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    Comparison of Eddy Viscosity Models for High Turbulence Nozzle Guide Vane Flows 

    Source: Journal of Turbomachinery:;2024:;volume( 146 ):;issue: 008:;page 81004-1
    Author(s): Amend, Jonas; Povey, Thomas
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this paper we investigate the performance of eddy viscosity turbulence models for high-pressure nozzle guide vane (NGV) flows with engine-realistic turbulence. Using metrics such as integrated kinetic energy (KE) loss ...
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    Impact of Lean-Burn Combustor Flow on Nozzle Guide Vane Performance 

    Source: Journal of Turbomachinery:;2024:;volume( 147 ):;issue: 001:;page 11001-1
    Author(s): Amend, Jonas; Chowdhury, Nafiz; Povey, Thomas
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this paper we investigate the impact of lean-burn-representative swirl and temperature distortion on the aerothermal performance of fully-cooled high-pressure nozzle guide vanes (NGVs) from a modern aero-engine. Experiments ...
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    Aerodynamic and Thermal Field Development of Cooled Transonic HP NGV 

    Source: Journal of Turbomachinery:;2023:;volume( 146 ):;issue: 002:;page 21010-1
    Author(s): Amend, Jonas; Lubbock, Roderick; Ornano, Francesco; Chowdhury, Nafiz; Povey, Thomas
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this study we present detailed aerodynamic and thermal field measurements downstream of an annular cascade of fully-cooled nozzle guide vanes (NGVs). The experiments were conducted in the Engine Component Aerothermal ...
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    Lean-Burn Combustor Simulator for an Engine-Component Test Facility: An Experimental and Computational Study 

    Source: Journal of Turbomachinery:;2023:;volume( 145 ):;issue: 006:;page 61014-1
    Author(s): Amend, Jonas; Lubbock, Roderick; Ornano, Francesco; Povey, Thomas
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The computational and experimental assessment of a lean-burn low-NOx combustor simulator for an engine component test facility is presented. The Engine Component Aero-Thermal (ECAT) facility is a full-scale engine-parts ...
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