Table 5 Sectional data of each airfoil under different schemes.
r(i) | β(°) | gmax/l | δmax/l |
---|---|---|---|
1.0 | 15.81 | 0.027 | 0.025 |
0.937 | 18.18 | 0.028 | 0.031 |
0.874 | 20.56 | 0.030 | 0.036 |
0.811 | 23.02 | 0.033 | 0.043 |
0.748 | 25.63 | 0.036 | 0.050 |
0.685 | 28.47 | 0.040 | 0.058 |
0.622 | 31.64 | 0.046 | 0.067 |
0.559 | 35.28 | 0.052 | 0.077 |
0.496 | 39.62 | 0.058 | 0.089 |
0.433 | 44.97 | 0.065 | 0.010 |
0.367 | 51.3 | 0.073 | 0.012 |