This report summarizes research dealing with analyzing the effects of widespread fatigue damage on aircraft structural integrity. Results are described for determining how cracks nucleate by corrosion, fatigue, or fretting fatigue, and once formed, grow, coalesce and lead to final fracture. The research is conducted in the context of the aging aircraft issue, which focuses on determining procedures for ensuring the continued safety of aircraft that operate beyond their original design lifetimes.


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    Titel :

    Analysis of Widespread Fatigue Damage in Aerospace Structures


    Beteiligte:
    A. F. Grandt (Autor:in) / T. N. Farris (Autor:in) / B. H. Hillberry (Autor:in)

    Erscheinungsdatum :

    1999


    Format / Umfang :

    158 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Widespread Fatigue Damage Assessment of Jet Transport Structures

    Gruber, M. L. / Johnson, B. E. / Whittaker, I. C. et al. | British Library Conference Proceedings | 2002


    Statistical Property of Widespread Fatigue Damage

    Shinozuka, M. / Deodatis, G. / Sampath, S. G. et al. | British Library Conference Proceedings | 1995


    Widespread Fatigue Damage in Combat Aircraft

    Ansell, H. / Johansson, T. / Advisory Group for Aerospace Research and Development et al. | British Library Conference Proceedings | 1995


    Analysis of Widespread Fatigue Damage in Lap Joints

    Grandt, A. F. / Wang, H. L. / SAE | British Library Conference Proceedings | 1999


    Analysis of Widespread Fatigue Damage in Lap Joints

    Grandt, A. F. / Wang, H. L. | SAE Technical Papers | 1999