Paper Title:
Damage Tolerance Analysis on Repaired Fuselage Skin
  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.

  Info
Periodical
Key Engineering Materials (Volumes 306-308)
Edited by
Ichsan Setya Putra and Djoko Suharto
Pages
265-270
DOI
10.4028/www.scientific.net/KEM.306-308.265
Citation
D. Legowo, I. W. Susena, S. Tambunan, "Damage Tolerance Analysis on Repaired Fuselage Skin", Key Engineering Materials, Vols. 306-308, pp. 265-270, 2006
Online since
March 2006
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Price
$32.00
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