✦ LIBER ✦
Method for reducing the fatigue crack growth rate of cracks in the aluminium alloy fuselage skin of an aircraft structure: Parker, E.R. and Parker, W.J. US Patent 5071492 (10 Dec 1991)
- Book ID
- 107891468
- Publisher
- Elsevier Science
- Year
- 1992
- Tongue
- English
- Weight
- 201 KB
- Volume
- 14
- Category
- Article
- ISSN
- 0142-1123
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