Smoothed ATR airfoil coordinates obtained using AFSMO (Harry Morgan's NASA smoothing program) 1.00000 0.00000 0.96800 0.00510 0.94100 0.00977 0.91400 0.01481 0.88500 0.02050 0.85900 0.02570 0.83000 0.03144 0.80500 0.03625 0.77600 0.04158 0.75100 0.04597 0.72300 0.05070 0.69600 0.05512 0.67000 0.05926 0.64900 0.06250 0.62300 0.06632 0.59800 0.06982 0.57500 0.07294 0.55600 0.07548 0.53500 0.07826 0.51700 0.08058 0.48800 0.08411 0.45800 0.08735 0.43100 0.08989 0.40500 0.09206 0.38100 0.09390 0.33800 0.09688 0.29500 0.09936 0.25400 0.10086 0.21400 0.10082 0.19100 0.09974 0.15800 0.09629 0.13100 0.09133 0.10700 0.08492 0.08200 0.07581 0.06070 0.06560 0.03380 0.04802 0.02560 0.04107 0.00925 0.02284 0.00443 0.01503 0.00092 0.00636 0.00000 -0.00012 0.00450 -0.01216 0.01320 -0.01921 0.01660 -0.02105 0.05140 -0.03155 0.09150 -0.03704 0.13000 -0.03998 0.15700 -0.04137 0.18200 -0.04237 0.21500 -0.04342 0.24600 -0.04423 0.26800 -0.04470 0.29100 -0.04507 0.32100 -0.04531 0.34600 -0.04525 0.37600 -0.04486 0.40500 -0.04421 0.43400 -0.04337 0.46000 -0.04250 0.48700 -0.04149 0.51100 -0.04047 0.53200 -0.03948 0.55200 -0.03846 0.57200 -0.03736 0.59600 -0.03590 0.62400 -0.03399 0.65000 -0.03207 0.68200 -0.02957 0.71400 -0.02704 0.74300 -0.02477 0.76900 -0.02270 0.79600 -0.02044 0.82600 -0.01769 0.85400 -0.01486 0.88500 -0.01148 0.91600 -0.00795 0.94600 -0.00461 0.97900 -0.00143 1.00000 0.00000