AIRFOIL GEOMETRY DSMA671(MODEL B) J X/C Y0/C PHI(DEG) Y0/C PHI(DEG) UPPER SURFACE LOWER SURFACE 1 0.000 0.00000 90.00 0.00000 90.00 2 0.002 0.01090 63.37 -0.00896 114.29 3 0.005 0.01330 48.74 -0.01304 126.84 4 0.010 0.01949 40.95 -0.01921 135.96 5 0.025 0.02826 25.20 -0.02968 151.04 6 0.050 0.03739 16.61 -0.04025 161.74 7 0.100 0.04905 10.52 -0.05200 170.39 8 0.150 0.05690 7.62 -0.05861 174.14 9 0.200 0.06277 5.86 -0.06276 176.20 10 0.250 0.06724 4.36 -0.06538 177.76 11 0.300 0.07043 2.97 -0.06672 179.17 12 0.350 0.07248 1.78 -0.06685 180.55 13 0.400 0.07357 0.73 -0.06569 182.14 14 0.443 0.07380 -0.14 -0.06348 183.79 15 0.450 0.07377 -0.28 -0.06300 184.09 16 0.493 0.07323 -1.17 -0.05921 185.99 17 0.500 0.07308 -1.32 -0.05846 186.30 18 0.550 0.07144 -2.43 -0.05195 188.51 19 0.593 0.06923 -3.46 -0.04486 190.15 20 0.600 0.06880 -3.63 -0.04359 190.37 21 0.650 0.06507 -4.90 -0.03384 191.57 22 0.693 0.06096 -6.02 -0.02485 191.93 23 0.700 0.06021 -6.21 -0.02337 191.93 24 0.750 0.05418 -7.55 -0.01298 191.39 25 0.793 0.04803 -8.75 -0.00474 190.20 26 0.800 0.04694 -8.96 -0.00349 189.94 27 0.843 0.03966 -10.28 -0.00328 187.79 28 0.850 0.03837 -10.51 0.00421 187.32 29 0.893 0.02982 -12.04 0.00836 183.32 30 0.900 0.02831 -12.34 0.00871 182.43 31 0.918 0.02424 -13.19 0.00908 179.82 32 0.949 0.01642 -15.31 0.00761 174.75 33 0.950 0.01615 -15.41 0.00751 174.59 34 0.970 0.01025 -17.49 0.00508 171.62 35 0.975 0.00865 -17.93 0.00432 170.95 36 0.990 0.00359 -19.49 0.00173 169.83 37 1.000 0.00002 -19.68 -0.00001 170.37