The application of reliability analysis methods to the estimation of probable aircraft structural fatigue performance was investigated. Use was made of order statistics to establish the means of assessing the fatigue performance reliability of a fleet or number of fatigue-exposed details. A reliability analysis plan for application to aluminum alloy structural fatigue performance was developed and compared with the current fixed-scatter-factor procedure for determining the safe life of a structural detail. (Author)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Reliability Analysis Approach to Fatigue Life Variability of Aircraft Structures


    Beteiligte:
    I. C. Whittaker (Autor:in) / P. M. Besuner (Autor:in)

    Erscheinungsdatum :

    1969


    Format / Umfang :

    262 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Aircraft structures reliability under corrosion fatigue

    Shi, Pan / Mahadevan, Sankaran | AIAA | 2001



    Corrosion Fatigue Life Prediction of Aircraft Structure Based on Fuzzy Reliability Approach

    Tan, X.-m. / Chen, Y.-l. / Jin, P. | British Library Online Contents | 2005


    AIAA-2001-1377 Aircraft Structures Reliability under Corrosion Fatigue

    Shi, P. / Mahadevan, S. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2001