The impact of flaws, inclusions, and cracks on the fatigue resistance of mechanical and aeronautical components, even those constructed of high strength-to-mass ratio materials, is discussed in this chapter. The numerical growth of fractures and flaws will be simulated using finite element techniques. The replicate experimental procedure will allow the results to be confirmed.
Author (s) Details
Sergio Baragetti
Department of Management, Information and Production Engineering, University of Bergamo Viale Marconi 5, 24044 Dalmine (BG), Italy.
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