An experimental and theoretical investigation of plane-stress fracture of 2024-T351 aluminum alloy
1970
Getr. Zählung
graph. Darst
Contract no. NAS 1-8522
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Report
English
ALUMINUM ALLOY PLATE 4.4Cu - 1.5Mg - 0.60Mn (2024-T351) Stress-Relief Stretched
SAE Technical Papers | 1967
ALUMINUM ALLOY PLATE 4.5Cu - 1.5Mg - 0.6Mn (2024-T351) Stress-Relief Stretched
SAE Technical Papers | 1964
ALUMINUM ALLOY PLATE 4.5Cu - 1.5Mg - 0.6Mn (2024-T351) Stress-Relief Stretched
SAE Technical Papers | 1960
ALUMINUM ALLOY BARS, ROLLED 4.5Cu - 1.5Mg - 0.6Mn (2024-T351) Stress-Relief Stretched
SAE Technical Papers | 1960
ALUMINUM ALLOY PLATE, ALCLAD 4.4Cu - 1.5Mg - 0.60Mn (Alclad 2024-T351) Stress-Relief Stretched
SAE Technical Papers | 1967