Tensile and energy density properties of 2024, 6013, 8090 and 2091 aircraft aluminum alloy after corrosion exposure

Theoretical and Applied Fracture Mechanics

Volumn 33, Issue 2, 2000, Pages 117-134

  Pantelakis, Sp G ^a   Daglaras, P G ^a   Apostolopoulos, Ch Alk ^a  

^a UNIVERSITY OF PATRAS   (Greece)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT MATERIALS; ALUMINUM ALLOYS; ALUMINUM CORROSION; ALUMINUM METALLOGRAPHY; STRESS ANALYSIS; TENSILE PROPERTIES; TENSILE STRESS; YIELD STRESS;

ALUMINUM ALLOY 2024 T351; ALUMINUM ALLOY 2091 T84; ALUMINUM ALLOY 6013 T6; ALUMINUM ALLOY 8090 T81;

FRACTURE MECHANICS;

AIRCRAFT; ALUMINUM ALLOY; CORROSION; ENERGY; TENSILE STRUCTURE;

EID: 0034065297     PISSN: 01678442     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0167-8442(00)00007-0     Document Type: Article

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