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    Free Vibration Response of Thin and Thick Nonhomogeneous Shells by Refined One Dimensional Analysis 

    Source: Journal of Vibration and Acoustics:;2014:;volume( 136 ):;issue: 006:;page 61001
    Author(s): Varello, Alberto; Carrera, Erasmo
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The free vibration analysis of thinand thickwalled layered structures via a refined onedimensional (1D) approach is addressed in this paper. Carrera unified formulation (CUF) is employed to introduce higherorder 1D models ...
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    Layerwise Analyses of Compact and Thin Walled Beams Made of Viscoelastic Materials 

    Source: Journal of Vibration and Acoustics:;2016:;volume( 138 ):;issue: 006:;page 64501
    Author(s): Filippi, Matteo; Carrera, Erasmo; Regalli, Andrea M.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper evaluates the vibration characteristics of structures with viscoelastic materials. The mechanical properties of viscoelastic layers have been described with the complex modulus approach. The equations of motion ...
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    A Node-Dependent Kinematic Approach for Rotordynamics Problems 

    Source: Journal of Engineering for Gas Turbines and Power:;2019:;volume( 141 ):;issue: 006:;page 62501
    Author(s): Filippi, Matteo; Zappino, Enrico; Carrera, Erasmo
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents the dynamic analysis of rotating structures using node-dependent kinematics (NDK) one-dimensional (1D) elements. These elements have the capabilities to assume a different kinematic at each node of a ...
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    A Method of Panel Flutter Suppression and Elimination for Aeroelastic Structures in Supersonic Airflow 

    Source: Journal of Vibration and Acoustics:;2018:;volume( 140 ):;issue: 006:;page 64501
    Author(s): Song, Zhi-Guang; Yang, Tian-Zhi; Li, Feng-Ming; Carrera, Erasmo; Hagedorn, Peter
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In traditional active flutter control, piezoelectric materials are used to increase the stiffness of the aeroelastic structure by providing an active stiffness, and usually the active stiffness matrix is symmetric. That ...
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