Effect of Adhesive Thickness on Fatigue Disbonding Through a Cohesive Zone Modelling Approach
Adhesively bonded joints are crucial to the aeronautical industry, contributing to weight reduction and more sustainable flights. However, certifying these joints is still a topic of debate due to the lack of reliable inspection methods to determine their strength. Additionally, prediction models fo...
Saved in:
Main Authors: | Johan Birnie, Maria Pia Falaschetti, Enrico Troiani |
---|---|
Format: | Article |
Language: | English |
Published: |
MDPI AG
2025-03-01
|
Series: | Engineering Proceedings |
Subjects: | |
Online Access: | https://www.mdpi.com/2673-4591/90/1/65 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
Implementation of a Non-Intrusive Primal–Dual Method with 2D-3D-Coupled Models for the Analysis of a DCB Test with Cohesive Zones
by: Ricardo Hernández, et al.
Published: (2025-06-01) -
MODELLING OF CRACK PROPAGATION: COMPARISON OF DISCRETE LATTICE SYSTEM AND COHESIVE ZONE MODEL
by: Karel Mikeš, et al.
Published: (2020-03-01) -
Influence of constructive solutions on the formation of fatigue curve of the side frames of freight car bogies
by: A. V. Sukhov, et al.
Published: (2016-10-01) -
FATIGUE CRACKING MECHANISMS OF TITANIUM ALLOY VT3-1 IN VERY-HIGH-CYCLE-FATIGUE REGIME
by: A. A. Shanyavskiy, et al.
Published: (2016-11-01) -
PCI for Chronic Total Occlusions with Distal Diffuse Disease: Stent Alone vs. Stent plus Drug Balloon
by: Xinyi Yan, et al.
Published: (2025-10-01)