Damage Tolerance Analysis on Repaired Fuselage Skin |
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| Journal | Key Engineering Materials (Volumes 306 - 308) |
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| Volume | Fracture and Strength of Solids VI |
| Edited by | Ichsan Setya Putra and Djoko Suharto |
| Pages | 265-270 |
| DOI | 10.4028/www.scientific.net/KEM.306-308.265 |
| Citation | Dibyo Legowo et al., 2006, Key Engineering Materials, 306-308, 265 |
| Online since | March, 2006 |
| Authors | Dibyo Legowo, I Wayan Susena, Sharudin Tambunan |
| Keywords | Damage Tolerance, Fuselage Skin, Repair |
| Abstract | This paper discussed about the method used by operator to perform damage tolerance analysis for repaired fuselage skin. Skin damage may be caused by accidental damage or fatigue crack. Some element needed for damage tolerance analysis and the method to develop load spectrum will be discussed briefly. Therefore, this paper will describe a case study of damage tolerance analysis on repaired fuselage skin of narrow body jet aircraft. |
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