In this paper, comparisons of fracture stress values obtained in graphite/epoxy composites with the predictions of the model are made. The experimental results of Brinson and Yeow[l] on unidirectionsl composites using double edge notch tensile coupons were used. The calculations are performed usinp
β¦ LIBER β¦
An automated finite element analysis of the initiation and growth of damage in carbonfibre composite materials
β Scribed by Keith Gamble; Martin Pilling; Andrew Wilson
- Publisher
- Elsevier Science
- Year
- 1995
- Tongue
- English
- Weight
- 913 KB
- Volume
- 32
- Category
- Article
- ISSN
- 0263-8223
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