Fatigue crack growth tests on 6082-T6 aluminium specimens have been carried out. The single edge notched tension specimens had a spark eroded 0.2 mm deep starter notch. In order to measure the crack growth, a special direct current potential drop method was used. The experiments were carried out at
β¦ LIBER β¦
Fatigue crack growth in high vacuum and gaseous atmospheres in an aluminium alloy
β Scribed by J Ruiz; M Elices
- Publisher
- Elsevier Science
- Year
- 1994
- Tongue
- English
- Weight
- 241 KB
- Volume
- 45
- Category
- Article
- ISSN
- 0042-207X
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