Abstract
Impact behavior of sandwich panels with auxetic and hexagonal honeycomb cores are investigated experimentally and numerically. Re-entrant and anti-tetrachiral geometries are considered for auxetic cores. In the experimental side of the study, auxetic and honeycomb cores are produced using a 3D printer. The sandwich panels are then produced by attaching aluminium face sheets and cores. The impact tests are performed using a particle impact test system. The numerical analyses are achieved by using LS-DYNA finite element software. The deformation results are compared and the effect of having different type of core is evaluated.
Original language | English |
---|---|
Title of host publication | 2019 9th International Conference on Recent Advances in Space Technologies (RAST) |
Publisher | Institute of Electrical and Electronics Engineers Inc. |
Pages | 69-72 |
Number of pages | 4 |
ISBN (Electronic) | 978-1-5386-9448-0 |
ISBN (Print) | 978-1-5386-9449-7 |
DOIs | |
Publication status | Published - 22 Jul 2019 |
Event | 2019 9th International Conference on Recent Advances in Space Technologies (RAST) - Istanbul, Turkey Duration: 11 Jun 2019 → 14 Jun 2019 https://ieeexplore.ieee.org/xpl/conhome/8760338/proceeding |
Conference
Conference | 2019 9th International Conference on Recent Advances in Space Technologies (RAST) |
---|---|
Country/Territory | Turkey |
City | Istanbul |
Period | 11/06/2019 → 14/06/2019 |
Internet address |