GOE 507 AIRFOIL 13. 13. 0.000000 0.000000 0.025000 0.024140 0.050000 0.033780 0.100000 0.048050 0.200000 0.064100 0.300000 0.070650 0.400000 0.071200 0.500000 0.067250 0.600000 0.060300 0.700000 0.048850 0.800000 0.033900 0.900000 0.016950 1.000000 0.000000 0.000000 0.000000 0.025000 -0.017860 0.050000 -0.021220 0.100000 -0.023450 0.200000 -0.019900 0.300000 -0.015850 0.400000 -0.012800 0.500000 -0.010250 0.600000 -0.008700 0.700000 -0.007150 0.800000 -0.005600 0.900000 -0.003050 1.000000 0.000000