NACA 63-210 AIRFOIL 26. 26. 0.000000 0.000000 0.004300 0.008760 0.006690 0.011070 0.011620 0.013790 0.023980 0.019390 0.048860 0.027530 0.073820 0.033720 0.098820 0.038770 0.148900 0.046650 0.199020 0.052400 0.249170 0.056470 0.299330 0.059100 0.349510 0.060300 0.399680 0.060090 0.449850 0.058610 0.500000 0.055990 0.550130 0.052350 0.600240 0.047860 0.650320 0.042640 0.700360 0.036840 0.750380 0.030610 0.800360 0.024140 0.850300 0.017610 0.900210 0.012120 0.950100 0.005300 1.000000 0.000000 0.000000 0.000000 0.005700 -0.007760 0.008310 -0.009670 0.013380 -0.011650 0.026020 -0.015670 0.051140 -0.021210 0.076180 -0.025240 0.101180 -0.028430 0.151100 -0.033190 0.200980 -0.036480 0.250830 -0.038570 0.300670 -0.039660 0.350490 -0.039700 0.400320 -0.038670 0.450150 -0.036710 0.500000 -0.033930 0.549870 -0.030450 0.589760 -0.026440 0.649680 -0.022040 0.699640 -0.017400 0.749620 -0.012710 0.799640 -0.008220 0.849700 -0.004150 0.899790 -0.000870 0.949900 0.001200 1.000000 0.000000