TY - JOUR
T1 - Structural integrity assessment of a full-scale adhesively-bonded bi-material joint for maritime applications
AU - Saeedifar, Milad
AU - Saleh, Mohamed Nasr
AU - Krairi, Anouar
AU - de Freitas, Sofia Teixeira
AU - Zarouchas, Dimitrios
PY - 2023
Y1 - 2023
N2 - The present study proposes a comprehensive integrity assessment approach for a full-scale adhesively-bonded bi-material joint for maritime applications. The joint represents a cross-section of the bond-line connection of a ship with a steel hull and a sandwich composite superstructure. The full-scale joint consists of a sandwich composite core adhesively bonded to two U-shaped steel brackets. The joint was subjected to a quasi-static loading profile including 6 load cycles up to the final failure. Each load cycle was followed by a dwell segment holding the joint at the maximum displacement for 30 s and then unloading to 50% of the maximum displacement. Three Structural Health Monitoring (SHM) techniques including Acoustic Emission (AE), Fiber Optic Sensor (FOS), and Digital Image Correlation (DIC) were employed during the test to assess the damage state of the joint. Moreover, a Finite Element Model (FEM) was developed to simulate the evolution behavior of different damage mechanisms in the joint and the FE results were compared against the experimental findings. The obtained results showed that the integration of all the employed techniques could successfully detect the damage initiation, assess the severity of the damage, localize the critical regions of the joint, and distinguish the different damage mechanisms.
AB - The present study proposes a comprehensive integrity assessment approach for a full-scale adhesively-bonded bi-material joint for maritime applications. The joint represents a cross-section of the bond-line connection of a ship with a steel hull and a sandwich composite superstructure. The full-scale joint consists of a sandwich composite core adhesively bonded to two U-shaped steel brackets. The joint was subjected to a quasi-static loading profile including 6 load cycles up to the final failure. Each load cycle was followed by a dwell segment holding the joint at the maximum displacement for 30 s and then unloading to 50% of the maximum displacement. Three Structural Health Monitoring (SHM) techniques including Acoustic Emission (AE), Fiber Optic Sensor (FOS), and Digital Image Correlation (DIC) were employed during the test to assess the damage state of the joint. Moreover, a Finite Element Model (FEM) was developed to simulate the evolution behavior of different damage mechanisms in the joint and the FE results were compared against the experimental findings. The obtained results showed that the integration of all the employed techniques could successfully detect the damage initiation, assess the severity of the damage, localize the critical regions of the joint, and distinguish the different damage mechanisms.
KW - Acoustic emission
KW - Adhesively-bonded bi-material joint
KW - Finite element analysis (FEA)
KW - Full-scale mechanical test
KW - Integrity assessment
KW - Structural health monitoring
UR - http://www.scopus.com/inward/record.url?scp=85144627635&partnerID=8YFLogxK
U2 - 10.1016/j.tws.2022.110487
DO - 10.1016/j.tws.2022.110487
M3 - Article
AN - SCOPUS:85144627635
VL - 184
JO - Thin-Walled Structures
JF - Thin-Walled Structures
SN - 0263-8231
M1 - 110487
ER -