The methods developed to predict the reliability of aircraft structures depend upon inspection effectiveness which, in turn, depends upon structural complexity, quality, and the percentage of the structure inspected. Reliability can be enhanced by choosing materials properly, designing damage-tolerant structures, and increasing inspection frequency. And, for fleet operations, costs can be minimized through proper inspection schedules, and enhanced reliability can be compatible with minimum cost. The methods are derived from a combination of probability theory and engineering equations. A discussion of these methods is presented
Changes in aircraft design concepts in recent years from “Safe-Life / Fail-Safe” to “Damage-Toleranc...
The 2018 Civil Engineering Research in Ireland Conference (CERI 2018), Dublin, Ireland, 29-30 August...
In evaluating the integrity of a system using fracture mechanics analysis, it is necessary to know t...
Abstract: This work presents a methodology for determining the reliability of fracture control plans...
The Federal Aviation Administration requires that transport aircraft be “damage tolerant.” That is, ...
As aircraft structures begin to age (that is, as flight hours accumulate), existing subcritical crac...
As aircraft structures begin to age (that is, as flight hours accumulate), existing subcritical crac...
The goal of this paper is to review the statistical methods used in the aerospace industries to eval...
In the present analysis, deterministic flaw growth analysis is used to project the failure distribut...
The INSIM computer program is described which simulates the 'limited fatigue life' environment in wh...
Periodic nondestructive tests are used to detect cracks on aircraft components that could be catastr...
Airline operations involving the detection of structural deterioration and associated maintenance pr...
Issued as Semi-annual report [1-4], and Final report, Project no. E-16-631Final report has title: Re...
The majority of aircraft structures are designed to be damage-tolerant such that safe operation can ...
AbstractDamage tolerant design and nondestructive inspection are key tasks for ensuring aircraft air...
Changes in aircraft design concepts in recent years from “Safe-Life / Fail-Safe” to “Damage-Toleranc...
The 2018 Civil Engineering Research in Ireland Conference (CERI 2018), Dublin, Ireland, 29-30 August...
In evaluating the integrity of a system using fracture mechanics analysis, it is necessary to know t...
Abstract: This work presents a methodology for determining the reliability of fracture control plans...
The Federal Aviation Administration requires that transport aircraft be “damage tolerant.” That is, ...
As aircraft structures begin to age (that is, as flight hours accumulate), existing subcritical crac...
As aircraft structures begin to age (that is, as flight hours accumulate), existing subcritical crac...
The goal of this paper is to review the statistical methods used in the aerospace industries to eval...
In the present analysis, deterministic flaw growth analysis is used to project the failure distribut...
The INSIM computer program is described which simulates the 'limited fatigue life' environment in wh...
Periodic nondestructive tests are used to detect cracks on aircraft components that could be catastr...
Airline operations involving the detection of structural deterioration and associated maintenance pr...
Issued as Semi-annual report [1-4], and Final report, Project no. E-16-631Final report has title: Re...
The majority of aircraft structures are designed to be damage-tolerant such that safe operation can ...
AbstractDamage tolerant design and nondestructive inspection are key tasks for ensuring aircraft air...
Changes in aircraft design concepts in recent years from “Safe-Life / Fail-Safe” to “Damage-Toleranc...
The 2018 Civil Engineering Research in Ireland Conference (CERI 2018), Dublin, Ireland, 29-30 August...
In evaluating the integrity of a system using fracture mechanics analysis, it is necessary to know t...