✦ LIBER ✦
On the fatigue crack growth analysis of spliced aircraft wing panels under sequential axial and shear loads
✍ Scribed by Yu, Xiaobo
- Book ID
- 121674962
- Publisher
- Elsevier Science
- Year
- 2014
- Tongue
- English
- Weight
- 1023 KB
- Volume
- 123
- Category
- Article
- ISSN
- 0013-7944
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