Damage Tolerance Analysis on Repaired Fuselage Skin

Tambunan, Sharudin; Legowo, Dibyo; Susena, I Wayan

Paper Titles

Detection Probability Improvement for Nondestructive Evaluation Using a Magnetic Camera, p.241
Detection of Surface Flaw in a Homogeneous Ceramic Product by Resonant Ultrasound, p.247
Damage Detection of a Circular Cylindrical Shell with Frequency Sensitivities, p.253
Model of Behavior of Materials with Delaminations under Hydrogen Embrittlement Conditions, p.259
Damage Tolerance Analysis on Repaired Fuselage Skin, p.265
Acoustic Emission as a Tool of Fatigue Assessment, p.271
Impact Damage and Strength Reduction Behavior of Honeycomb Sandwich Structure Subjected to Low Velocity Impact, p.279
A Damage Analysis on the Composite Plate Subjected to Low Velocity Impact, p.285
Penetration Fracture Characteristics of CFRP Curved Shells According to Oblique Impact, p.291

Home > Key Engineering Materials > Fracture and Strength of Solids VI > Damage Tolerance Analysis on Repaired Fuselage...

Paper Title:

Damage Tolerance Analysis on Repaired Fuselage Skin

Periodical	Key Engineering Materials (Volumes 306 - 308)
Main Theme	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
Price	US$ 28,-

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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.