S102B Airfoil

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

DOWNLOAD FROM HERE

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