Benefits of improved fuselage skin sheet alloy 2524-T3 in multisite damage scenarios

Light Metal Age

Volumn 56, Issue 11-12, 1998, Pages

  Bray, Gary H ^a   Bucci, Robert J ^a   Kulak, Michael ^a   Warren, Charles J ^a   Grandt Jr , Alten F ^a   Golden, Patrick J ^a   Sexton, Darren G ^a  

^a ALCOA INC   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

DAMAGE TOLERANCE; FATIGUE CRACK GROWTH RESISTANCE; MAINTENANCE COST; MULTISITE DAMAGE; RESIDUAL STRENGTH; SKIN SHEET ALLOY;

AIRCRAFT; CORROSION; CRACK PROPAGATION; FATIGUE OF MATERIALS; FATIGUE TESTING; FRACTURE TOUGHNESS; FUSELAGES; IMPACT RESISTANCE; MAINTENANCE; STRENGTH OF MATERIALS; STRESS CORROSION CRACKING; TENSILE STRENGTH;

ALUMINUM ALLOYS;

EID: 0032297291     PISSN: 00243345     EISSN: None     Source Type: Trade Journal    
DOI: None     Document Type: Article

References (11)