Multi-crack panel type aluminum specimens were tested under constant amplitude loading, constant amplitude with superimposed overloads loading and random variable amplitude load history. A numerical procedure of real-time generation of a truncated and condensed random load history corresponding to a
β¦ LIBER β¦
Analysis of short fatigue crack growth in cast aluminum alloys
β Scribed by S Ishihara; A.J McEvily
- Book ID
- 108401179
- Publisher
- Elsevier Science
- Year
- 2002
- Tongue
- English
- Weight
- 131 KB
- Volume
- 24
- Category
- Article
- ISSN
- 0142-1123
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