Abstract
The dynamic response of laminated plates subjected to the localised air blast loading is investigated numerically. In-plane stiffness and inertia effects are considered when formulating the dynamic response of the laminated composite plate subjected to the localised blast loading. The geometric nonlinearity effects are also taken into account by using the von Kármán large deflection theory of thin plates. The effect of the magnitude and localization of the air blast load on the dynamic response is investigated. The displacement-time histories are obtained and compared with the ones obtained by using a commercial finite element code ANSYS. The results are found to be in an agreement.
| Original language | English |
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| Title of host publication | Proceedings of the 10th International Conference on Computational Structures Technology, CST 2010 |
| Publisher | Civil-Comp Press |
| Volume | 93 |
| ISBN (Print) | 9781905088386 |
| Publication status | Published - 2010 |
| Event | 10th International Conference on Computational Structures Technology, CST 2010 - Valencia, Spain Duration: 14 Sept 2010 → 17 Sept 2010 |
Conference
| Conference | 10th International Conference on Computational Structures Technology, CST 2010 |
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| Country/Territory | Spain |
| City | Valencia |
| Period | 14/09/10 → 17/09/10 |
Keywords
- Blast loading
- Dynamic response
- Laminated plate
- Large deflection
- Localised blast
- Nonlinear