Titlebook: Damage Tolerance of Metallic Aircraft Structures; Materials and Numeri Sérgio M. O. Tavares,Paulo M. S. T. de Castro Book 2019 The Author(s

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Fatigue Crack GrowthReaders of this book will have previous knowledge of fracture mechanics, and as such no effort will be made to delve here into fundamental concepts.

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Damage Tolerance of Metallic Aircraft Structures978-3-319-70190-5Series ISSN 2191-530X Series E-ISSN 2191-5318

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H. Peter Knudsen,Allen S. Lefohnepresent a substantial part of the aircraft. This section briefly reviews the fatigue crack propagation behaviour of typical Al alloys, including Al-Li alloys of interest because of their low weight and high strength. Al prominence is now disputed by composites; other alloys as Ti alloys and steel are used for specific applications.

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Materials the long period of preeminence of aluminum as the main material for structures of aircraft, Merati [.]. Facing competition from composite fiber reinforced plastics, aluminum producers are trying to reduce weight and improve performance developing new alloys. In parallel, joining techniques as laser