Dergiler / European Mechanical Science / 2017 / Cilt: 1 - Sayı: 4

Characterization of Delamination Crack in Multidirectional E-glass/epoxy Composite under Mode I Loading

Sayfa
117–128
Yayın Tarihi
2017-11-27
DOI
—
🏛️Bu makalenin bibliyografik verileri ve tam metin bağlantısı DergiPark üzerinden sağlanmıştır.
DergiPark Kaydı ↗
✨

Yapay Zeka Hızlı Bakış & Çıkarımlar

AI Insight
⚡ TL;DR(1 Cümlede Hızlı Çıkarım)

According to the results, while fiber orientation affects significantly the extended crack length and the GIc distribution along the specimen width, stacking sequence only affects the GIc distribution.

📌 3 Maddede Bu Makale

🎯
Amaç & Hipotez:In this study, mode I critical strain energy release rate (GIc) of unidirectional E-glass/epoxy was determined by double cantilever beam (DCB) test.
📊
Temel Bulgular & Veri:The effect of stacking sequence and fiber orientation of the sublaminates and the effect of thickness on mode I delamination crack length and GIc distribution along the specimen width in 0o//0o interface have been studied using ANSYS®. 3-D 8-node linear interface element INTER 205 is used to create a predefined crack path.
💡
Sonuç & Katkı:According to the results, while fiber orientation affects significantly the extended crack length and the GIc distribution along the specimen width, stacking sequence only affects the GIc distribution.
🔬Tür:Modelleme & Sayısal Simülasyon
📍Kapsam:Genişletilmiş Akademik Örneklem
⚙️Değişkenler:E-glass/epoxy · Double Cantilever Beam · Delamination

Abstract

In this study, mode I critical strain energy release rate (GIc) of unidirectional E-glass/epoxy was determined by double cantilever beam (DCB) test. Calculated GIc was used to initiate delamination in numerical models. The effect of stacking sequence and fiber orientation of the sublaminates and the effect of thickness on mode I delamination crack length and GIc distribution along the specimen width in 0o//0o interface have been studied using ANSYS®. 3-D 8-node linear interface element INTER 205 is used to create a predefined crack path. To investigate the fiber orientation effect, composites with [+θ2, 902, -θ2, 02]s stacking sequences were modeled. Interlaminar fracture analyses were performed by Virtual Crack Closure Technique (VCCT). Experimental and numerical critical loads (Pcr) showed a good agreement. According to the results, while fiber orientation affects significantly the extended crack length and the GIc distribution along the specimen width, stacking sequence only affects the GIc distribution.

🔖

Bu Makaleye Atıf Yap

Darıcık, F., Aslan, Z. (2017). Characterization of Delamination Crack in Multidirectional E-glass/epoxy Composite under Mode I Loading. European Mechanical Science, Cilt: 1 - Sayı: 4, 117–128. https://ajindex.com/articles/665210

📄 Tam Metin PDF Okuyucu

📄

PDF görüntüleyici hazırlanıyor...

Kaynakça (9)

  1. Aoki, Y., Kondo, H., & Hatta, H. (2007). Effect of delamination propagation on mechanical behavior in compression after impact. 16th International Conference on Composite Materials. Kyoto, Japan. Shokrieh, M. M., Rajabpour-Shirazi, H., Heidari-Rarani, M., Haghpanahi, M. (2012). Simulation of mode I delamination propagation in multidirectional composites with R-curve effects using VCCT method. Computational Materials Science, 65, 66-73.
  2. Mathews, M. J., Swanson, S. R. (2007). Characterization of the interlaminar fracture toughness of a laminated carbon/epoxy composite. Composites Science and Technology, 67, 1489-1498. ASTM Standard D5528-01. (2001). Standard test method for mode I interlaminar fractre toughness of unidirectional continuous fiber reinforced polymer matrix composites. Philadelphia. Shokrieh, M. M., Heidari-Rarani, M. (2011). Effect of stacking sequence on R-curve behavior of glass/epoxy DCB laminates with 0o//0o crack interface. Materials Science and Engineering A, 529, 265-269. de Morais, A. B., de Moura, M. F., Marques, A. T., de Castro, P. T. (2002). Mode-I interlaminar fracture of carbon/epoxy cross-ply composites. Composites Science and Technology, 62, 5, 679-686.
  3. Sebaey, T. A., Blanco, N., Lopes, C. S., Costa, J. (2011). Numerical investigation to prevent crack jumping in double cantilever beam tests of multidirectional composite laminates. Composites Science and Technology, 71, 13, 1587-1592.
  4. Davidson, B. D., Krüger, R., König, M. (1996). Effect of stacking sequence on energy release rate distributions in multidirectional DCB and ENF specimens. Engineering Fracture Mechanics, 55, 4, 557-569.
  5. Prombut, P., Michel, L., Lachaud, F., Barrau, J. J. (2006). Delamination of multidirectional composite laminates at 0/ ply interfaces. Engineering Fracture Mechanics, 73, 16, 2427-2442.
  6. Shetty, M. R., Vijay Kumar, K. R., Sudhir, S., Raghu, P., Madhuranath, A. D., Rao, R. M. (2000). Effect of fibre orientation on mode-I interlaminar fracture toughness of glass epoxy composites. Journal of Reinforced Plastics and Composites, 19, 8, 606-620.
  7. Jimenez, M. A., Miravete, A. (2004). Application of the finite-element method to predict the onset of delamination growth. Journal of Composite Materials, 38, 1309-1335.
  8. Valvo, P. S. (2012). A revised virtual crack closure technique for physically consistent fracture mode partitioning. International Journal of Fracture, 173, 1, 1-20.
  9. Zhang, Y., Chryssanthopoulos, M. (2012). Modelling of mode I fracture behaviour of