Hybrid (Bolted/Bonded) Joints Applied to Aeronautic Parts: Analytical Two-Dimensional Model of a Single-Lap Joint | Zendy

Éric Paroissien | Zendy; Marc Sartor | Zendy; Jacques Huet | Zendy; Frédéric Lachaud | Zendy

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Hybrid (Bolted/Bonded) Joints Applied to Aeronautic Parts: Analytical Two-Dimensional Model of a Single-Lap Joint

Author(s) -

Éric Paroissien,

Marc Sartor,

Jacques Huet,

Frédéric Lachaud

Publication year - 2006

Publication title -

hal (le centre pour la communication scientifique directe)

Language(s) - English

Resource type - Conference proceedings

DOI - 10.2514/6.2006-2268

Subject(s) - joint (building) , materials science , lap joint , bolted joint , structural engineering , composite material , finite element method , engineering

The mechanical behavior of hybrid (bolted/bonded) joints is investigated. The joints under study are balanced single-lap joints, and an elastic behavior of the materials is assumed. A fully parametric analytical two-dimensional model, based on the Finite Element Method, is presented. A special Finite Element (“Bonded Beams” element) is computed in order to simulate the bonded adherends. The simulation of fasteners is examined through experimental and numerical approaches. Good agreement was found between the experimental and numerical results

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