GOE 404 AIRFOIL 17. 17. 0.000000 0.000000 0.011530 0.031260 0.023570 0.045930 0.048020 0.063690 0.072600 0.077260 0.097290 0.087130 0.146880 0.100370 0.196590 0.109810 0.296400 0.115620 0.396560 0.110730 0.496870 0.100550 0.597350 0.085080 0.697920 0.066910 0.798530 0.047230 0.899250 0.024270 0.949610 0.012530 1.000000 0.000800 0.000000 0.000000 0.013150 -0.020890 0.025800 -0.025800 0.050930 -0.029820 0.075920 -0.029540 0.100860 -0.027660 0.150750 -0.024010 0.200630 -0.020360 0.300500 -0.016150 0.400410 -0.013050 0.500340 -0.011040 0.600280 -0.008930 0.700180 -0.005820 0.800130 -0.004320 0.900110 -0.003410 0.950070 -0.002350 1.000000 -0.000800