Modelling of fatigue crack growth in 7075-T651 aluminium alloy plate
1985
12 Bl
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Report
English
Observations of fatigue crack initiation in 7075-T651
Tema Archive | 2010
|Aluminum Alloy Plate - 5.6zn - 2.5mg - 1.6cu - 0.26cr (7075-T651)
SAE Technical Papers | 1968
Aluminum Alloy Plate, Alclad - 5.6zn - 2.5mg - 1.6cu - 0.26cr (Alclad 7075-T651)
SAE Technical Papers | 1968
ALUMINUM ALLOY PLATE 5.6Zn - 2.5Mg - 1.6Cu - 0.30Cr (7075-T651) Stress-Relief Stretched
SAE Technical Papers | 1966
ALUMINUM ALLOY PLATE 5.6Zn - 2.5Mg - 1.6Cu - 0.30Cr (7075-T651) Stress-Relief Stretched
SAE Technical Papers | 1967