deposition With Hot Streaks in an Uncooled Turbine Vane Passage 

    Source: Journal of Turbomachinery:;2014:;volume( 136 ):;issue: 004:;page 41017
    Author(s): Casaday, Brian; Prenter, Robin; Bonilla, Carlos; Lawrence, Michael; Clum, Carey; Ameri, Ali A.; Bons, Jeffrey P.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The effect of hot streaks on deposition in a high pressure turbine vane passage was studied both experimentally and computationally. Modifications to Ohio State's Turbine Reaction Flow Rig allowed for the creation of ...
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    Experimental and Numerical Investigation of Sweeping Jet Film Cooling 

    Source: Journal of Turbomachinery:;2018:;volume 140:;issue 003:;page 31009
    Author(s): Hossain, Mohammad A.; Prenter, Robin; Lundgreen, Ryan K.; Ameri, Ali; Gregory, James W.; Bons, Jeffrey P.
    Publisher: The American Society of Mechanical Engineers (ASME)
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