A fatigue test program was conducted to investigate m&i-site damage of commerical wide-bodied aircraft fuselage lap joints. Crack growth data were generated using specimens representative of a typical lap joint. It was also demonstrated that a boron/epoxy composite doubler, bonded over the joint, co
โฆ LIBER โฆ
Probabilistic analysis of multi-site damage in aircraft fuselages
โ Scribed by C. Proppe
- Book ID
- 106157865
- Publisher
- Springer
- Year
- 2003
- Tongue
- English
- Weight
- 297 KB
- Volume
- 30
- Category
- Article
- ISSN
- 0178-7675
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