On the Potential Static Strength of Hybrid (Bolted/Bonded) Lap Joints with Functionally Graded Adhesives-Reference-Cited by-同舟云学术

On the Potential Static Strength of Hybrid (Bolted/Bonded) Lap Joints with Functionally Graded Adhesives

Published:2019-09 Issue:9 Volume:57 Page:4093-4103
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Paroissien Eric¹,Lachaud Frédéric¹

Affiliation:

1. Clément Ader Institute (ICA), University of Toulouse, ISAE-SUPAERO, INSA, IMT MINES ALBI, UTIII, CNRS, 3 Rue Caroline Aigle, 31400 Toulouse, France

Funder

ISAE-SUPAERO

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference45 articles.

1. Hart-SmithL. J. “Design Methodology for Bonded-Bolted Composite Joints,” AFWAL TR-81-3154, 1982, Douglas Aircraft Company, Long Beach, CA.

2. Adhesive bonding of aircraft structures

3. Analysis of the Effects of Thin Sealant Layers in Aircraft Structural Joints

4. Bonded-bolted composite joints

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