NACA 64-012A AIRFOIL 1.000000 0.000250 0.950000 0.006440 0.900000 0.012630 0.850000 0.018820 0.800000 0.025000 0.750000 0.031180 0.700000 0.037210 0.650000 0.042890 0.600000 0.048010 0.550000 0.052440 0.500000 0.056050 0.450000 0.058630 0.400000 0.059930 0.350000 0.059650 0.300000 0.058090 0.250000 0.055340 0.200000 0.051320 0.150000 0.045800 0.100000 0.038390 0.075000 0.033640 0.050000 0.027880 0.025000 0.020180 0.012500 0.014640 0.007500 0.011580 0.005000 0.009610 0.000000 0.000000 0.005000 -0.009610 0.007500 -0.011580 0.012500 -0.014640 0.025000 -0.020180 0.050000 -0.027880 0.075000 -0.033640 0.100000 -0.038390 0.150000 -0.045800 0.200000 -0.051320 0.250000 -0.055340 0.300000 -0.058090 0.350000 -0.059650 0.400000 -0.059930 0.450000 -0.058630 0.500000 -0.056050 0.550000 -0.052440 0.600000 -0.048010 0.650000 -0.042890 0.700000 -0.037210 0.750000 -0.031180 0.800000 -0.025000 0.850000 -0.018820 0.900000 -0.012630 0.950000 -0.006440 1.000000 -0.000250