A comparative study evaluating the hybrid composite-metal aviation structure

A comparative study evaluating the hybrid composite-metal aviation structure

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 e...

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Veröffentlicht in:INCAS bulletin 2021-06, Vol.13 (2), p.3-9
Hauptverfasser: BARAN, Daniela, MARIN, Romeo, PETRE, Mihaela, BOGATEANU, Radu
Format: Artikel
Sprache:eng
Schlagworte:
Aeronautics
Aircraft
Comparative studies
composite structures
Computer simulation
Finite element analysis
finite element simulations
Hybrid composites
Laboratories
Laboratory tests
Mathematical models
Mechanical tests
Nastran
Simulation
Stress analysis
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Zusammenfassung: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.
ISSN:2066-8201
2247-4528
DOI:10.13111/2066-8201.2021.13.2.1