The present work is devoted to study the influence of high cycle fatigue damage rate at R = 0.1, on the mechanical properties of aluminum alloy 2024-T3 which is largely used in aircraft industry. The study consists of an experimental investigation in the evolution of the static properties such as th
Influence of surface condition on the fatigue of an aluminum-lithium alloy (2090-T3)
โ Scribed by A. Eftekhari; J.E. Talia; P.K. Mazumdar
- Publisher
- Elsevier Science
- Year
- 1995
- Tongue
- English
- Weight
- 282 KB
- Volume
- 199
- Category
- Article
- ISSN
- 0921-5093
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