The Effects of Ply Orientation on Nonlinear Buckling of Aircraft composite Stiffened Panel
In this paper, gradual demand for curved, stiffened panels composite emerged from carbon fiber reinforced plastics (CFRP); these are structures that are frequently used in aerospace engineering. Up to 50% of the primary structure of the Boeing 787 is made up of woven graphite–epoxy. This research em...
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| Language: | English |
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Gruppo Italiano Frattura
2019-08-01
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| Series: | Fracture and Structural Integrity |
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| Online Access: | https://www.fracturae.com/index.php/fis/article/view/2548 |
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| author | Ouadia Mouhat Abdelmajid Bybi Ahmed El Bouhmidi Mohamed Rougui |
| author_facet | Ouadia Mouhat Abdelmajid Bybi Ahmed El Bouhmidi Mohamed Rougui |
| author_sort | Ouadia Mouhat |
| collection | DOAJ |
| description | In this paper, gradual demand for curved, stiffened panels composite emerged from carbon fiber reinforced plastics (CFRP); these are structures that are frequently used in aerospace engineering. Up to 50% of the primary structure of the Boeing 787 is made up of woven graphite–epoxy. This research emphasizes the buckling analysis of stiffened composite panels using the nonlinear, finite element modeling. The stiffened panel is assumed to be subjected to a uniform axial compression load of . For the nonlinear buckling analysis, a stiffened composite panel is made of carbon fibre composite (CFC) in epoxy, Kevlar in epoxy and E-glass (EG) in epoxy. Due to the fact that there are numerous stiffened composite panels materials, this paper, therefore uses a numerical approach, to present the study and results of the nonlinear static buckling analysis of I-stiffened, on different composite panels. This research also presented the effect of the different ply orientations using Abaqus finite element analysis (FEA). |
| format | Article |
| id | doaj-art-3dd40cf791e547a984d340ccca3963cc |
| institution | Kabale University |
| issn | 1971-8993 |
| language | English |
| publishDate | 2019-08-01 |
| publisher | Gruppo Italiano Frattura |
| record_format | Article |
| series | Fracture and Structural Integrity |
| spelling | doaj-art-3dd40cf791e547a984d340ccca3963cc2025-01-03T00:39:47ZengGruppo Italiano FratturaFracture and Structural Integrity1971-89932019-08-011350The Effects of Ply Orientation on Nonlinear Buckling of Aircraft composite Stiffened PanelOuadia Mouhat0Abdelmajid Bybi1Ahmed El Bouhmidi2Mohamed Rougui3Mohammed V University, Structure LGCE l’EST, Salé -CED de l’EMI, Rabat, MoroccoMohammed V University in Rabat, EST Sale - Morocco MEAT - Materials Energy Acoustics Team-CED of Mohammadia Engineering School, Rabat.Mohammed V University, Structure LGCE, EST Sale -CED of Mohammadia Engineering School, Rabat, Morocco.Mohammed V University, Structure LGCE, EST Sale -CED of Mohammadia Engineering School, Rabat, Morocco.In this paper, gradual demand for curved, stiffened panels composite emerged from carbon fiber reinforced plastics (CFRP); these are structures that are frequently used in aerospace engineering. Up to 50% of the primary structure of the Boeing 787 is made up of woven graphite–epoxy. This research emphasizes the buckling analysis of stiffened composite panels using the nonlinear, finite element modeling. The stiffened panel is assumed to be subjected to a uniform axial compression load of . For the nonlinear buckling analysis, a stiffened composite panel is made of carbon fibre composite (CFC) in epoxy, Kevlar in epoxy and E-glass (EG) in epoxy. Due to the fact that there are numerous stiffened composite panels materials, this paper, therefore uses a numerical approach, to present the study and results of the nonlinear static buckling analysis of I-stiffened, on different composite panels. This research also presented the effect of the different ply orientations using Abaqus finite element analysis (FEA).https://www.fracturae.com/index.php/fis/article/view/2548Stiffened composite panelsNonlinear buckling analysisFEM ply orientations |
| spellingShingle | Ouadia Mouhat Abdelmajid Bybi Ahmed El Bouhmidi Mohamed Rougui The Effects of Ply Orientation on Nonlinear Buckling of Aircraft composite Stiffened Panel Fracture and Structural Integrity Stiffened composite panels Nonlinear buckling analysis FEM ply orientations |
| title | The Effects of Ply Orientation on Nonlinear Buckling of Aircraft composite Stiffened Panel |
| title_full | The Effects of Ply Orientation on Nonlinear Buckling of Aircraft composite Stiffened Panel |
| title_fullStr | The Effects of Ply Orientation on Nonlinear Buckling of Aircraft composite Stiffened Panel |
| title_full_unstemmed | The Effects of Ply Orientation on Nonlinear Buckling of Aircraft composite Stiffened Panel |
| title_short | The Effects of Ply Orientation on Nonlinear Buckling of Aircraft composite Stiffened Panel |
| title_sort | effects of ply orientation on nonlinear buckling of aircraft composite stiffened panel |
| topic | Stiffened composite panels Nonlinear buckling analysis FEM ply orientations |
| url | https://www.fracturae.com/index.php/fis/article/view/2548 |
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