Identification of the maximum stress value that occur at The wing-fuselage joints at 1-G symmetrical level flight condition / Abdul Jalil A.M.H. … [et al.]
This paper described the identification of the maximum value of stress that acts at the wing-fuselage joints. The finite element models of the wing, the wing lugs and the fuselage lugs were developed. Finite Element Analyses were performed using NASTRAN finite element software. CQUAD4 and BAR2 eleme...
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| Format: | Article |
| Language: | English |
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Faculty of Mechanical Engineering Universiti Teknologi MARA (UiTM)
2014
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| Online Access: | https://ir.uitm.edu.my/id/eprint/17644/ |
| _version_ | 1848804322044805120 |
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| author | Abdul Jalil A.M.H |
| author_facet | Abdul Jalil A.M.H |
| author_sort | Abdul Jalil A.M.H |
| building | UiTM Institutional Repository |
| collection | Online Access |
| description | This paper described the identification of the maximum value of stress that acts at the wing-fuselage joints. The finite element models of the wing, the wing lugs and the fuselage lugs were developed. Finite Element Analyses were performed using NASTRAN finite element software. CQUAD4 and BAR2 elements were used to represent the individual structures of the wing such as the ribs and stringers are presented in detail in this paper. The applied load was based on 1-g symmetric level flight condition that was the load applied at the wing is equal to the net weight of the aircraft. Once the load distribution acting at the wing have been calculated and applied, reaction forces at the nodes representing the wing lugs are obtained and these values are applied to the lug models where the maximum stress value acting at the lugs was obtained. This stress value can be further used for fatigue calculations. |
| first_indexed | 2025-11-14T21:53:17Z |
| format | Article |
| id | uitm-17644 |
| institution | Universiti Teknologi MARA |
| institution_category | Local University |
| language | English |
| last_indexed | 2025-11-14T21:53:17Z |
| publishDate | 2014 |
| publisher | Faculty of Mechanical Engineering Universiti Teknologi MARA (UiTM) |
| recordtype | eprints |
| repository_type | Digital Repository |
| spelling | uitm-176442019-08-22T03:35:14Z https://ir.uitm.edu.my/id/eprint/17644/ Identification of the maximum stress value that occur at The wing-fuselage joints at 1-G symmetrical level flight condition / Abdul Jalil A.M.H. … [et al.] jmeche Abdul Jalil A.M.H This paper described the identification of the maximum value of stress that acts at the wing-fuselage joints. The finite element models of the wing, the wing lugs and the fuselage lugs were developed. Finite Element Analyses were performed using NASTRAN finite element software. CQUAD4 and BAR2 elements were used to represent the individual structures of the wing such as the ribs and stringers are presented in detail in this paper. The applied load was based on 1-g symmetric level flight condition that was the load applied at the wing is equal to the net weight of the aircraft. Once the load distribution acting at the wing have been calculated and applied, reaction forces at the nodes representing the wing lugs are obtained and these values are applied to the lug models where the maximum stress value acting at the lugs was obtained. This stress value can be further used for fatigue calculations. Faculty of Mechanical Engineering Universiti Teknologi MARA (UiTM) 2014 Article PeerReviewed text en https://ir.uitm.edu.my/id/eprint/17644/2/AJ_ABDUL%20JALIL%2C%20A.M.H.%20JME%2014.pdf Abdul Jalil A.M.H (2014) Identification of the maximum stress value that occur at The wing-fuselage joints at 1-G symmetrical level flight condition / Abdul Jalil A.M.H. … [et al.]. (2014) Journal of Mechanical Engineering (JMechE) <https://ir.uitm.edu.my/view/publication/Journal_of_Mechanical_Engineering_=28JMechE=29.html>, 11 (2). pp. 79-91. ISSN 1823-5514 ; 2550-164X https://jmeche.uitm.edu.my/ |
| spellingShingle | Abdul Jalil A.M.H Identification of the maximum stress value that occur at The wing-fuselage joints at 1-G symmetrical level flight condition / Abdul Jalil A.M.H. … [et al.] |
| title | Identification of the maximum stress value that occur at The wing-fuselage joints at 1-G symmetrical level flight condition / Abdul Jalil A.M.H. … [et al.] |
| title_full | Identification of the maximum stress value that occur at The wing-fuselage joints at 1-G symmetrical level flight condition / Abdul Jalil A.M.H. … [et al.] |
| title_fullStr | Identification of the maximum stress value that occur at The wing-fuselage joints at 1-G symmetrical level flight condition / Abdul Jalil A.M.H. … [et al.] |
| title_full_unstemmed | Identification of the maximum stress value that occur at The wing-fuselage joints at 1-G symmetrical level flight condition / Abdul Jalil A.M.H. … [et al.] |
| title_short | Identification of the maximum stress value that occur at The wing-fuselage joints at 1-G symmetrical level flight condition / Abdul Jalil A.M.H. … [et al.] |
| title_sort | identification of the maximum stress value that occur at the wing-fuselage joints at 1-g symmetrical level flight condition / abdul jalil a.m.h. … [et al.] |
| url | https://ir.uitm.edu.my/id/eprint/17644/ https://ir.uitm.edu.my/id/eprint/17644/ |