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.
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)
1995
72 pages
Report
Keine Angabe
Englisch
Composite Materials , Materials Degradation & Fouling , Engineering Materials , Aircraft , Glass fiber reinforced plastics , Fiber laminates , Fuselages , Aircraft construction materials , Fatigue tests , Riveted joints , Lap joints , Curved panels , Flat plates , Skin(Structural member) , Scale models , Structural strain , Crack initiation , Crack propagation , Tensile deformation , Foreign technology
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