Abstract
Flying aerodynamic heating makes great effect on the reliability of nose fuze. The computational model of air boundary layer of rocket fuze was established. Considering different material characteristics, correlative mathematic model was built by finite element analysis. The simulation was conducted by Fluent software. The simulation results show that the method possesses high accuracy and lays the foundation for thermal supervision of nose fuze.
| Original language | English |
|---|---|
| Pages (from-to) | 406-410 |
| Number of pages | 5 |
| Journal | Binggong Xuebao/Acta Armamentarii |
| Volume | 28 |
| Issue number | 4 |
| Publication status | Published - Apr 2007 |
Keywords
- Finite element method
- Fuze
- Thermal characteristic simulation
- Thermology