Dillner 20-32-C low Reynolds number airfoil
2032c Airfoil (x,y) Co-ordinates
0 | 0 |
0.0125 | 0.0193 |
0.025 | 0.0317 |
0.05 | 0.0513 |
0.075 | 0.0664 |
0.1 | 0.078 |
0.15 | 0.0934 |
0.2 | 0.1013 |
0.25 | 0.1044 |
0.3 | 0.1048 |
0.4 | 0.1002 |
0.5 | 0.0905 |
0.6 | 0.0771 |
0.7 | 0.061 |
0.8 | 0.0428 |
0.9 | 0.0229 |
0.95 | 0.0124 |
1 | 0.0016 |
1 | -0.0016 |
0.95 | 0.0044 |
0.9 | 0.01 |
0.8 | 0.0202 |
0.7 | 0.0286 |
0.6 | 0.035 |
0.5 | 0.0386 |
0.4 | 0.0385 |
0.3 | 0.0333 |
0.25 | 0.0282 |
0.2 | 0.0217 |
0.15 | 0.0145 |
0.1 | 0.0068 |
0.075 | 0.0028 |
0.05 | -0.001 |
0.025 | -0.0042 |
0.0125 | -0.005 |
0 | 0 |
2032c Airfoil CAD files