## Abstract The bending properties of composite materials are often characterized with simply supported beams under concentrated loads. The results from such tests are commonly based on homogeneous beam equations. For laminated materials, however, these formulas must be modified to account for the
β¦ LIBER β¦
Mode II Delamination of a Unidirectional Carbon Fiber/Epoxy Composite in Four-Point Bend End-Notched Flexure Tests
β Scribed by E. Zile; V. Tamuzs
- Book ID
- 106467770
- Publisher
- Springer US
- Year
- 2005
- Tongue
- English
- Weight
- 273 KB
- Volume
- 41
- Category
- Article
- ISSN
- 1573-8922
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## Abstract In this article, interlaminar crack initiation and propagation under mode I and II dynamic loading of an epoxy matrix reinforced with unidirectional carbon fibers were evaluated. Delamination in mode I was carried out employing the DCB test (Double Cantilever Beam). In mode II, the ENF