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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    Title :

    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)


    Contributors:

    Publication date :

    1995


    Size :

    72 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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