Dan Somers airfoil for the Toyota general aviation airplane
S102B Airfoil (x,y) Co-ordinates
| 0.00001 | 0.00039 |
| 0.00017 | 0.00217 |
| 0.00357 | 0.01122 |
| 0.01117 | 0.02128 |
| 0.02281 | 0.0316 |
| 0.03845 | 0.04166 |
| 0.05803 | 0.05091 |
| 0.08181 | 0.05887 |
| 0.11019 | 0.06562 |
| 0.14297 | 0.07163 |
| 0.17954 | 0.07704 |
| 0.21937 | 0.08178 |
| 0.26191 | 0.08578 |
| 0.30662 | 0.08892 |
| 0.35296 | 0.09109 |
| 0.40037 | 0.09215 |
| 0.44828 | 0.09194 |
| 0.49614 | 0.09013 |
| 0.54379 | 0.0862 |
| 0.59159 | 0.08025 |
| 0.63946 | 0.07299 |
| 0.68678 | 0.06502 |
| 0.7329 | 0.05672 |
| 0.77715 | 0.04842 |
| 0.81885 | 0.04036 |
| 0.85732 | 0.03272 |
| 0.89191 | 0.02553 |
| 0.92409 | 0.01864 |
| 0.95097 | 0.01279 |
| 1 | 0 |
| 0.94228 | 0.00238 |
| 0.91073 | 0.0018 |
| 0.87343 | -0.00018 |
| 0.83135 | -0.00377 |
| 0.78548 | -0.009 |
| 0.73682 | -0.01572 |
| 0.68645 | -0.02371 |
| 0.63544 | -0.03252 |
| 0.58486 | -0.04152 |
| 0.5357 | -0.04955 |
| 0.48787 | -0.05495 |
| 0.44011 | -0.05736 |
| 0.39208 | -0.05776 |
| 0.34441 | -0.05678 |
| 0.29769 | -0.05467 |
| 0.2525 | -0.05166 |
| 0.20943 | -0.04791 |
| 0.16902 | -0.04357 |
| 0.1318 | -0.03876 |
| 0.0983 | -0.03357 |
| 0.06896 | -0.02811 |
| 0.04424 | -0.02243 |
| 0.02452 | -0.0166 |
| 0.01018 | -0.01065 |
| 0.003 | -0.006 |
| 0.00151 | -0.00454 |
| 0.00054 | -0.00308 |
| 0.00009 | -0.00147 |
| 0.00001 | 0.00039 |
S102B Airfoil CAD files