Accurate Stress Analysis of Variable Angle Tow Shells by High-Order Equivalent-Single-Layer and Layer-Wise Finite Element Models
New concepts of lightweight components are conceived nowadays thanks to the advances in the manufacture of composite structures. For instance, mature technologies such as Automatic Fibre Placement (AFP) are employed in the fabrication of structural parts where fibres are steered along curvilinear pa...
Guardado en:
Autores principales: | , , , |
---|---|
Formato: | article |
Lenguaje: | EN |
Publicado: |
MDPI AG
2021
|
Materias: | |
Acceso en línea: | https://doaj.org/article/4392c7ff32734566a07a54d98ca2aacc |
Etiquetas: |
Agregar Etiqueta
Sin Etiquetas, Sea el primero en etiquetar este registro!
|
id |
oai:doaj.org-article:4392c7ff32734566a07a54d98ca2aacc |
---|---|
record_format |
dspace |
spelling |
oai:doaj.org-article:4392c7ff32734566a07a54d98ca2aacc2021-11-11T18:03:41ZAccurate Stress Analysis of Variable Angle Tow Shells by High-Order Equivalent-Single-Layer and Layer-Wise Finite Element Models10.3390/ma142164861996-1944https://doaj.org/article/4392c7ff32734566a07a54d98ca2aacc2021-10-01T00:00:00Zhttps://www.mdpi.com/1996-1944/14/21/6486https://doaj.org/toc/1996-1944New concepts of lightweight components are conceived nowadays thanks to the advances in the manufacture of composite structures. For instance, mature technologies such as Automatic Fibre Placement (AFP) are employed in the fabrication of structural parts where fibres are steered along curvilinear paths, namely variable angle tow (VAT), which can enhance the mechanical performance and alleviate the structural weight. This is of utmost importance in the aerospace field, where weight savings are one of the main goals. For that reason, shell structures are commonly found in the aerospace industry because of their capabilities of supporting external loadings. Straight-fibre composite shell structures have been studied in recent decades and, now, spatially varying composite shells are attracting the attention of manufacturers. This work analyses the mechanical behaviour of VAT composite shells subjected to different external loadings and boundary conditions. The Carrera Unified Formulation (CUF) is employed to obtain the different structural models in a systematic and hierarchic manner. The outcomes of such numerical models are discussed and compared with commercial software Abaqus.Alberto Racionero Sánchez-MajanoRodolfo AzzaraAlfonso PaganiErasmo CarreraMDPI AGarticlecomposite aerospace structuresstress analysisnumerical methodsTechnologyTElectrical engineering. Electronics. Nuclear engineeringTK1-9971Engineering (General). Civil engineering (General)TA1-2040MicroscopyQH201-278.5Descriptive and experimental mechanicsQC120-168.85ENMaterials, Vol 14, Iss 6486, p 6486 (2021) |
institution |
DOAJ |
collection |
DOAJ |
language |
EN |
topic |
composite aerospace structures stress analysis numerical methods Technology T Electrical engineering. Electronics. Nuclear engineering TK1-9971 Engineering (General). Civil engineering (General) TA1-2040 Microscopy QH201-278.5 Descriptive and experimental mechanics QC120-168.85 |
spellingShingle |
composite aerospace structures stress analysis numerical methods Technology T Electrical engineering. Electronics. Nuclear engineering TK1-9971 Engineering (General). Civil engineering (General) TA1-2040 Microscopy QH201-278.5 Descriptive and experimental mechanics QC120-168.85 Alberto Racionero Sánchez-Majano Rodolfo Azzara Alfonso Pagani Erasmo Carrera Accurate Stress Analysis of Variable Angle Tow Shells by High-Order Equivalent-Single-Layer and Layer-Wise Finite Element Models |
description |
New concepts of lightweight components are conceived nowadays thanks to the advances in the manufacture of composite structures. For instance, mature technologies such as Automatic Fibre Placement (AFP) are employed in the fabrication of structural parts where fibres are steered along curvilinear paths, namely variable angle tow (VAT), which can enhance the mechanical performance and alleviate the structural weight. This is of utmost importance in the aerospace field, where weight savings are one of the main goals. For that reason, shell structures are commonly found in the aerospace industry because of their capabilities of supporting external loadings. Straight-fibre composite shell structures have been studied in recent decades and, now, spatially varying composite shells are attracting the attention of manufacturers. This work analyses the mechanical behaviour of VAT composite shells subjected to different external loadings and boundary conditions. The Carrera Unified Formulation (CUF) is employed to obtain the different structural models in a systematic and hierarchic manner. The outcomes of such numerical models are discussed and compared with commercial software Abaqus. |
format |
article |
author |
Alberto Racionero Sánchez-Majano Rodolfo Azzara Alfonso Pagani Erasmo Carrera |
author_facet |
Alberto Racionero Sánchez-Majano Rodolfo Azzara Alfonso Pagani Erasmo Carrera |
author_sort |
Alberto Racionero Sánchez-Majano |
title |
Accurate Stress Analysis of Variable Angle Tow Shells by High-Order Equivalent-Single-Layer and Layer-Wise Finite Element Models |
title_short |
Accurate Stress Analysis of Variable Angle Tow Shells by High-Order Equivalent-Single-Layer and Layer-Wise Finite Element Models |
title_full |
Accurate Stress Analysis of Variable Angle Tow Shells by High-Order Equivalent-Single-Layer and Layer-Wise Finite Element Models |
title_fullStr |
Accurate Stress Analysis of Variable Angle Tow Shells by High-Order Equivalent-Single-Layer and Layer-Wise Finite Element Models |
title_full_unstemmed |
Accurate Stress Analysis of Variable Angle Tow Shells by High-Order Equivalent-Single-Layer and Layer-Wise Finite Element Models |
title_sort |
accurate stress analysis of variable angle tow shells by high-order equivalent-single-layer and layer-wise finite element models |
publisher |
MDPI AG |
publishDate |
2021 |
url |
https://doaj.org/article/4392c7ff32734566a07a54d98ca2aacc |
work_keys_str_mv |
AT albertoracionerosanchezmajano accuratestressanalysisofvariableangletowshellsbyhighorderequivalentsinglelayerandlayerwisefiniteelementmodels AT rodolfoazzara accuratestressanalysisofvariableangletowshellsbyhighorderequivalentsinglelayerandlayerwisefiniteelementmodels AT alfonsopagani accuratestressanalysisofvariableangletowshellsbyhighorderequivalentsinglelayerandlayerwisefiniteelementmodels AT erasmocarrera accuratestressanalysisofvariableangletowshellsbyhighorderequivalentsinglelayerandlayerwisefiniteelementmodels |
_version_ |
1718431938390261760 |