Corrosion-induced hydrogen embrittlement of 2024 and 6013 aluminum alloys

The effect of corrosion on the mechanical behavior of the aircraft aluminum alloys 2024 and 6013 has been investigated experimentally. It is shown that corrosion exposure leads to moderate reduction in yield and ultimate tensile stress. Dramatic reduction in elongation to failure and strain energy d...

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Veröffentlicht in:	Theoretical and applied fracture mechanics 2004-04, Vol.41 (1), p.173-183
Hauptverfasser:	Petroyiannis, P.V., Kermanidis, Al.Th, Papanikos, P., Pantelakis, Sp.G.
Format:	Artikel
Sprache:	eng
Schlagworte:	Aircraft Aluminum Corrosion Hydrogen embrittlement Multiscaling Residual strength Strain energy density
Online-Zugang:	Volltext
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