Smoothed ATR airfoil coordinates obtained using AFSMO (Harry Morgan's NASA smoothing program) 1.000000 0.000000 0.968000 0.005100 0.941000 0.009770 0.914000 0.014810 0.885000 0.020500 0.859000 0.025700 0.830000 0.031440 0.805000 0.036250 0.776000 0.041580 0.751000 0.045970 0.723000 0.050700 0.696000 0.055120 0.670000 0.059260 0.649000 0.062500 0.623000 0.066320 0.598000 0.069820 0.575000 0.072940 0.556000 0.075480 0.535000 0.078260 0.517000 0.080580 0.488000 0.084110 0.458000 0.087350 0.431000 0.089890 0.405000 0.092060 0.381000 0.093900 0.338000 0.096880 0.295000 0.099360 0.254000 0.100860 0.214000 0.100820 0.191000 0.099740 0.158000 0.096290 0.131000 0.091330 0.107000 0.084920 0.082000 0.075810 0.060700 0.065600 0.033800 0.048020 0.025600 0.041070 0.009250 0.022840 0.004430 0.015030 0.000920 0.006360 0.000000 -0.000120 0.004500 -0.012160 0.013200 -0.019210 0.016600 -0.021050 0.051400 -0.031550 0.091500 -0.037040 0.130000 -0.039980 0.157000 -0.041370 0.182000 -0.042370 0.215000 -0.043420 0.246000 -0.044230 0.268000 -0.044700 0.291000 -0.045070 0.321000 -0.045310 0.346000 -0.045250 0.376000 -0.044860 0.405000 -0.044210 0.434000 -0.043370 0.460000 -0.042500 0.487000 -0.041490 0.511000 -0.040470 0.532000 -0.039480 0.552000 -0.038460 0.572000 -0.037360 0.596000 -0.035900 0.624000 -0.033990 0.650000 -0.032070 0.682000 -0.029570 0.714000 -0.027040 0.743000 -0.024770 0.769000 -0.022700 0.796000 -0.020440 0.826000 -0.017690 0.854000 -0.014860 0.885000 -0.011480 0.916000 -0.007950 0.946000 -0.004610 0.979000 -0.001430 1.000000 0.000000