Corrosion-fatigue crack nucleatiom in Alclad 2024-T3 commercial aircraft skin

ASTM Special Technical Publication

Volumn 1298, Issue , 1997, Pages 74-88

  Schmidt, Charles G ^a   Crocker, James E ^a,b   Giovanola, Jacques H ^a   Kanazawa, Christine H ^a   Shockey, Donald A ^a   Flournoy, Thomas H ^c  

^a SRI INTERNATIONAL   (United States)

^b UNIVERSITY OF CONNECTICUT   (United States)

^c WILLIAM J HUGHES TECHNICAL CENTER   (United States)

Author keywords

Alclad 2024 T3; Corrosion fatigue; Crack nucleation

Indexed keywords

AIRCRAFT MATERIALS; ALUMINUM CLADDING; ALUMINUM CORROSION; CORROSION FATIGUE; CRACK PROPAGATION; DISSOLUTION; HYDROGEN EMBRITTLEMENT; PH EFFECTS; PITTING; SALINE WATER;

AIRCRAFT SKIN; ALUMINUM ALLOY ALCLAD 2024 T3;

ALUMINUM ALLOYS;

EID: 0031121531     PISSN: 00660558     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Article

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