33th Congress of the International Council of the Aeronautical Sciences

04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity

VIBRO-ACOUSTIC ANALYSIS OF MULTI-LAYER CYLINDRICAL SHELL-CAVITY SYSTEMS VIA CUF FINITE ELEMENTS

M.C. Moruzzi¹, M. Cinefra, Poliecnico di Bari, Italy; S. Bagassi¹, E. Zappino, Politecnico di Torino, Italy; ¹Università di Bologna, Italy

The noise footprint of a commercial passenger aircraft depends on several parameters. The sound travels through vibrations, which are displacements in a rigid body. These variables are described by the structural models depending on the structures itself and on other parameters. In this paper we apply an innovative shell model, based on Carrera's Unified Formulation, on a cylindrical structure.


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