Experiments are described in which notched specimens of 2024-T351 aluminum alloy were subjected to fatigue load distribution typical of that encountered by aircraft operating continuously at low altitude; they serve to demonstrate effects of design stress level on life and suggest that lives of general-purpose aircraft currently used in these roles may be as low as 2000 to 3000 hrs; other findings. (48492)
Fatigue tests on notched specimens of 2024-T351 aluminum alloy under low altitude aircraft load spectrum
Nat Res Counc Can, Aeronaut Rep
1968
Report
English
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Notch Size Effects in 2024-T351 Aluminum Alloy Under Fatigue Spectrum Loading
British Library Online Contents | 1998
|Notch Size Effects in 2024-T351 Aluminum Alloy Under Fatigue Spectrum Loading
Online Contents | 1998
|