Table 2 The value of the drag force at different grid numbers
From: Mathematical modeling of the aerodynamic coefficients of a sail blade
u (m/s) | Fdf at C1 | Fdf at C2 | Fdf at C3 |
|---|---|---|---|
3 | 0.62 | 0.5 | 0.52 |
5 | 1.35 | 1.2 | 1.24 |
7 | 1.75 | 1.95 | 1.98 |
9 | 2.45 | 2.75 | 2.77 |
12 | 3.71 | 3.82 | 3.85 |
15 | 5.01 | 5.15 | 5.19 |