Service Communautaire d'Information sur la Recherche et le Développement - CORDIS

Damage tolerance and fatigue design methodology

The shape, number and conditions of impact of the samples for extensive materials testing have been fixed, the complete evaluation programme is nearing completion and microscopy studies of relations between laminate lay up and shape of delaminations after impact have been completed.

Reported by

Construcciones Aeronauticas SA
Avd John Lennon S/N
28906 Getafe (Madrid)
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