Open AccessA comparative study evaluating the hybrid composite-metal aviation structure
Author(s) -
Daniela Baran,
Romeo Marin,
PETRE Mihaela,
Radu Bogateanu
Publication year - 2021
Publication title -
incas buletin
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.282
H-Index - 10
eISSN - 2247-4528
pISSN - 2066-8201
DOI - 10.13111/2066-8201.2021.13.2.1
Subject(s) - finite element method , composite number , structural engineering , aviation , engineering , computer simulation , computer science , mechanical engineering , aerospace engineering , simulation , algorithm
The main purpose of this paper is to develop some numerical experiences based on mechanical tests performed on a hybrid composite metal aeronautical structure using finite element commercial codes (here NASTRAN). The results of the numerical simulations are consistent with the laboratory tests and encourage us to continue to improve the models using NASTRAN capabilities to obtain a realistic simulation of aeronautical structures made of such composites, taking into account their special properties.