Investigation of failure mechanisms in aged aerospace composites
The effect of isothermal ageing on two high temperature, bismaleimide composite materials, a novel CSIRO CBR 320/328 composite and a commercial CIBA GEIGY Matrimid® 5292 composite, was examined at 204 and 250-°C. Delamination is a major cause of failure
|Collections||ANU Research Publications|
|Source:||Engineering Failure Analysis|
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