GOE 165 (MVA MK.11) AIRFOIL 17. 17. 0.000000 0.000000 0.011950 0.019440 0.024080 0.032480 0.048650 0.047680 0.073210 0.062880 0.097930 0.072880 0.147500 0.088190 0.197230 0.097700 0.297080 0.102940 0.397130 0.101080 0.497300 0.095220 0.597660 0.082470 0.698070 0.067830 0.798530 0.051680 0.899110 0.031330 0.949460 0.018860 1.000000 0.000600 0.000000 0.000000 0.012690 -0.006640 0.025310 -0.010880 0.050420 -0.014870 0.075550 -0.019350 0.100600 -0.020940 0.150690 -0.024120 0.200660 -0.023300 0.300420 -0.014670 0.399910 0.003260 0.499430 0.019980 0.599220 0.027420 0.699240 0.026760 0.799390 0.021500 0.899640 0.012750 0.949830 0.006080 1.000000 -0.000600