Fatigue tests on notched specimens of 2024-T351 aluminum alloy under a low altitude aircraft load spectrum
1968
V, 19 S.
graph. Darst.
Book
English
Notch Size Effects in 2024-T351 Aluminum Alloy Under Fatigue Spectrum Loading
Online Contents | 1998
|Notch Size Effects in 2024-T351 Aluminum Alloy Under Fatigue Spectrum Loading
British Library Online Contents | 1998
|ALUMINUM ALLOY PLATE 4.5Cu - 1.5Mg - 0.6Mn (2024-T351) Stress-Relief Stretched
SAE Technical Papers | 1960