Abstract
Inlet start/unstart detection is one of the most important issues of hypersonic inlet and is also the foundation of inlet protection control. To solve this problem, the 2-D inner steady flow of hypersonic inlet at different flow conditions and back pressures was numerically simulated. The sensor location reduction to the inlet by using rough set algorithm was presented. The judgment criterion of hypersonic inlet start/unstart was given and the inner physical mechanism was analyzed. The judgment criterion was validated by the else simulation data, the result proves the validity.
| Original language | English |
|---|---|
| Pages (from-to) | 136-140 |
| Number of pages | 5 |
| Journal | Yuhang Xuebao/Journal of Astronautics |
| Volume | 27 |
| Issue number | SUPPL. |
| State | Published - Dec 2006 |
| Externally published | Yes |
Keywords
- Classification criterion
- Hypersonic inlet
- Rough set
- Unstart
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