GOE 548 AIRFOIL 17. 17. 0.000000 0.000000 0.012500 0.013800 0.025000 0.022100 0.050000 0.035200 0.075000 0.043300 0.100000 0.050400 0.150000 0.060600 0.200000 0.068300 0.300000 0.078700 0.400000 0.081600 0.500000 0.079000 0.600000 0.071900 0.700000 0.059550 0.800000 0.045200 0.900000 0.024000 0.950000 0.013300 1.000000 0.000000 0.000000 0.000000 0.012500 -0.012200 0.025000 -0.017400 0.050000 -0.023300 0.075000 -0.028200 0.100000 -0.031600 0.150000 -0.036400 0.200000 -0.038700 0.300000 -0.039800 0.400000 -0.037400 0.500000 -0.033000 0.600000 -0.027100 0.700000 -0.020700 0.800000 -0.013800 0.900000 -0.006900 0.950000 -0.003700 1.000000 0.000000