NACA 63-015A AIRFOIL 26. 26. 0.000000 0.000000 0.005000 0.012030 0.007500 0.014480 0.012500 0.018440 0.025000 0.025790 0.050000 0.036180 0.075000 0.043820 0.100000 0.049970 0.150000 0.059420 0.200000 0.066190 0.250000 0.070910 0.300000 0.073840 0.350000 0.074960 0.400000 0.074350 0.450000 0.072150 0.500000 0.068580 0.550000 0.063870 0.600000 0.058200 0.650000 0.051730 0.700000 0.044680 0.750000 0.037310 0.800000 0.029910 0.850000 0.022520 0.900000 0.015120 0.950000 0.007720 1.000000 0.000320 0.000000 0.000000 0.005000 -0.012030 0.007500 -0.014480 0.012500 -0.018440 0.025000 -0.025790 0.050000 -0.036180 0.075000 -0.043820 0.100000 -0.049970 0.150000 -0.059420 0.200000 -0.066190 0.250000 -0.070910 0.300000 -0.073840 0.350000 -0.074960 0.400000 -0.074350 0.450000 -0.072150 0.500000 -0.068580 0.550000 -0.063870 0.600000 -0.058200 0.650000 -0.051730 0.700000 -0.044680 0.750000 -0.037310 0.800000 -0.029910 0.850000 -0.022520 0.900000 -0.015120 0.950000 -0.007720 1.000000 -0.000320