Table 3 Comparison of the lift and drag coefficients between the different spatial resolutions at α=5 deg and α=10 deg
From: Aerodynamic analysis of a generic wing featuring an elasto-flexible lifting surface
- | Coarse | Medium | Fine |
|---|---|---|---|
CL at α=5 deg | 0.519 ±0.027 | 0.516 | 0.515 |
CD at α=5 deg | 0.032 ±0.003 | 0.029 | 0.029 |
CL at α=10 deg | 0.906 ±0.026 | 0.898 | 0.897 |
CD at α=10 deg | 0.066 ±0.005 | 0.063 | 0.062 |