Consideration of lamination structural analysis in a multi-layered composite and failure analysis on wing design application
A finite element (FE) model is developed to study the structural performance on a composite wing of a UAV with a tubercle design at the leading edge of the wing. The experimental study of the designation of the composite at the wing skin is carried out to prove the simulation validity through materi...
| Main Authors: | , , , |
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| Format: | Article |
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Multidisciplinary Digital Publishing Institute
2021
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| Online Access: | http://psasir.upm.edu.my/id/eprint/96513/ |
| _version_ | 1848862383884206080 |
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| author | Basri, Ernnie Illyani Hameed Sultan, Mohamed Thariq Basri, Adi Azriff Mustapha, Faizal |
| author_facet | Basri, Ernnie Illyani Hameed Sultan, Mohamed Thariq Basri, Adi Azriff Mustapha, Faizal |
| author_sort | Basri, Ernnie Illyani |
| building | UPM Institutional Repository |
| collection | Online Access |
| description | A finite element (FE) model is developed to study the structural performance on a composite wing of a UAV with a tubercle design at the leading edge of the wing. The experimental study of the designation of the composite at the wing skin is carried out to prove the simulation validity through material characteristics. In this paper, the numerical modeling for simulation is highlighted to correlate the process parameter setting of simulation replicating the actual experimental tests. The percentage difference was calculated to be 11.1% by tensile and 10.47% by flexural. The numerical work applied the study of FE analysis and developed a standardized numerical approach for structural optimization, known as FE-ACP simulation. The significant findings of deformation are obtained according to Schrenk's aerodynamic loading, while the prediction of failure mode of Tsai-Wu under interaction among stresses and strains was acquired at the seventh and eighth layer of both spars. |
| first_indexed | 2025-11-15T13:16:10Z |
| format | Article |
| id | upm-96513 |
| institution | Universiti Putra Malaysia |
| institution_category | Local University |
| last_indexed | 2025-11-15T13:16:10Z |
| publishDate | 2021 |
| publisher | Multidisciplinary Digital Publishing Institute |
| recordtype | eprints |
| repository_type | Digital Repository |
| spelling | upm-965132023-01-11T08:58:38Z http://psasir.upm.edu.my/id/eprint/96513/ Consideration of lamination structural analysis in a multi-layered composite and failure analysis on wing design application Basri, Ernnie Illyani Hameed Sultan, Mohamed Thariq Basri, Adi Azriff Mustapha, Faizal A finite element (FE) model is developed to study the structural performance on a composite wing of a UAV with a tubercle design at the leading edge of the wing. The experimental study of the designation of the composite at the wing skin is carried out to prove the simulation validity through material characteristics. In this paper, the numerical modeling for simulation is highlighted to correlate the process parameter setting of simulation replicating the actual experimental tests. The percentage difference was calculated to be 11.1% by tensile and 10.47% by flexural. The numerical work applied the study of FE analysis and developed a standardized numerical approach for structural optimization, known as FE-ACP simulation. The significant findings of deformation are obtained according to Schrenk's aerodynamic loading, while the prediction of failure mode of Tsai-Wu under interaction among stresses and strains was acquired at the seventh and eighth layer of both spars. Multidisciplinary Digital Publishing Institute 2021 Article PeerReviewed Basri, Ernnie Illyani and Hameed Sultan, Mohamed Thariq and Basri, Adi Azriff and Mustapha, Faizal (2021) Consideration of lamination structural analysis in a multi-layered composite and failure analysis on wing design application. Materials, 14 (13). art. no. 3705. pp. 1-10. ISSN 1996-1944 https://www.mdpi.com/1996-1944/14/13/3705 10.3390/ma14133705 |
| spellingShingle | Basri, Ernnie Illyani Hameed Sultan, Mohamed Thariq Basri, Adi Azriff Mustapha, Faizal Consideration of lamination structural analysis in a multi-layered composite and failure analysis on wing design application |
| title | Consideration of lamination structural analysis in a multi-layered composite and failure analysis on wing design application |
| title_full | Consideration of lamination structural analysis in a multi-layered composite and failure analysis on wing design application |
| title_fullStr | Consideration of lamination structural analysis in a multi-layered composite and failure analysis on wing design application |
| title_full_unstemmed | Consideration of lamination structural analysis in a multi-layered composite and failure analysis on wing design application |
| title_short | Consideration of lamination structural analysis in a multi-layered composite and failure analysis on wing design application |
| title_sort | consideration of lamination structural analysis in a multi-layered composite and failure analysis on wing design application |
| url | http://psasir.upm.edu.my/id/eprint/96513/ http://psasir.upm.edu.my/id/eprint/96513/ http://psasir.upm.edu.my/id/eprint/96513/ |