GOE 565 AIRFOIL 16. 16. 0.000000 0.000000 0.012500 0.016630 0.025000 0.023450 0.050000 0.034110 0.075000 0.041760 0.100000 0.047920 0.150000 0.055730 0.200000 0.061540 0.300000 0.067160 0.400000 0.067780 0.500000 0.064400 0.600000 0.058020 0.700000 0.047640 0.800000 0.034760 0.900000 0.018380 1.000000 0.000000 0.000000 0.000000 0.012500 -0.011370 0.025000 -0.015540 0.050000 -0.018390 0.075000 -0.020230 0.100000 -0.020580 0.150000 -0.021270 0.200000 -0.020960 0.300000 -0.016840 0.400000 -0.012720 0.500000 -0.008600 0.600000 -0.004480 0.700000 -0.001360 0.800000 -0.000740 0.900000 -0.000120 1.000000 0.000000