GOE 134 (MVA H.12) AIRFOIL 17. 17. 0.000000 0.000000 0.012500 0.020710 0.025000 0.031120 0.050000 0.045040 0.075000 0.055270 0.100000 0.063290 0.150000 0.075430 0.200000 0.082680 0.300000 0.088270 0.400000 0.086860 0.500000 0.080550 0.600000 0.070740 0.700000 0.058330 0.800000 0.045220 0.900000 0.028610 0.950000 0.019060 1.000000 0.009000 0.000000 0.000000 0.012500 -0.008790 0.025000 -0.008680 0.050000 -0.008450 0.075000 -0.008230 0.100000 -0.008010 0.150000 -0.007570 0.200000 -0.007120 0.300000 -0.006230 0.400000 -0.005340 0.500000 -0.004450 0.600000 -0.003560 0.700000 -0.002670 0.800000 -0.001780 0.900000 -0.000890 0.950000 -0.000450 1.000000 0.000000