GOE 114 (MVA MK.1) AIRFOIL 17. 17. 0.000000 0.000000 0.012250 0.007130 0.024540 0.013070 0.049190 0.022940 0.073860 0.032310 0.098620 0.039180 0.148180 0.051630 0.197820 0.061680 0.297380 0.074100 0.397260 0.077620 0.497360 0.074760 0.597640 0.067000 0.698080 0.054340 0.798660 0.038090 0.899300 0.019950 0.949640 0.010220 1.000000 0.000000 0.000000 0.000000 0.012710 -0.005850 0.025340 -0.009710 0.050580 -0.016510 0.075750 -0.021330 0.100870 -0.024740 0.150970 -0.027470 0.201000 -0.028200 0.300750 -0.021180 0.400380 -0.010670 0.500160 -0.004640 0.600020 -0.000620 0.699970 0.000910 0.799950 0.001340 0.899980 0.000670 0.949990 0.000330 1.000000 0.000000