Abstract
Aircraft components made from composites are subject to impact damage during service. Their performance and structural integrity would be affected and need to be assessed for establishing the allowable damage limits. One of the damage tolerant criteria is to allow no growth of the damaged region during the life of the aircraft. Considered also are repair methods for reinforcing damaged composite parts.
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© 1995 Springer Science+Business Media Dordrecht
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Campolo, C., Cipri, F. (1995). Damage Characterization, Damage Growth Validation and Repair Consideration of Advanced Aircraft Composite Structures. In: Sih, G.C., Carpinteri, A., Surace, G. (eds) Advanced Technology for Design and Fabrication of Composite Materials and Structures. Engineering Applications of Fracture Mechanics, vol 14. Springer, Dordrecht. https://doi.org/10.1007/978-94-015-8563-7_20
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DOI: https://doi.org/10.1007/978-94-015-8563-7_20
Publisher Name: Springer, Dordrecht
Print ISBN: 978-90-481-4507-2
Online ISBN: 978-94-015-8563-7
eBook Packages: Springer Book Archive