Fatigue-crack propagation data have been obtained for a variety of aluminum alloys. tempers, and products in relatively thick sections of interest for large aircraft shapes. For the higher stress-intensity ranges. the alloys rate in about the same order with regard to resistance to fatigue crack pro
โฆ LIBER โฆ
Some aspects of variability in fatigue crack initiation and propagation in thick aluminium alloy sections
โ Scribed by J.Y. Mann; R.A. Pell; A.S. Machin
- Publisher
- Elsevier Science
- Year
- 1986
- Tongue
- English
- Weight
- 758 KB
- Volume
- 8
- Category
- Article
- ISSN
- 0142-1123
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