Abstract
In this paper, typical multi-element airfoil is optimized by aerodynamic optimization system based on MADS method and chimera technology, some design variables such as gap, and overlap are optimized to get excellent aerodynamic characteristic. The results show that the aerodynamic optimization system has high optimization efficient and computational precision.
| Original language | English |
|---|---|
| Pages (from-to) | 405-409 |
| Number of pages | 5 |
| Journal | Kongqi Donglixue Xuebao/Acta Aerodynamica Sinica |
| Volume | 28 |
| Issue number | 4 |
| State | Published - Aug 2010 |
Keywords
- Chimera technology
- MADS method
- Mesh size
- Optimization of multi-element airfoil
- Positive bases