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.


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    Title :

    Life and Damage Monitoring-Using NDI Data Interpretation for Corrosion Damage and Remaining Life Assessments


    Contributors:

    Publication date :

    2003


    Size :

    14 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English








    Nondestructive Characterization of Pitting Corrosion Damage and Fatigue Life

    Rokhlin, S. I. / Zoofan, B. / Kim, J.-Y. et al. | British Library Conference Proceedings | 1998