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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Bibliographic Details
Main Authors: Daniela BARAN, Romeo MARIN, Mihaela PETRE, Radu BOGATEANU
Format: Article
Language:English
Published: National Institute for Aerospace Research “Elie Carafoli” - INCAS 2021-06-01
Series:INCAS Bulletin
Subjects:
Online Access:https://bulletin.incas.ro/files/baran_marin_petre_bogateanu__vol_13_iss_2.pdf

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