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    Experimental Study of Impact of In-Service Deterioration on Aerodynamic Performance of High-Pressure Nozzle Guide Vanes 

    Source: Journal of Turbomachinery:;2023:;volume( 145 ):;issue: 006:;page 61017-1
    Author(s): Michaud, Mathias; Jackson, Dougal; Goenaga, Frédéric; Povey, Thomas
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this paper we experimentally evaluate the impact of in-service deterioration on the aerodynamic performance of heavily film-cooled high-pressure nozzle guide vanes from large civil jet engines. We study 15 mid-life to ...
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    Secondary Flow Control in Low Aspect Ratio Vanes Using Splitters 

    Source: Journal of Turbomachinery:;2017:;volume( 139 ):;issue: 009:;page 91003
    Author(s): Clark, Christopher J.; Pullan, Graham; Curtis, Eric; Goenaga, Frederic
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Low aspect ratio vanes, often the result of overall engine architecture constraints, create strong secondary flows and high end-wall loss. In this paper, a splitter concept is demonstrated that reduces secondary flow ...
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    Understanding Capacity Sensitivity of Cooled Transonic Nozzle Guide Vanes: A Parametric Experimental and Computational Study of the Impact of Trailing Edge Geometry 

    Source: Journal of Turbomachinery:;2021:;volume( 143 ):;issue: 005:;page 051001-1
    Author(s): Burdett, Daniel; Goenaga, Frédéric; Povey, Thomas
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: High-pressure (HP) nozzle guide vane (NGV) capacity is one of the most important parameters for setting overall turbine power output, for stage matching, and for understanding turbine performance. Accurate capacity prediction ...
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