[HTML][HTML] Fatigue failure of soft adhesive systems: a state-of-the-art review

C Yao, Y **a, Z Yang, Z Zhu, Z Li, H Jiang - Giant, 2024 - Elsevier
Soft adhesive systems (SASs), which consist of a soft adhesive layer and/or soft adherends,
have been extensively applied in advanced fields such as biomedicine, flexible electronics …

A review on reductions in the stress-intensity factor of cracked plates using bonded composite patches

A Aabid, M Hrairi, JSM Ali, TA Sebaey - Materials, 2022 - mdpi.com
In aerospace engineering applications, lightweight material structures are considered to
perform difficult service conditions and afford energy efficiency. Therefore, composite …

[HTML][HTML] XFEM–ANN approach to predict the fatigue performance of a composite patch repaired aluminium panel

S Suman, K Dwivedi, S Anand, H Pathak - Composites Part C: Open Access, 2022 - Elsevier
A novel extended finite element method (XFEM)-artificial neural network (ANN) approach is
proposed to predict the performance of aluminium panels repaired single-sided with a …

Numerical investigation of fatigue behavior of non-patched and patched aluminum/composite plates

H Adin, Z Sağlam, MŞ Adin - European Mechanical Science, 2021 - dergipark.org.tr
In this study, the fatigue behavior of composite patched and non-patched Al 5083 aluminum
plates was numerically investigated. Al 5083 Aluminum plates with semi-circular notched (2 …

XFEM and CZM modeling to predict the repair damage by composite patch of aircraft structures: Debonding parameters

MA Bellali, B Serier, M Mokhtari, RDSG Campilho… - Composite …, 2021 - Elsevier
In this work, a model based on the combination of two approaches XFEM and CZM, has
been used to predict the damage of repairs by composite patch (patch/adhesive/plate …

Comparison of repair methods for cracked titanium alloy aircraft structures with single-sided adhesively bonded composite patches

J Hu, C Li, J Fang, S Chen, S Xuan, W Tian - Materials, 2023 - mdpi.com
Composite patches are widely accepted as a useful practice for the repair of cracked aircraft
components and the repair method is of vital importance to the final performance of the …

Numerical investigation of patch geometry effect on the fatigue life of aluminum panels containing cracks repaired with CFRP composite patch using XFEM and CZM …

E Mosayyebi, TN Chakherlou - International Journal of Adhesion and …, 2025 - Elsevier
This study investigated numerically the effect of using composite patches with various
geometric shapes to improve the fatigue life of aluminum panels of AA7075-T6 and AA2024 …

Fatigue life improvement of cracked aluminum 6061-T6 plates repaired by composite patches

A Yousefi, S Jolaiy, R Hedayati, A Serjouei, M Bodaghi - Materials, 2021 - mdpi.com
Bonded patches are widely used in several industry sectors for repairing damaged plates,
cracks in metallic structures, and reinforcement of damaged structures. Composite patches …

An experimental and parametrical study on repair of cracked titanium airframe structures with single-side bonded carbon fiber-reinforced polymer prepreg patches

J Hu, R Kang, J Fang, S Chen, S Xuan, J Zhou… - Composite …, 2024 - Elsevier
The present research aims to investigate efficient repair techniques of cracked Ti-alloy
aircraft structures with adhesively bonded carbon fiber-reinforced polymer prepreg patches …

Effect of patch length and elevated temperature on fatigue behaviour of repaired aluminium panels with a CFRP patch

HP Shinde, N Sonawane, MG Karnik… - The Journal of …, 2023 - Taylor & Francis
Thin panels of aluminium alloy 6061-T6 with a centre pre-crack were repaired with a one-
sided asymmetrical CFRP patch through co-curing of epoxy at the room temperature to have …