Abstract
In this paper, thermomechanical coupled analysis of carbon/phenolic composites structures in reentry environment was performed. The interface of thermomechanical coupled analysis was constructed using commercial software. The governing equations of temperature and displacement fields were considered to simulate change of physical behavior due to pyrolysis and ablation effects. The results of thermomechanical coupled analysis were compared with the results of ablation test using arc-heated wind tunnel. Also, the structural stability of reentry capsule was analyzed using the analysis interface. The excellent ablation characteristics and thermal protection effects of the carbon/phenolic composites were confirmed and the constructed analysis interface can be effectively used to perform thermal protection system design.
| Original language | English |
|---|---|
| Pages (from-to) | 414-421 |
| Number of pages | 8 |
| Journal | Journal of the Korean Society for Aeronautical and Space Sciences |
| Volume | 47 |
| Issue number | 6 |
| DOIs | |
| State | Published - 2019.06 |
Keywords
- Ablation
- Carbon/phenolic Composites
- Thermal Protection System
- Thermomechanical Coupled Analysis
Quacquarelli Symonds(QS) Subject Topics
- Engineering - Mechanical
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