GOE 501 AIRFOIL 17. 17. 0.000000 0.000000 0.012500 0.027370 0.025000 0.039240 0.050000 0.055480 0.075000 0.068210 0.100000 0.078950 0.150000 0.093420 0.200000 0.105400 0.300000 0.118850 0.400000 0.120300 0.500000 0.114250 0.600000 0.103200 0.700000 0.084150 0.800000 0.060600 0.900000 0.032050 0.950000 0.015530 1.000000 0.000000 0.000000 0.000000 0.012500 -0.014630 0.025000 -0.020260 0.050000 -0.024530 0.075000 -0.025690 0.100000 -0.026550 0.150000 -0.024080 0.200000 -0.020100 0.300000 -0.009150 0.400000 0.002800 0.500000 0.011750 0.600000 0.018700 0.700000 0.021150 0.800000 0.018600 0.900000 0.011550 0.950000 0.006520 1.000000 0.000000