Please use this identifier to cite or link to this item:
https://www.um.edu.mt/library/oar/handle/123456789/88866| Title: | Finite element modelling of foam filled sandwich panels subjected to quasi-static low-velocity impact |
| Authors: | Vella, Rudie De Marco Muscat-Fenech, Claire Mollicone, Pierluigi |
| Keywords: | Composite construction Laminated materials Sandwich construction Metals -- Testing Materials science Materials -- Mechanical properties Strength of materials |
| Issue Date: | 2014 |
| Publisher: | CAE |
| Citation: | Vella, R., De Marco Muscat-Fenech, C., & Mollicone, P. (2014). Finite element modelling of foam filled sandwich panels subjected to quasi-static low-velocity impact. International CAE Conference, Pacengo del Garda (Verona), Italy, October 27-29, 2014. |
| Abstract: | Composite sandwich panels provide superior stiffness-to-weight ratios when compared to composite laminates due to the sandwich effect. The sandwich effect describes the increase of the second moment of area of a structure by sandwiching a lightweight and high shear modulus core between two high in-plane elastic modulus and low shear modulus skin. |
| URI: | https://www.um.edu.mt/library/oar/handle/123456789/88866 |
| Appears in Collections: | Scholarly Works - FacEngME |
Files in This Item:
| File | Description | Size | Format | |
|---|---|---|---|---|
| 16 FEA modelling of Foam filled sandwichpanels subjected to QSLVI CAE2014.pdf Restricted Access | 98.53 kB | Adobe PDF | View/Open Request a copy |
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