The effect of disbonds on stability aspects of adhesively bonded aluminum panels during compression loading-Reference-Cited by-同舟云学术

The effect of disbonds on stability aspects of adhesively bonded aluminum panels during compression loading

Published:2015-11 Issue: Volume:96 Page:372-382
ISSN:0263-8231
Container-title:Thin-Walled Structures
language:en
Short-container-title:Thin-Walled Structures

Author:

Zarouchas D.S.,Alderliesten R.C.

Publisher

Elsevier BV

Subject

Mechanical Engineering,Building and Construction,Civil and Structural Engineering

Reference25 articles.

1. Adhesive bonding of aircraft structures;Higgins;Int. J, Adhes. Adhes.,2000

2. Handbook of Adhesion Technology;Da Silva,2011

3. U.G. Goranson, Damage tolerance facts and fiction, in: International Conference on Damage Tolerance of Aircraft Structures, Delft University of Technology, Delft, the Netherlands, 2007.

4. Analytical prediction of Mode I stress intensity factors for cracked panels containing bonded stiffeners;Rans;Eng. Fract. Mech.,2013

5. Damage tolerance of bonded aircraft structures;Alderliesten;Int. J. Fatigue,2009

Cited by 9 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Fracture analysis of composite-titanium adhesively bonded joints under mode-Ⅰ loading;Engineering Fracture Mechanics;2023-10

2. Buckling and Post-Buckling Behaviours of Adhesively Bonded Aluminium Beams: A Review;REV ADHES ADHES;2022

3. Structural health monitoring of aerospace sandwich structures via strain measurements along zero-strain trajectories;Engineering Failure Analysis;2021-08

4. Composites airframe panel design for post-buckling – An experimental investigation;Composite Structures;2020-06

5. Strain-based health indicators for the structural health monitoring of stiffened composite panels;Journal of Intelligent Material Systems and Structures;2020-05-27