In this paper the finite element analysis of the composite supporting structure of an aircraft triple seat model is presented. For the involved composite structural elements a linearly elastic constitutive behaviour is assumed and the micromechanical properties are reduced to those ones of an equivalent homogeneous non isotropic material through homogenization techniques. The numerical results, concerning both static and dynamic analyses, are obtained by the commercial code Ansys.
Dell'Amore Fachinetti, S., Vairo, G. (2004). Analisi agli elementi finiti della struttura primaria in materiale composito di una poltrona tripla per aereo (in Italian) - Finite element anlysis of the main structure in composite material of an aircraft triple seat. In Atti del XXXIII Convegno nazionale associazione italiana per l'analisi delle sollecitazioni (AIAS 2004). Bari.
Analisi agli elementi finiti della struttura primaria in materiale composito di una poltrona tripla per aereo (in Italian) - Finite element anlysis of the main structure in composite material of an aircraft triple seat
VAIRO, GIUSEPPE
2004-09-01
Abstract
In this paper the finite element analysis of the composite supporting structure of an aircraft triple seat model is presented. For the involved composite structural elements a linearly elastic constitutive behaviour is assumed and the micromechanical properties are reduced to those ones of an equivalent homogeneous non isotropic material through homogenization techniques. The numerical results, concerning both static and dynamic analyses, are obtained by the commercial code Ansys.I documenti in IRIS sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.
