Abstract
Since composite sandwich structures are susceptible to low-velocity impact damage, a thorough characterization of the loading and damage process during impact is important. In the present paper, the low-velocity impact response of carbon fiber composites lattice structures is investigated by experimental and numerical methods. Impact tests on composite plates are performed using an instrumented drop-weight machine (Instron 9250HV) and a new damage mode is observed. A three-dimensional finite element model is built by ABAQUS/Explicit and user subroutine (VUMAT) to predict the peak loading and simulate the complicated damage problem. The numerical predictions are in good agreement with the experimental results.
| Original language | English |
|---|---|
| Pages (from-to) | 801-805 |
| Number of pages | 5 |
| Journal | Journal of Harbin Institute of Technology (New Series) |
| Volume | 17 |
| Issue number | 6 |
| State | Published - Dec 2010 |
Keywords
- Composites lattice core
- Damage mode
- Low-velocity impact
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