GOE 121 (MVA H.1) AIRFOIL 17. 17. 0.000000 0.000000 0.012280 0.015370 0.024670 0.023050 0.049490 0.035900 0.074370 0.044360 0.099250 0.052910 0.149110 0.062820 0.199010 0.070030 0.298930 0.075240 0.398940 0.074460 0.499010 0.069390 0.599120 0.062110 0.699300 0.049830 0.799490 0.036250 0.899720 0.019780 0.949830 0.011890 1.000000 0.001000 0.000000 0.000000 0.012670 -0.012320 0.025190 -0.014240 0.050210 -0.014490 0.075180 -0.012530 0.100120 -0.008380 0.150030 -0.002270 0.199950 0.003640 0.299800 0.013960 0.399750 0.017580 0.499750 0.017900 0.599790 0.015020 0.699830 0.012040 0.799870 0.009160 0.899930 0.005180 0.949950 0.002280 1.000000 -0.001000