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...
Main Authors: | , , , |
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Format: | Article |
Language: | English |
Published: |
National Institute for Aerospace Research “Elie Carafoli” - INCAS
2021-06-01
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Series: | INCAS Bulletin |
Subjects: | |
Online Access: | https://bulletin.incas.ro/files/baran_marin_petre_bogateanu__vol_13_iss_2.pdf |