Hybrid (bolted/bonded)joints applied to aeronautic parts: analytical two-dimensional model of a single-lap joint - Archive ouverte HAL Access content directly
Journal Articles Journal of Aircraft Year : 2007

Hybrid (bolted/bonded)joints applied to aeronautic parts: analytical two-dimensional model of a single-lap joint

Abstract

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.
Fichier principal
Vignette du fichier
Paroissien_896.pdf (273.76 Ko) Télécharger le fichier
Origin : Files produced by the author(s)
Loading...

Dates and versions

hal-01892180 , version 1 (10-10-2018)

Identifiers

Cite

Eric Paroissien, Marc Sartor, Jacques Huet, Frederic Lachaud. Hybrid (bolted/bonded)joints applied to aeronautic parts: analytical two-dimensional model of a single-lap joint. Journal of Aircraft, 2007, 4 (2), pp.573-582. ⟨10.2514/1.24452⟩. ⟨hal-01892180⟩
31 View
72 Download

Altmetric

Share

Gmail Facebook X LinkedIn More