NACA M13 AIRFOIL 17. 17. 0.000000 0.000000 0.012500 0.012780 0.025000 0.019370 0.050000 0.029640 0.075000 0.037910 0.100000 0.044680 0.150000 0.055420 0.200000 0.062760 0.300000 0.070140 0.400000 0.069420 0.500000 0.063600 0.600000 0.053780 0.700000 0.041860 0.800000 0.029240 0.900000 0.016420 0.950000 0.010560 1.000000 0.004400 0.000000 0.000000 0.012500 -0.008120 0.025000 -0.008130 0.050000 -0.007910 0.075000 -0.004390 0.100000 -0.002220 0.150000 0.001920 0.200000 0.005060 0.300000 0.008040 0.400000 0.007720 0.500000 0.005500 0.600000 0.002280 0.700000 -0.000640 0.800000 -0.002260 0.900000 -0.002280 0.950000 -0.001440 1.000000 0.000000