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Fatigue crack growth specimen configuration with compressive loads present

✍ Scribed by R. I. Stephens


Publisher
Springer Netherlands
Year
1976
Tongue
English
Weight
158 KB
Volume
12
Category
Article
ISSN
1573-2673

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Influence of specimen configuration and
✍ Vikas Kumar Saxena; G. Malakondaiah; V.M. Radhakrishnan πŸ“‚ Article πŸ“… 1994 πŸ› Elsevier Science 🌐 English βš– 425 KB

## Experimental investigations have been carried out to study the effect of specimen configuration and loading history on the crack growth behaviour of 2024-T3 aluminium alloy at room temperature. It has been observed that fatigue crack growth rate in specimens loaded symmetrically is higher than