Residual strength analysis using CTOA criteria for fuselage structures containing multiple site damage

Residual Strength of Aging Aircraft with Multiple Site Damage/Multiple Element Damage

A numerical study is presented of the residual strength of an aircraft fuselage in the presence of multiple site damage (MSD)/muItiple element damage. The analyses were carried out using a software package that was developed to facilitate automated analyses of full-scale fuselage panels with widespread fatigue damage, using a hierarchical approach and elastic-plastic finite element alternating ...

Residual strength prediction for aircraft panels with Multiple Site Damage, using the EPFEAM for stable crack growth analysis

190 Abstract In this paper, a new analytical method for solving stable crack propagation problems in a ductile panel with a row of cracks, is presented. The main purpose of the present study is to estimate the maximum load carrying capacity of such panels accurately. The so called Elastic Plastic Finite Element Alternating Method (Pyo et al. (1994)) was extended to account for the propagating c...

Bonded composite repair structures multiple site damage analysis

Purpose – The purpose of this work is to describe the effects of the length of cracks and the patch size on the stress intensity factors in a bonded composite repair structure containing multiple site damage. Design/methodology/approach – Finite element method was applied to simulate a bonded repair of a cracked aluminum plate with multiple site damage. A two-dimensional three-layer technique w...

Damage tolerance and residual strength of composite sandwich structures

analysis of ruin probability for insurance companies using markov chain

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