GOE 389 AIRFOIL 17. 17. 0.000000 0.000000 0.012150 0.017140 0.024440 0.027990 0.049150 0.042190 0.073930 0.053290 0.098770 0.061190 0.148500 0.074390 0.198320 0.083300 0.298170 0.090610 0.398220 0.088420 0.498390 0.082170 0.598540 0.072360 0.698840 0.057480 0.799160 0.041500 0.899550 0.022330 0.949740 0.012740 1.000000 0.001050 0.000000 0.000000 0.012750 -0.012440 0.025310 -0.015390 0.050360 -0.017990 0.075370 -0.018580 0.100390 -0.019180 0.150370 -0.018670 0.200350 -0.017160 0.300250 -0.012550 0.400180 -0.008940 0.500120 -0.005820 0.600060 -0.002810 0.700040 -0.001790 0.800030 -0.001380 0.900020 -0.000960 0.950020 -0.000960 1.000000 -0.001050