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    Influence of Gap Detailing on Calculated Unsteady Non-Adjacent Blade Row Aero-Forcing in a Transonic Compressor Stage 

    Source: Journal of Turbomachinery:;2020:;volume( 142 ):;issue: 011:;page 0111010-1
    Author(s): Gezork, Tobias; Petrie-Repar, Paul
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Resonant or close to resonant forced response excitation of compressor blades limits component life time and can potentially lead to high-cycle fatigue failure if the exciting forces are large and damping is insufficient. ...
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