Experimental and theoretical studies of corrosion-induced mechanical properties degradation of aircraft 2024 aluminum alloy

Materials Science and Engineering: A

Volumn 498, Issue 1-2, 2008, Pages 248-257

  Alexopoulos, N D ^a   Papanikos, P ^b  

^a NATIONAL TECHNICAL UNIVERSITY OF ATHENS   (Greece)

^b UNIVERSITY OF THE AEGEAN   (Greece)

Author keywords

2024 T3 alloy; Corrosion; Finite element analysis; Fracture toughness; Tensile test

Indexed keywords

ALUMINUM ALLOYS; ALUMINUM CORROSION; DEGRADATION; FIGHTER AIRCRAFT; FRACTURE; FRACTURE TOUGHNESS; HYDROGEN; HYDROGEN EMBRITTLEMENT; SURFACE DEFECTS; TENSILE TESTING;

2024 ALUMINIUM ALLOYS; 2024-T3; 2024-T3 ALLOY; DEGRADATION MECHANISM; EFFECTIVE THICKNESS; EXPOSURE-TIME; FINITE ELEMENT ANALYSE; PROPERTY DEGRADATION; TENSILE TEST; THEORETICAL STUDY;

FINITE ELEMENT METHOD;

EID: 54349094467     PISSN: 09215093     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.msea.2008.08.024     Document Type: Article

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