The progress achieved in the understanding and modelling of fatigue and fracture in aircraft structures has led to the development of Damage Tolerance as the framework for ensuring continued airworthiness. Success of Damage Tolerance and Fail-Safe concepts combined with general economic conditions led to the current situation where an increasing number of aircraft are operated beyond their original design goal.
Life and Damage Monitoring-Using NDI Data Interpretation for Corrosion Damage and Remaining Life Assessments
2003
14 pages
Report
No indication
English
Remaining useful life estimation under degradation and shock damage
Online Contents | 2015
|Problem of relating accumulated service fatigue damage to remaining life
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|THE PROBLEM OF RELATING ACCUMULATED SERVICE FATIGUE DAMAGE TO REMAINING LIFE
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British Library Conference Proceedings | 1998
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