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    Fan Stability With Leading Edge Damage: Blind Prediction and Validation 

    Source: Journal of Turbomachinery:;2022:;volume( 144 ):;issue: 009:;page 91015
    Author(s): Gunn, E. J.;Brandvik, T.;Wilson, M. J.;Maxwell, R.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper considers the impact of a damaged leading edge (LE) on the stall margin and stall inception mechanisms of a transonic, low-pressure ratio fan. The damage takes the form of a squared-off leading edge over the ...
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    Mid-Span Stall Inception in Low-Pressure-Ratio Transonic Fans 

    Source: Journal of Turbomachinery:;2024:;volume( 146 ):;issue: 006:;page 61010-1
    Author(s): Verschueren, H.; Hall, C. A.; Wilson, M. J.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this paper, steady and unsteady computational fluid dynamics (CFD) have been used to investigate stall inception for a modern low-pressure-ratio transonic fan. The computational results are validated against measurement ...
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    Stall Inception in Low-Pressure Ratio Fans 

    Source: Journal of Turbomachinery:;2019:;volume( 141 ):;issue: 007:;page 71005
    Author(s): Kim, S.; Pullan, G.; Hall, C. A.; Grewe, R. P.; Wilson, M. J.; Gunn, E.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A combined experimental and computational test program, with two low-pressure ratio aero-engine fans, has been used to identify the flow mechanisms at stall inception and the subsequent stall cell growth. The two fans have ...
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