Ageing of a carbon epoxy composite for aeronautic applications
β Scribed by V. Bellenger; J. Decelle; N. Huet
- Publisher
- Elsevier Science
- Year
- 2005
- Tongue
- English
- Weight
- 235 KB
- Volume
- 36
- Category
- Article
- ISSN
- 1359-8368
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Nanoindentation tests on a carbon fiber and carbon matrix composite (C/C composite) for nuclear applications were carried out over a load range from 50pN to 20mN on two different crosssections, normal and parallel to the fiber axis. For reference, an isotropic nuclear graphite was also examined. Bot
## Abstract This work deals with the effect of temperature on the electrical properties of laminated epoxy composites containing 60% by volume of commercial unidirectional carbon fibers. The temperature was varied from 30Β°C to 120Β°C and the frequency range was from 10 Hz to 10 kHz. It is found that