NACA 64-215 AIRFOIL 26. 26. 0.000000 0.000000 0.003990 0.012540 0.006370 0.015220 0.011220 0.019450 0.023530 0.027100 0.048360 0.038160 0.073310 0.046610 0.098310 0.053560 0.148400 0.064560 0.198570 0.072740 0.248780 0.078790 0.299010 0.082900 0.349260 0.085120 0.399520 0.085440 0.449770 0.083190 0.500000 0.079130 0.550200 0.073610 0.600360 0.066910 0.650480 0.059250 0.700550 0.050850 0.750580 0.041910 0.800550 0.032670 0.850460 0.023490 0.900330 0.014660 0.950160 0.006620 1.000000 0.000000 0.000000 0.000000 0.006010 -0.011540 0.008630 -0.013820 0.013780 -0.017310 0.026470 -0.023380 0.051640 -0.031840 0.076690 -0.038130 0.101690 -0.043220 0.151600 -0.051100 0.201430 -0.056820 0.251220 -0.060890 0.300990 -0.063460 0.350740 -0.064520 0.400480 -0.064020 0.450230 -0.061290 0.500000 -0.057070 0.549800 -0.051710 0.599640 -0.045490 0.649520 -0.038650 0.699450 -0.031410 0.749420 -0.024010 0.799450 -0.016750 0.849540 -0.010030 0.899670 -0.004320 0.949840 -0.000300 1.000000 0.000000