n0009sm Airfoil

NACA 0009 airfoil (smoothed)

n0009sm Airfoil (x,y) Co-ordinates

1 0
0.99572 0.00057
0.98296 0.00218
0.96194 0.00463
0.93301 0.0077
0.89668 0.01127
0.85355 0.01522
0.80438 0.01945
0.75 0.02384
0.69134 0.02823
0.62941 0.03247
0.56526 0.03638
0.5 0.03978
0.43474 0.04248
0.37059 0.04431
0.33928 0.04484
0.30866 0.04509
0.27886 0.04504
0.25 0.04466
0.22221 0.04397
0.19562 0.04295
0.17033 0.04161
0.14645 0.03994
0.12408 0.03795
0.10332 0.03564
0.08427 0.03305
0.06699 0.03023
0.05156 0.0272
0.03806 0.02395
0.02653 0.02039
0.01704 0.01646
0.00961 0.01214
0.00428 0.00767
0.00107 0.00349
0 0
0.00107 -0.00349
0.00428 -0.00767
0.00961 -0.01214
0.01704 -0.01646
0.02653 -0.02039
0.03806 -0.02395
0.05156 -0.0272
0.06699 -0.03023
0.08427 -0.03305
0.10332 -0.03564
0.12408 -0.03795
0.14645 -0.03994
0.17033 -0.04161
0.19562 -0.04295
0.22221 -0.04397
0.25 -0.04466
0.27886 -0.04504
0.30866 -0.04509
0.33928 -0.04484
0.37059 -0.04431
0.43474 -0.04248
0.5 -0.03978
0.56526 -0.03638
0.62941 -0.03247
0.69134 -0.02823
0.75 -0.02384
0.80438 -0.01945
0.85355 -0.01522
0.89668 -0.01127
0.93301 -0.0077
0.96194 -0.00463
0.98296 -0.00218
0.99572 -0.00057
1 0

n0009sm Airfoil CAD files

DOWNLOAD FROM HERE

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