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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Faculty of Mechanical Engineering Universiti Teknologi MARA (UiTM),
2014.
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