Failure Behavior of Composite Laminates with Multi-Pin Loaded Holes

KARAKUZU R., Icten B. M., Tekinsen O.

JOURNAL OF REINFORCED PLASTICS AND COMPOSITES, cilt.29, sa.2, ss.247-253, 2010 (SCI-Expanded) identifier identifier

  • Yayın Türü: Makale / Tam Makale
  • Cilt numarası: 29 Sayı: 2
  • Basım Tarihi: 2010
  • Doi Numarası: 10.1177/0731684408097758
  • Dergi Adı: JOURNAL OF REINFORCED PLASTICS AND COMPOSITES
  • Derginin Tarandığı İndeksler: Science Citation Index Expanded (SCI-EXPANDED), Scopus
  • Sayfa Sayıları: ss.247-253
  • Anahtar Kelimeler: failure load, failure mode, glass epoxy composite, multi-pin loading, GEOMETRIC PARAMETERS, BOLTED JOINTS, STRENGTH, PLATES
  • Dokuz Eylül Üniversitesi Adresli: Evet

Özet

The aim of this study is to determine the failure behavior of laminated glass-epoxy composite plate which is subjected to a traction force by four pins. The failure load and failure mode of composite plates which have the stacking sequence of [0/90/+/- 45](S) has been observed experimentally. The ratio of edge distance from the hole center to pin diameter (E/D), the ratio of longitudinal holes distance to pin diameter (F/D) and the ratio of transverse holes distance to pin diameter (G/D) were selected as parameters. The results showed that the specimens except for E/D = 2 have similar behavior in terms of failure loads and failure modes.