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.
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Communication dans un congrès
47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Material Conference, May 2006, Newport, Rhode Island, United States. 47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, pp. 1-23, 2006
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Dernière modification le : vendredi 14 décembre 2018 - 13:54:03
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  • HAL Id : hal-01494327, version 1
  • OATAO : 17643

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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. 47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Material Conference, May 2006, Newport, Rhode Island, United States. 47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, pp. 1-23, 2006. 〈hal-01494327〉

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