A critical assessment has been performed by compiling experimental data concerning the temperature dependence of stage If fatigue crack growth. For aluminium alloys, high strength steels, austenitic stainless steels and superalloys, the power coefficient, M, for the Paris reIationship is temperature
โฆ LIBER โฆ
Use of a kinetic equation to describe the temperature dependence of fatigue-crack-growth rate
โ Scribed by S. Ya. Yarema; O. P. Ostash
- Publisher
- Springer
- Year
- 1977
- Tongue
- English
- Weight
- 229 KB
- Volume
- 12
- Category
- Article
- ISSN
- 1573-885X
No coin nor oath required. For personal study only.
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The presented experimental results for 2xxx, 6xxx and 7xxx type aluminium alloys show a variability of the fatigue crack growth rates in the Paris regime to an extent important for the materials selection according to the damage tolerant design concept in the aircraft industry. This paper briefly re