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    Effect of the Aero-Engine Mounting Stiffness on the Whole Engine Coupling Vibration 

    Source: Journal of Engineering for Gas Turbines and Power:;2018:;volume( 140 ):;issue: 007:;page 72501
    Author(s): Qu, M. J.; Chen, G.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A finite element (FE) model of the rotor tester of an aero-engine, having a thin-walled casing structure, mounted with the way of an actual engine, is developed to simulate the intrinsic vibration characteristics under ...
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