This document focuses on the fatigue behavoir of reduced-scale barrels, curved panels and flat panels. Two types of skin material, GLARE 3 3/2-0.3 and 2024-T3 clad, are investigated. The significant of coupon tests for the fatigue behavior of a riveted lap joint in a fuselage is evaluated. Special attention is paid to the behavior of reduced-scale barrel specimens in comparison to flat specimens. Differences between flat coupons and fuselages are discussed based on calculations and experiments.


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    Titel :

    Fatigue Strength of Riveted Lap Joints in GLARE 3 3/2-0.3 Reduced-Scale Barrel, Curved Panel and Flat Panel Design (BE2040 Subtask 6.1)


    Beteiligte:
    R. P. G. Mueller (Autor:in) / E. Holleman (Autor:in)

    Erscheinungsdatum :

    1995


    Format / Umfang :

    72 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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    Corrosion Fatigue of Aluminum and GLARE Riveted Lap Joints

    Mueller, R. P. G. / Roebroeks, G. / Bridge, J. W. et al. | British Library Conference Proceedings | 1995


    Corrosion fatigue of aluminum and GLARE riveted lap joints

    Müller, R.P.G. / Roebrooks, G. / Bridge, J.W. | Tema Archiv | 1995


    Corrosion Fatigue of Aluminum and GLARE Riveted Lap Joints

    Mueller, R. P. G. / Roebroeks, G. / Bridge, J. W. | British Library Online Contents | 1995


    The Fatigue Strength of Riveted Joints

    Smith, C.R. | Emerald Group Publishing | 1957