Fatigue properties of AlSi10Mg obtained by additive manufacturing: Defect-based modelling and prediction of fatigue strength

Author:

Romano S.,Brückner-Foit A.,Brandão A.,Gumpinger J.,Ghidini T.,Beretta S.

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Reference81 articles.

1. Moriaux F. Additive manufacturing for space application; 2015. .

2. U.S. Department of Transportation. FAA Advisory Circular 25. 1309-1A System Design and Analysis; 1988.

3. U.S. Department of Transportation. FAA Advisory Circular 33.70-1. Guidance Material for Aircraft Engine Life-Limited Parts Requirements; 2009.

4. National Aeronautics and Space Administration (NASA). EM20 – Engineering and Quality Standard for Additively Manufactured Spaceflight Hardware (draft). Tech. rep.; 2015.

5. Defect distribution and microstructure heterogeneity effects on fracture resistance and fatigue behavior of EBM Ti-6Al-4V;Seifi;Int J Fatigue,2017

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