NACA M17 AIRFOIL 17. 17. 0.000000 0.000000 0.012530 0.015570 0.025050 0.023450 0.050070 0.035800 0.075090 0.045650 0.100110 0.053590 0.150130 0.065090 0.200150 0.073190 0.300170 0.081480 0.400160 0.079880 0.500150 0.071070 0.600120 0.057670 0.700090 0.042460 0.800060 0.026860 0.900030 0.012950 0.950010 0.007050 1.000000 0.002050 0.000000 0.000000 0.012480 -0.010430 0.024980 -0.011550 0.049980 -0.011000 0.074980 -0.009450 0.099980 -0.007500 0.149990 -0.004110 0.200000 -0.001410 0.300000 0.000780 0.400000 -0.000920 0.499990 -0.004620 0.599980 -0.009630 0.699970 -0.012330 0.799970 -0.013040 0.899980 -0.010140 0.949990 -0.006750 1.000000 -0.002050