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    Stall Inception in a Boundary Layer Ingesting Fan 

    Source: Journal of Turbomachinery:;2019:;volume 141:;issue 009:;page 91007
    Author(s): Perovic, D.; Hall, C. A.; Gunn, E. J.
    Publisher: American Society of Mechanical Engineers (ASME)
    Abstract: Jet engines with boundary layer ingestion (BLI) could offer significant reductions in aircraft fuel burn compared with podded turbofans. However, the engine fans must run continuously with severe inlet distortion, which ...
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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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