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    Coal Ash Deposition on Nozzle Guide Vanes—Part II: Computational Modeling 

    Source: Journal of Turbomachinery:;2013:;volume( 135 ):;issue: 001:;page 11015
    Author(s): Barker, B.; Casaday, B.; Shankara, P.; Ameri, A.; Bons, J. P.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Coal ash deposition was numerically modeled on a GEE3 high pressure turbine vane passage. A model was developed, in conjunction with FLUENTâ„¢ software, to track individual particles through the turbine passage. Two sticking ...
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    Coal Ash Deposition on Nozzle Guide Vanes—Part I: Experimental Characteristics of Four Coal Ash Types 

    Source: Journal of Turbomachinery:;2013:;volume( 135 ):;issue: 002:;page 21033
    Author(s): Webb, J.; Casaday, B.; Barker, B.; Bons, J. P.; Gledhill, A. D.; Padture, N. P.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An accelerated deposition test facility was operated with four different coal ash species to study the effect of ash composition on deposition rate and spatial distribution. The facility seeds a combusting (natural gas) ...
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    Aerothermal Optimization of Turbine Squealer Tip Geometries With Arbitrary Cooling Injection 

    Source: Journal of Turbomachinery:;2021:;volume( 143 ):;issue: 011:;page 0111010-1
    Author(s): De Maesschalck, C.; Andreoli, V.; Paniagua, G.; Gillen, T.; Barker, B.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The optimization of the turbine rotor tip geometry remains a vital opportunity to create more efficient and durable engines. Balancing the aerodynamic and thermal aspects, while maintaining the mechanical integrity, is key ...
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