MORAN: PROGRAM PANEL INPUT NLOWER,NUPPER 20,20 INPUT NACA NUMBER 4412 BODY SHAPE I X Y 1 1.00000 0.00000 2 0.99373 -0.00005 3 0.97509 -0.00022 4 0.94460 -0.00054 5 0.90307 -0.00108 6 0.85163 -0.00195 7 0.79162 -0.00325 8 0.72458 -0.00509 9 0.65223 -0.00751 10 0.57636 -0.01045 11 0.49883 -0.01372 12 0.42151 -0.01698 13 0.34711 -0.02015 14 0.27679 -0.02367 15 0.21167 -0.02679 16 0.15312 -0.02871 17 0.10242 -0.02869 18 0.06077 -0.02617 19 0.02925 -0.02070 20 0.00876 -0.01203 21 0.00000 0.00000 22 0.00355 0.01447 23 0.01969 0.03019 24 0.04822 0.04648 25 0.08856 0.06233 26 0.13977 0.07656 27 0.20054 0.08799 28 0.26922 0.09560 29 0.34387 0.09866 30 0.42206 0.09687 31 0.50117 0.09150 32 0.58008 0.08340 33 0.65679 0.07312 34 0.72941 0.06133 35 0.79617 0.04877 36 0.85548 0.03624 37 0.90594 0.02452 38 0.94641 0.01441 39 0.97597 0.00661 40 0.99396 0.00168 INPUT ALPHA IN DEGREES: 4 PRESSURE DISTRIBUTION I X Y CP 1 0.9969 0.0000 0.34251 2 0.9844 -0.0001 0.26832 3 0.9598 -0.0004 0.23183 4 0.9238 -0.0008 0.21354 5 0.8774 -0.0015 0.20469 6 0.8216 -0.0026 0.20066 7 0.7581 -0.0042 0.19863 8 0.6884 -0.0063 0.19695 9 0.6143 -0.0090 0.19492 10 0.5376 -0.0121 0.19311 11 0.4602 -0.0153 0.19553 12 0.3843 -0.0186 0.20299 13 0.3120 -0.0219 0.20284 14 0.2442 -0.0252 0.19958 15 0.1824 -0.0277 0.20115 16 0.1278 -0.0287 0.21867 17 0.0816 -0.0274 0.27202 18 0.0450 -0.0234 0.40418 19 0.0190 -0.0164 0.70531 20 0.0044 -0.0060 0.97767 21 0.0018 0.0072 -0.40045 22 0.0116 0.0223 -1.31225 23 0.0340 0.0383 -1.37558 24 0.0684 0.0544 -1.33493 25 0.1142 0.0694 -1.29022 26 0.1702 0.0823 -1.23864 27 0.2349 0.0918 -1.16962 28 0.3065 0.0971 -1.07431 29 0.3830 0.0978 -0.94111 30 0.4616 0.0942 -0.80455 31 0.5406 0.0874 -0.68282 32 0.6184 0.0783 -0.57020 33 0.6931 0.0672 -0.46208 34 0.7628 0.0551 -0.35616 35 0.8258 0.0425 -0.25070 36 0.8807 0.0304 -0.14431 37 0.9262 0.0195 -0.03571 38 0.9612 0.0105 0.07699 39 0.9850 0.0041 0.19887 40 0.9970 0.0008 0.34251 AT ALPHA = 4.000 CD = -0.00246 CL = 0.95835 CM = -0.34437 Another angle of attack? (Y/N): n STOP