S102S Airfoil

Dan Somers airfoil for the Toyota general aviation airplane

S102S 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
0.92221 0.01865
0.94818 0.0122
0.96965 0.00672
0.98603 0.00278
0.99642 0.00062
1 0
0.99636 0.00034
0.98544 0.00115
0.96734 0.00199
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

S102S Airfoil CAD files

DOWNLOAD FROM HERE

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