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Numerical and experimental study on stability of aluminium alloy riveted and stiffened panels under in-plane shear
| Content Provider | Scilit |
|---|---|
| Copyright Year | 2017 |
| Description | The manufacturing defects, contact and damage problems are inevitable, which need to be considered in the nonlinear FEM analysis. Anyfantis et al. (2012) studied the progressive post-buckling and the final failure response of stiffened composite panels based on the structural nonlinear FEM. Orifici et al. (2008) combined the post-buckling deformations and several composite damage mechanisms to successfully predict the damage growth and collapse behaviour of composite stiffened structures under compression. The buckling behavior influenced by the type of stiffeners, panel orthotropic ratio, tensile stiffness and shear stiffness ratios of stiffener and skin (Jain, 2010). Book Name: Civil, Architecture and Environmental Engineering |
| Related Links | https://content.taylorfrancis.com/books/download?dac=C2016-0-00067-4&isbn=9781315226187&doi=10.1201/9781315226187-96&format=pdf |
| Ending Page | 561 |
| Page Count | 4 |
| Starting Page | 558 |
| DOI | 10.1201/9781315226187-96 |
| Language | English |
| Publisher | Informa UK Limited |
| Publisher Date | 2017-04-24 |
| Access Restriction | Open |
| Subject Keyword | Book Name: Civil, Architecture and Environmental Engineering Mechanics Behavior Stiffness Nonlinear Buckling Structural Panels Stiffened |
| Content Type | Text |
| Resource Type | Chapter |