A critical consideration for the use of Al-cladding for protecting aircraft aluminum alloy 2024 against corrosion

Theoretical and Applied Fracture Mechanics

Volumn 57, Issue 1, 2012, Pages 36-42

  Pantelakis, Sp G ^a   Chamos, A N ^a   Kermanidis, Al Th ^a  

^a UNIVERSITY OF PATRAS   (Greece)

Author keywords

Cladding; Corrosion environment; Mechanical properties; Protection

Indexed keywords

2024 ALLOY; 3.5%NACL; AIRCRAFT STRUCTURE; CLADDING LAYER; CORROSION DAMAGE; CORROSION ENVIRONMENT; CORROSION TESTS; EXFOLIATION CORROSION; FATIGUE BEHAVIOR; LABORATORY SIMULATION; MECHANICAL TESTS; PROTECTION; SERVICE CONDITIONS;

AIRCRAFT MANUFACTURE; AIRFRAMES; ALUMINUM ALLOYS; ATMOSPHERIC CORROSION; CLADDING (COATING); CONCRETE BEAMS AND GIRDERS; CORROSION PROTECTION; MECHANICAL PROPERTIES; SODIUM CHLORIDE; WELDS;

ALUMINUM;

EID: 84858285074     PISSN: 01678442     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.tafmec.2011.12.006     Document Type: Article

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