Fatigue and damage tolerance behaviour of corroded 2024 T351 aircraft aluminum alloy

Theoretical and Applied Fracture Mechanics

Volumn 43, Issue 1, 2005, Pages 121-132

  Kermanidis, Al Th ^a   Petroyiannis, P V ^a   Pantelakis, Sp G ^a  

^a UNIVERSITY OF PATRAS   (Greece)

Author keywords

Corroded 2024; Damage tolerance; Fatigue crack growth; Fatigue life; Fracture toughness; Hydrogen embrittlement

Indexed keywords

AIRCRAFT PARTS AND EQUIPMENT; ALUMINUM ALLOYS; CORROSION; CRACK PROPAGATION; CRACKS; FRACTURE TOUGHNESS; HYDROGEN EMBRITTLEMENT;

DAMAGE TOLERANCE BEHAVIOR; FATIGUE CRACK GROWTH CURVES; FATIGUE RESISTANCE; PRE-CORRODED 2024 T351 ALUMINUM ALLOY;

FATIGUE OF MATERIALS;

ALUMINUM; CRACK PROPAGATION; DAMAGE; FATIGUE; HYDROGEN EMBRITTLEMENT;

EID: 14944374275     PISSN: 01678442     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.tafmec.2004.12.008     Document Type: Article

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