Damage tolerance analysis of aircraft reinforced panels
This work is aimed at reproducing numerically a campaign of experimental tests performed for the development of reinforced panels, typically found in aircraft fuselage. The bonded reinforcements can significantly reduce the rate of fatigue crack growth and increase the residual strength of the skin....
| Main Authors: | , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
Gruppo Italiano Frattura
2013-04-01
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| Series: | Frattura ed Integrità Strutturale |
| Online Access: | https://212.237.37.202/index.php/fis/article/view/113 |
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