TR
EN
Interlaminar Fracture Response of Glass Fibre/Epoxy Laminates Toughened with Glass Fibre Veils
Öz
This study investigates the influence of glass fibre veil interlayers on the Mode I interlaminar fracture behaviour of glass fibre-reinforced epoxy laminates. Laminates with a stacking sequence of [0]₈ were manufactured using a vacuum-assisted resin infusion process. A 30 g/m² glass fibre veil is inserted at the mid-plane to evaluate the toughening efficiency of the veils. Mode-I interlaminar fracture properties are determined through double cantilever beam (DCB) tests in accordance with ASTM D5528. The fracture initiation (GI,C) and propagation (GI,R) energies are calculated using Modified Beam Theory (MBT). The load–displacement responses revealed stable crack growth for both laminate configurations, while veil-toughened laminates exhibit higher fracture resistance during crack initiation and propagation under mode-I loading. The incorporation of the glass fibre veils leads to ∼44% increase in fracture initiation energy and a ∼22% increase in propagation fracture energy compared to the untoughened baseline laminates. Rising R-curve behaviour is observed in untoughened and toughened laminates, indicating the activation of intrinsic and extrinsic toughening mechanisms under mode-I loading conditions. The digital images captured from the specimens demonstrate that fibre bridging fracture mechanisms are established in both laminate systems. In addition, crack migration toward neighbouring lamina is observed from both laminates. The study concludes that crack deviation is more closely associated with fibre waviness induced by stitching patterns in non-crimp fibre fabric preforms rather than differences in interfacial material properties. Overall, the results demonstrate that glass fibre veils offer an effective and easy-to-apply strategy for improving the interlaminar fracture resistance of glass fibre-reinforced epoxy laminates.
Anahtar Kelimeler
Etik Beyan
Ethics committee approval was not required for this study because of there was no study on animals or humans.
Kaynakça
- Akbolat, M. Ç., Katnam, K. B., Soutis, C., Potluri, P., Sprenger, S., & Taylor, J. (2022). On mode-I and mode-II interlaminar crack migration and R-curves in carbon/epoxy laminates with hybrid toughening via core-shell rubber particles and thermoplastic micro-fibre veils. Composites Part B: Engineering, 238, Article 109900. https://doi.org/10.1016/j.compositesb.2022.109900
- ASTM International. (2022). Standard test method for mode I interlaminar fracture toughness of unidirectional fiber-reinforced polymer matrix composites (ASTM D5528). https://www.astm.org/Standards/D5528
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- Guild, F. J., Tsang, W. L., & Taylor, A. C. (2022). Silica nano-particle filled polymers: Debonding and microstructure. Composites Science and Technology, 218, Article 109202. https://doi.org/10.1016/j.compscitech.2021.109202
- Hojo, M., Matsuda, S., Tanaka, M., Ochiai, S., & Murakami, A. (2006). Mode I delamination fatigue properties of interlayer-toughened CF/epoxy laminates. Composites Science and Technology, 66, 665–675. https://doi.org/10.1016/j.compscitech.2005.07.038
- Katnam, K. B., Da Silva, L. F. M., & Young, T. M. (2013). Bonded repair of composite aircraft structures: A review of scientific challenges and opportunities. Progress in Aerospace Sciences, 61, 26–42. https://doi.org/10.1016/j.paerosci.2013.03.003
Ayrıntılar
Birincil Dil
İngilizce
Konular
Havacılık Malzemeleri
Bölüm
Araştırma Makalesi
Yazarlar
Yayımlanma Tarihi
15 Temmuz 2026
Gönderilme Tarihi
28 Nisan 2026
Kabul Tarihi
11 Haziran 2026
Yayımlandığı Sayı
Yıl 2026 Cilt: 9 Sayı: 4
APA
Akbolat, M. Ç. (2026). Interlaminar Fracture Response of Glass Fibre/Epoxy Laminates Toughened with Glass Fibre Veils. Black Sea Journal of Engineering and Science, 9(4), 1659-1664. https://doi.org/10.34248/bsengineering.1939671
AMA
1.Akbolat MÇ. Interlaminar Fracture Response of Glass Fibre/Epoxy Laminates Toughened with Glass Fibre Veils. BSJ Eng. Sci. 2026;9(4):1659-1664. doi:10.34248/bsengineering.1939671
Chicago
Akbolat, Mehmet Çağatay. 2026. “Interlaminar Fracture Response of Glass Fibre/Epoxy Laminates Toughened with Glass Fibre Veils”. Black Sea Journal of Engineering and Science 9 (4): 1659-64. https://doi.org/10.34248/bsengineering.1939671.
EndNote
Akbolat MÇ (01 Temmuz 2026) Interlaminar Fracture Response of Glass Fibre/Epoxy Laminates Toughened with Glass Fibre Veils. Black Sea Journal of Engineering and Science 9 4 1659–1664.
IEEE
[1]M. Ç. Akbolat, “Interlaminar Fracture Response of Glass Fibre/Epoxy Laminates Toughened with Glass Fibre Veils”, BSJ Eng. Sci., c. 9, sy 4, ss. 1659–1664, Tem. 2026, doi: 10.34248/bsengineering.1939671.
ISNAD
Akbolat, Mehmet Çağatay. “Interlaminar Fracture Response of Glass Fibre/Epoxy Laminates Toughened with Glass Fibre Veils”. Black Sea Journal of Engineering and Science 9/4 (01 Temmuz 2026): 1659-1664. https://doi.org/10.34248/bsengineering.1939671.
JAMA
1.Akbolat MÇ. Interlaminar Fracture Response of Glass Fibre/Epoxy Laminates Toughened with Glass Fibre Veils. BSJ Eng. Sci. 2026;9:1659–1664.
MLA
Akbolat, Mehmet Çağatay. “Interlaminar Fracture Response of Glass Fibre/Epoxy Laminates Toughened with Glass Fibre Veils”. Black Sea Journal of Engineering and Science, c. 9, sy 4, Temmuz 2026, ss. 1659-64, doi:10.34248/bsengineering.1939671.
Vancouver
1.Mehmet Çağatay Akbolat. Interlaminar Fracture Response of Glass Fibre/Epoxy Laminates Toughened with Glass Fibre Veils. BSJ Eng. Sci. 01 Temmuz 2026;9(4):1659-64. doi:10.34248/bsengineering.1939671