Fatigue of Aeronautical Structures

General

Code: ΜΕΑ_ΜΕ32

Description

Aeronautical materials – Fundamental aspects of fatigue – Woehler curves – Fatigue mechanisms – Design concepts – Damage tolerance design – Fatigue fracture characteristics – Fatigue crack growth under constant amplitude loading – Effect of overloads & underloads on the fatigue crack growth behavior – Fatigue crack growth under variable and real loading conditions – Multi-site damage and ageing aircraft – Structural integrity – Environmental effects (corrosion, temperature) on the fatigue behavior of aeronautical materials – Fatigue of aircraft structures.

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DateFile
13-09-2006 13-09-2006.PDF