Abstract
The fatigue qualification of critical components in Glassfiber Epoxy Composite materials, which are going to be installed on a new design helicopter is carried out according to methods which are also typical for the same components made in metal.
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© 1983 Plenum Press, New York
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Brivio, A., Parenti, G., Samanni, G., Wagner, V., Zanotti, C. (1983). Consideration on the Fatigue Damage of Specimens Used for Composite Critical Components Qualification. In: Seferis, J.C., Nicolais, L. (eds) The Role of the Polymeric Matrix in the Processing and Structural Properties Composite Materials. Springer, Boston, MA. https://doi.org/10.1007/978-1-4615-9293-8_34
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DOI: https://doi.org/10.1007/978-1-4615-9293-8_34
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