NACA-M1 AIRFOIL 17. 17. 0.000000 0.000000 0.012500 0.010300 0.025000 0.013600 0.050000 0.018000 0.075000 0.021000 0.100000 0.023400 0.150000 0.026700 0.200000 0.028800 0.300000 0.030800 0.400000 0.030500 0.500000 0.028500 0.600000 0.025300 0.700000 0.020800 0.800000 0.015400 0.900000 0.009100 0.950000 0.005700 1.000000 0.002000 0.000000 0.000000 0.012500 -0.010300 0.025000 -0.013600 0.050000 -0.018000 0.075000 -0.021000 0.100000 -0.023400 0.150000 -0.026700 0.200000 -0.028800 0.300000 -0.030800 0.400000 -0.030500 0.500000 -0.028500 0.600000 -0.025300 0.700000 -0.020800 0.800000 -0.015400 0.900000 -0.009100 0.950000 -0.005700 1.000000 -0.002000