Abstract
The effects of fibre fraction on thermal degradation of composites containing glass, carbon and glass/carbon hybrid reinforcements in a bifunctional epoxy resin system were studied. Thermogravimetric technique was used to monitor the weight loss with the temperature. The degradation patterns so obtained were correlated with the fibre fraction of the composites.
Get full access to this article
View all access options for this article.
References
1.
1.
Zweben, C.
and
Norman, J.C.
(July 1976 ). Kevlar 49/Thornel 300 hybrid fabric composites for aerospace applications . SAMPE Quarterly , 1 -10 .
2.
2.
Bunsell, A.R.
and
Harris, B.
(July, 1974 ). Hybrid carbon and glass fibre composites . Composites , 157 -164 .
3.
3.
French, A.M.
and
Pritchard, G.
(1992 ). Environmental stress corrosion of hybrid fibre composites . Composites Science and Technology , 45 : 257 -263 .
4.
4.
Wendland, W.W.
(1986 ). Chemical analysis - a series of monographs on analytical chemistry and its applications . Thermal Analysis , 19 (3 ): 195 -199 .
5.
5.
Wendel, T.J.
(1978 ). Critical evaluation of several methods for determining fibre fraction of cured graphite/epoxy composites . ISAMPE , 23 : 160 .
6.
6. Annual book of ASTM Standards , (1992 ). (Revised edition ) pp. 35 -36 .
