Abstract
To investigate the performance of a cyclone filter for hot gas generator of a missile system, the cold-flow experimental and numerical simulation were given. The IPSA algorithm based on multi-fluid model was used for the numerical simulation of three-dimensional two-phase flow in the cyclone filter. The calculations agree well with the experimental data, the separation limited diameter from calculation is about 2μm-3μm.
| Original language | English |
|---|---|
| Pages (from-to) | 138-140 |
| Number of pages | 3 |
| Journal | Tuijin Jishu/Journal of Propulsion Technology |
| Volume | 24 |
| Issue number | 2 |
| Publication status | Published - Apr 2003 |
Keywords
- Cold flow test
- Filter
- Gas generator
- Internal aerodynamic
- Numerical simulation