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
✦ LIBER ✦
Thermo-mechanical fatigue behaviour of a modern γ-TiAl alloy
✍ Scribed by Marcel Roth; Horst Biermann
- Publisher
- Elsevier Science
- Year
- 2008
- Tongue
- English
- Weight
- 324 KB
- Volume
- 30
- Category
- Article
- ISSN
- 0142-1123
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✦ Synopsis
The cyclic deformation and fatigue behaviour under thermo-mechanical load of the 3rd generation c-TiAl alloy TNB-V5 are evaluated. Strain controlled thermo-mechanical and isothermal fatigue tests were carried out with two different strain ranges, different temperature-strain cycles and different temperature ranges from 400 °C to 800 °C. Cyclic deformation curves, stress-strain hysteresis loops and fatigue lives of the tests are presented. The fatigue lives were well described by the Smith-Watson-Topper damage parameter.
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