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    On Force Control of an Engine Order–Type Excitation Applied to a Bladed Disk With Underplatform Dampers 

    Source: Journal of Vibration and Acoustics:;2013:;volume( 135 ):;issue: 004:;page 41103
    Author(s): Firrone, Christian M.; Berruti, Teresa M.; Gola, Muzio M.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The paper presents an original multiple excitation system based on electromagnets with force control. The system is specifically designed in order to investigate the dynamics of bladed disks, since it mimics the excitation ...
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    Modeling the Microslip in the Flange Joint and Its Effect on the Dynamics of a Multistage Bladed Disk Assembly 

    Source: Journal of Computational and Nonlinear Dynamics:;2018:;volume( 013 ):;issue: 001:;page 11011
    Author(s): Firrone, Christian M.; Battiato, Giuseppe; Epureanu, Bogdan I.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The complex architecture of aircraft engines requires demanding computational efforts when the dynamic coupling of their components has to be predicted. For this reason, numerically efficient reduced-order models (ROM) ...
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    Experimental Joint Identification Using System Equivalent Model Mixing in a Bladed Disk 

    Source: Journal of Vibration and Acoustics:;2020:;volume( 142 ):;issue: 005:;page 051001-1
    Author(s): Saeed, Zeeshan; Klaassen, Steven W. B.; Firrone, Christian M.; Berruti, Teresa M.; Rixen, Daniel J.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A joint between two components can be seen as a means to transmit dynamic information from one side to the other. To identify the joint, a reverse process called decoupling can be applied. This is not as straightforward ...
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    Reduced Order Modeling for Multistage Bladed Disks With Friction Contacts at the Flange Joint 

    Source: Journal of Engineering for Gas Turbines and Power:;2018:;volume( 140 ):;issue: 005:;page 52505
    Author(s): Battiato, Giuseppe; Firrone, Christian M.; Berruti, Teresa M.; Epureanu, Bogdan I.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Most aircraft turbojet engines consist of multiple stages coupled by means of bolted flange joints which potentially represent source of nonlinearities due to friction phenomena. Methods aimed at predicting the forced ...
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