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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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:
composite structures
mechanical tests
finite element simulations
Online Access:https://bulletin.incas.ro/files/baran_marin_petre_bogateanu__vol_13_iss_2.pdf
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spelling doaj-8e4a0119354f4276b3667b379ec23de52021-06-06T15:19:11ZengNational Institute for Aerospace Research “Elie Carafoli” - INCASINCAS Bulletin2066-82012247-45282021-06-011323910.13111/2066-8201.2021.13.2.1A comparative study evaluating the hybrid composite-metal aviation structureDaniela BARAN0Romeo MARIN1Mihaela PETRE2Radu BOGATEANU3AEROSPACE Consulting, B-dul Iuliu Maniu 220, Bucharest 061126, Romania, baran.daniela@incas.roINCAS – National Institute for Aerospace Research “Elie Carafoli”, B-dul Iuliu Maniu 220, Bucharest 061126, Romania, marin.romeo@incas.roAEROSPACE Consulting, B-dul Iuliu Maniu 220, Bucharest 061126, Romania, petre.mihaela@incas.roINCAS – National Institute for Aerospace Research “Elie Carafoli”, B-dul Iuliu Maniu 220, Bucharest 061126, Romania, bogateanu.radu@incas.roThe 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.https://bulletin.incas.ro/files/baran_marin_petre_bogateanu__vol_13_iss_2.pdfcomposite structuresmechanical testsfinite element simulations
collection DOAJ
language English
format Article
sources DOAJ
author Daniela BARAN
Romeo MARIN
Mihaela PETRE
Radu BOGATEANU
spellingShingle Daniela BARAN
Romeo MARIN
Mihaela PETRE
Radu BOGATEANU
A comparative study evaluating the hybrid composite-metal aviation structure
INCAS Bulletin
composite structures
mechanical tests
finite element simulations
author_facet Daniela BARAN
Romeo MARIN
Mihaela PETRE
Radu BOGATEANU
author_sort Daniela BARAN
title A comparative study evaluating the hybrid composite-metal aviation structure
title_short A comparative study evaluating the hybrid composite-metal aviation structure
title_full A comparative study evaluating the hybrid composite-metal aviation structure
title_fullStr A comparative study evaluating the hybrid composite-metal aviation structure
title_full_unstemmed A comparative study evaluating the hybrid composite-metal aviation structure
title_sort comparative study evaluating the hybrid composite-metal aviation structure
publisher National Institute for Aerospace Research “Elie Carafoli” - INCAS
series INCAS Bulletin
issn 2066-8201
2247-4528
publishDate 2021-06-01
description 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.
topic composite structures
mechanical tests
finite element simulations
url https://bulletin.incas.ro/files/baran_marin_petre_bogateanu__vol_13_iss_2.pdf
work_keys_str_mv AT danielabaran acomparativestudyevaluatingthehybridcompositemetalaviationstructure
AT romeomarin acomparativestudyevaluatingthehybridcompositemetalaviationstructure
AT mihaelapetre acomparativestudyevaluatingthehybridcompositemetalaviationstructure
AT radubogateanu acomparativestudyevaluatingthehybridcompositemetalaviationstructure
AT danielabaran comparativestudyevaluatingthehybridcompositemetalaviationstructure
AT romeomarin comparativestudyevaluatingthehybridcompositemetalaviationstructure
AT mihaelapetre comparativestudyevaluatingthehybridcompositemetalaviationstructure
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