NREL's S806A Airfoil (modified line 35) 1.000000 0.000000 0.979980 0.006770 0.959950 0.009400 0.939940 0.012060 0.919940 0.014840 0.900000 0.017950 0.850000 0.027910 0.800000 0.038130 0.750000 0.048530 0.700020 0.058740 0.650030 0.067950 0.600020 0.075320 0.550010 0.080580 0.500000 0.083720 0.450000 0.084960 0.400000 0.084640 0.350000 0.082930 0.299990 0.079850 0.249990 0.075350 0.199980 0.069240 0.149990 0.061200 0.119980 0.055200 0.099960 0.050550 0.079970 0.045240 0.060000 0.039050 0.049920 0.035480 0.039990 0.031540 0.029900 0.026950 0.019900 0.021610 0.009980 0.014700 0.002710 0.006910 0.000000 0.000000 0.000000 -0.000210 0.002970 -0.005500 0.010020 -0.008890 0.019970 -0.011590 0.029980 -0.013770 0.039980 -0.015330 0.050000 -0.016590 0.059990 -0.017720 0.079990 -0.019650 0.100000 -0.021200 0.120000 -0.022520 0.150000 -0.024190 0.200000 -0.026340 0.250000 -0.027920 0.300000 -0.029030 0.350000 -0.029710 0.400000 -0.030000 0.450000 -0.029930 0.500000 -0.029490 0.550000 -0.028670 0.600000 -0.027450 0.650000 -0.025750 0.700010 -0.023400 0.750010 -0.020210 0.800000 -0.016210 0.850000 -0.011660 0.900000 -0.006860 0.919980 -0.005920 0.939980 -0.005400 0.959990 -0.005000 0.980000 -0.004620 1.000000 0.000000