a63a108c Airfoil

NASA/AMES modification of the NACA 63A-108 airfoil

a63a108c Airfoil (x,y) Co-ordinates

0 0
0.0002 0.00445
0.0004 0.00549
0.0006 0.00626
0.0008 0.00687
0.001 0.00741
0.002 0.00943
0.003 0.01091
0.004 0.01212
0.005 0.01315
0.01 0.01695
0.02 0.02192
0.03 0.02539
0.04 0.02807
0.05 0.03024
0.06 0.03206
0.07 0.0336
0.08 0.03493
0.09 0.03608
0.1 0.03709
0.125 0.03911
0.15 0.04062
0.175 0.04173
0.2 0.04255
0.25 0.04351
0.3 0.04385
0.35 0.04362
0.4 0.04293
0.45 0.04176
0.5 0.04015
0.55 0.0381
0.6 0.03559
0.65 0.03258
0.7 0.02906
0.725 0.0272
0.75 0.0252
0.775 0.0231
0.8 0.0209
0.825 0.0187
0.85 0.0164
0.875 0.0141
0.9 0.012
0.925 0.0101
0.95 0.0086
0.96 0.008
0.97 0.0076
0.98 0.0073
0.99 0.0071
0.995 0.007
1 0.007
1 0
0.995 -0.00029
0.99 -0.00059
0.98 -0.00117
0.97 -0.00176
0.96 -0.00234
0.95 -0.00292
0.925 -0.00438
0.9 -0.00584
0.875 -0.00729
0.85 -0.00874
0.825 -0.01018
0.8 -0.01167
0.775 -0.01327
0.75 -0.01492
0.725 -0.01661
0.7 -0.0183
0.65 -0.02157
0.6 -0.02459
0.55 -0.02728
0.5 -0.02957
0.45 -0.0314
0.4 -0.03269
0.35 -0.0334
0.3 -0.0335
0.25 -0.03297
0.2 -0.03183
0.175 -0.03097
0.15 -0.02989
0.125 -0.02852
0.1 -0.0268
0.09 -0.02598
0.08 -0.02506
0.07 -0.02403
0.06 -0.02286
0.05 -0.02152
0.04 -0.01996
0.03 -0.01808
0.02 -0.01569
0.01 -0.01228
0.005 -0.00959
0.004 -0.00885
0.003 -0.00796
0.002 -0.00686
0.001 -0.00531
0.0008 -0.00489
0.0006 -0.0044
0.0004 -0.00379
0.0002 -0.00277
0 0

a63a108c Airfoil CAD files

DOWNLOAD FROM HERE

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