XFOIL Version 6.96 Calculated polar for: AH 93-W-174 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 0.500 e 6 Ncrit = 9.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -16.750 -0.7736 0.08984 0.08678 -0.0577 1.0000 0.0274 -16.500 -0.8158 0.07853 0.07525 -0.0652 1.0000 0.0274 -16.250 -0.8408 0.07062 0.06717 -0.0705 1.0000 0.0275 -16.000 -0.8589 0.06415 0.06055 -0.0749 1.0000 0.0277 -15.750 -0.8742 0.05848 0.05473 -0.0787 1.0000 0.0279 -15.500 -0.8844 0.05377 0.04989 -0.0817 1.0000 0.0282 -15.250 -0.8935 0.04946 0.04544 -0.0844 1.0000 0.0284 -15.000 -0.8999 0.04574 0.04158 -0.0864 1.0000 0.0287 -14.750 -0.9042 0.04250 0.03820 -0.0880 1.0000 0.0290 -14.500 -0.9061 0.03976 0.03531 -0.0891 1.0000 0.0292 -14.250 -0.9097 0.03696 0.03240 -0.0895 1.0000 0.0295 -14.000 -0.9106 0.03458 0.02999 -0.0894 1.0000 0.0301 -13.750 -0.9068 0.03284 0.02822 -0.0891 1.0000 0.0305 -13.500 -0.8523 0.03055 0.02585 -0.0987 0.9288 0.0316 -13.250 -0.7704 0.02831 0.02305 -0.1139 0.8375 0.0333 -13.000 -0.7648 0.02734 0.02177 -0.1125 0.7920 0.0338 -12.750 -0.7584 0.02650 0.02069 -0.1110 0.7654 0.0342 -12.500 -0.7544 0.02503 0.01909 -0.1092 0.7461 0.0349 -12.250 -0.7471 0.02408 0.01803 -0.1075 0.7303 0.0356 -12.000 -0.7381 0.02338 0.01723 -0.1057 0.7172 0.0362 -11.750 -0.7287 0.02273 0.01650 -0.1037 0.7061 0.0370 -11.500 -0.7196 0.02219 0.01584 -0.1015 0.6972 0.0378 -11.250 -0.7059 0.02170 0.01523 -0.0998 0.6886 0.0389 -11.000 -0.6894 0.02124 0.01461 -0.0984 0.6814 0.0396 -10.750 -0.6759 0.02023 0.01357 -0.0970 0.6747 0.0407 -10.500 -0.6587 0.01965 0.01294 -0.0958 0.6683 0.0418 -10.250 -0.6392 0.01920 0.01242 -0.0948 0.6624 0.0429 -10.000 -0.6182 0.01878 0.01193 -0.0940 0.6567 0.0444 -9.750 -0.5963 0.01844 0.01146 -0.0933 0.6514 0.0457 -9.500 -0.5778 0.01773 0.01069 -0.0923 0.6468 0.0473 -9.250 -0.5560 0.01725 0.01021 -0.0916 0.6425 0.0489 -9.000 -0.5328 0.01689 0.00980 -0.0911 0.6380 0.0507 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0.1636 -4.000 -0.0176 0.01150 0.00413 -0.0868 0.5754 0.1810 -3.750 0.0099 0.01130 0.00401 -0.0868 0.5729 0.2014 -3.500 0.0375 0.01110 0.00389 -0.0869 0.5705 0.2252 -3.250 0.0652 0.01092 0.00378 -0.0870 0.5681 0.2522 -3.000 0.0929 0.01072 0.00368 -0.0871 0.5658 0.2844 -2.750 0.1205 0.01053 0.00360 -0.0873 0.5634 0.3240 -2.500 0.1483 0.01039 0.00358 -0.0874 0.5608 0.3702 -2.250 0.1757 0.01014 0.00352 -0.0875 0.5587 0.4221 -2.000 0.2034 0.00994 0.00350 -0.0876 0.5565 0.4728 -1.750 0.2313 0.00980 0.00351 -0.0877 0.5542 0.5189 -1.500 0.2595 0.00972 0.00352 -0.0878 0.5520 0.5580 -1.250 0.2878 0.00967 0.00354 -0.0878 0.5497 0.5904 -1.000 0.3163 0.00967 0.00357 -0.0879 0.5475 0.6179 -0.750 0.3448 0.00974 0.00365 -0.0880 0.5451 0.6414 -0.500 0.3732 0.00979 0.00375 -0.0880 0.5430 0.6619 -0.250 0.4015 0.00981 0.00381 -0.0880 0.5411 0.6799 0.000 0.4299 0.00984 0.00388 -0.0881 0.5389 0.6953 0.250 0.4584 0.00989 0.00394 -0.0881 0.5366 0.7096 0.500 0.4870 0.00994 0.00399 -0.0882 0.5343 0.7235 0.750 0.5152 0.00999 0.00405 -0.0882 0.5321 0.7357 1.000 0.5436 0.01007 0.00413 -0.0882 0.5301 0.7471 1.250 0.5726 0.01027 0.00427 -0.0884 0.5279 0.7590 1.500 0.6000 0.01032 0.00440 -0.0883 0.5260 0.7691 1.750 0.6279 0.01038 0.00449 -0.0882 0.5239 0.7794 2.000 0.6555 0.01044 0.00460 -0.0881 0.5215 0.7899 2.250 0.6831 0.01050 0.00469 -0.0880 0.5192 0.7997 2.500 0.7112 0.01059 0.00478 -0.0880 0.5172 0.8097 2.750 0.7388 0.01066 0.00487 -0.0878 0.5152 0.8176 3.000 0.7669 0.01078 0.00497 -0.0879 0.5131 0.8260 3.250 0.7947 0.01095 0.00514 -0.0879 0.5107 0.8331 3.500 0.8214 0.01100 0.00526 -0.0877 0.5087 0.8408 3.750 0.8486 0.01107 0.00538 -0.0876 0.5065 0.8483 4.000 0.8752 0.01113 0.00549 -0.0873 0.5042 0.8555 4.250 0.9029 0.01121 0.00557 -0.0873 0.5018 0.8632 4.500 0.9293 0.01126 0.00565 -0.0870 0.4996 0.8698 4.750 0.9569 0.01136 0.00575 -0.0870 0.4975 0.8775 5.000 0.9839 0.01154 0.00593 -0.0869 0.4951 0.8842 5.250 1.0092 0.01160 0.00608 -0.0864 0.4929 0.8923 5.500 1.0342 0.01165 0.00621 -0.0859 0.4905 0.8999 5.750 1.0594 0.01171 0.00633 -0.0854 0.4879 0.9085 6.000 1.0841 0.01174 0.00640 -0.0848 0.4854 0.9169 6.250 1.1097 0.01179 0.00647 -0.0844 0.4830 0.9266 6.500 1.1335 0.01185 0.00655 -0.0836 0.4805 0.9368 6.750 1.1569 0.01193 0.00669 -0.0828 0.4777 0.9493 7.000 1.1826 0.01191 0.00677 -0.0824 0.4742 0.9657 7.250 1.2185 0.01192 0.00684 -0.0844 0.4702 0.9882 7.500 1.2487 0.01197 0.00689 -0.0851 0.4666 1.0000 7.750 1.2781 0.01214 0.00702 -0.0858 0.4626 1.0000 8.000 1.3042 0.01221 0.00720 -0.0858 0.4584 1.0000 8.250 1.3309 0.01226 0.00729 -0.0859 0.4536 1.0000 8.500 1.3577 0.01234 0.00734 -0.0859 0.4484 1.0000 8.750 1.3818 0.01243 0.00752 -0.0855 0.4423 1.0000 9.000 1.4059 0.01249 0.00761 -0.0850 0.4355 1.0000 9.250 1.4297 0.01265 0.00778 -0.0846 0.4293 1.0000 9.500 1.4528 0.01279 0.00799 -0.0840 0.4225 1.0000 9.750 1.4742 0.01298 0.00818 -0.0831 0.4147 1.0000 10.000 1.4944 0.01318 0.00842 -0.0820 0.4045 1.0000 10.250 1.5131 0.01343 0.00870 -0.0807 0.3940 1.0000 10.500 1.5289 0.01377 0.00904 -0.0789 0.3833 1.0000 10.750 1.5392 0.01418 0.00943 -0.0762 0.3708 1.0000 11.000 1.5475 0.01469 0.00993 -0.0732 0.3566 1.0000 11.250 1.5503 0.01542 0.01062 -0.0696 0.3402 1.0000 11.500 1.5499 0.01637 0.01153 -0.0659 0.3226 1.0000 11.750 1.5433 0.01775 0.01285 -0.0620 0.3029 1.0000 12.000 1.5309 0.01973 0.01477 -0.0582 0.2832 1.0000 12.250 1.5165 0.02225 0.01724 -0.0550 0.2650 1.0000 12.500 1.5012 0.02520 0.02013 -0.0525 0.2465 1.0000 12.750 1.4844 0.02850 0.02339 -0.0503 0.2285 1.0000 13.000 1.4685 0.03191 0.02676 -0.0484 0.2127 1.0000 13.250 1.4532 0.03540 0.03021 -0.0468 0.1979 1.0000 13.500 1.4379 0.03898 0.03375 -0.0454 0.1831 1.0000 13.750 1.4253 0.04247 0.03720 -0.0444 0.1700 1.0000 14.000 1.4134 0.04606 0.04076 -0.0435 0.1563 1.0000 14.250 1.4036 0.04959 0.04425 -0.0430 0.1435 1.0000 14.500 1.3951 0.05311 0.04773 -0.0425 0.1312 1.0000 14.750 1.3871 0.05671 0.05129 -0.0423 0.1194 1.0000 15.000 1.3805 0.06024 0.05478 -0.0422 0.1077 1.0000 15.250 1.3761 0.06360 0.05811 -0.0422 0.0971 1.0000 15.500 1.3716 0.06709 0.06159 -0.0424 0.0873 1.0000 15.750 1.3684 0.07047 0.06495 -0.0426 0.0784 1.0000 16.000 1.3648 0.07399 0.06846 -0.0429 0.0710 1.0000 16.250 1.3614 0.07755 0.07200 -0.0434 0.0637 1.0000 16.500 1.3601 0.08093 0.07537 -0.0439 0.0569 1.0000 16.750 1.3585 0.08438 0.07883 -0.0444 0.0513 1.0000 17.000 1.3552 0.08813 0.08258 -0.0451 0.0465 1.0000 17.250 1.3550 0.09152 0.08599 -0.0459 0.0423 1.0000 17.500 1.3532 0.09520 0.08970 -0.0467 0.0388 1.0000 17.750 1.3521 0.09879 0.09332 -0.0476 0.0355 1.0000 18.000 1.3502 0.10258 0.09714 -0.0486 0.0332 1.0000 18.250 1.3506 0.10606 0.10067 -0.0496 0.0308 1.0000