3D Explicit Simulation of Bearing Failure in Composite Fuselage Joints
Author(s) -
B. Egan,
C.T. McCarthy,
M.A. McCarthy
Publication year - 2013
Language(s) - English
DOI - 10.13140/rg.2.1.2274.9201
Subject(s) - fuselage , structural engineering , composite number , joint (building) , bearing (navigation) , stress (linguistics) , contact mechanics , boundary value problem , boundary (topology) , materials science , engineering , composite material , finite element method , computer science , mathematics , mathematical analysis , artificial intelligence , philosophy , linguistics
A typical FE model of a countersunk joint is shown in Fig. 2, where boundary conditions simulate in-plane loading. The mesh is refined near the fasteners to capture high stress gradients and contact conditions are enforced using the general contact algorithm of Abaqus/Explicit. The inclusion of interior contact surfaces facilitates simulation of progressive hole crushing featured in bearing failure.
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