Table 3 Depending on the unique effect of the co-flow jet technology on the aerodynamic characteristics of the airfoil, the design variables at different locations on the upper surface are taken at different values from experience
P (W) | Static pressure (Pa) | veloctiy (m/s) | ||||
|---|---|---|---|---|---|---|
10 | 20 | 30 | 10 | 20 | 30 | |
\({{\alpha }\,(^{\circ })}\) | ||||||
0 | 97,761 | 97,738 | 97,721 | 8.79 | 10.77 | 12.02 |
2 | 97,756 | 97,732 | 97,717 | 9.25 | 11.23 | 12.30 |
4 | 97,751 | 97,727 | 97,709 | 9.78 | 11.59 | 12.84 |
6 | 97,747 | 97,721 | 97,699 | 9.95 | 12.02 | 13.48 |
8 | 97,740 | 97,710 | 97,693 | 10.61 | 12.77 | 14.15 |
10 | 97,732 | 97,703 | 97,685 | 11.23 | 13.22 | 14.32 |