Corrosion-Fatigue Crack Nucleation in the Alclad Layer of 2024-T3 Commercial Aircraft Skin
Symposium; International mechanical engineering congress, Structural integrity in aging aircraft ; 1995 ; San Francisco; CA
1995-01-01
4 pages
Aufsatz (Konferenz)
Englisch
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Corrosion-Fatigue Crack Nucleation in the Alclad Layer of 2024-T3 Commercial Aircraft Skin
British Library Online Contents | 1995
|ALUMINUM ALLOY SHEET AND PLATE, ALCLAD 4.4Cu - 1.5Mg - 0.60Mn (Alclad 2024 and 1-1/2% Alclad 2024-0)
SAE Technical Papers | 1983
SAE Technical Papers | 1989
ALUMINUM ALLOY SHEET AND PLATE, ALCLAD 4.4Cu - 1.5Mg - 0.60Mn (Alclad 2024 and 1-1/2% Alclad 2024-0)
SAE Technical Papers | 1974