XFOIL Version 6.96 Calculated polar for: AH 82-150 A 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 1.000 e 6 Ncrit = 5.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -15.750 -0.8363 0.04696 0.04426 -0.1080 0.9360 0.0051 -15.500 -0.8222 0.04055 0.03753 -0.1192 0.9167 0.0052 -15.250 -0.8189 0.03648 0.03314 -0.1240 0.8882 0.0052 -15.000 -0.8123 0.03470 0.03118 -0.1245 0.8685 0.0054 -14.750 -0.8165 0.03233 0.02860 -0.1240 0.8528 0.0054 -14.500 -0.8168 0.03046 0.02655 -0.1232 0.8407 0.0054 -14.250 -0.8110 0.02910 0.02507 -0.1224 0.8314 0.0056 -14.000 -0.8084 0.02757 0.02339 -0.1212 0.8235 0.0056 -13.750 -0.8038 0.02620 0.02188 -0.1199 0.8161 0.0057 -13.500 -0.7938 0.02525 0.02081 -0.1188 0.8099 0.0060 -13.250 -0.7862 0.02414 0.01959 -0.1174 0.8037 0.0060 -13.000 -0.7760 0.02324 0.01857 -0.1161 0.7980 0.0061 -12.750 -0.7668 0.02226 0.01747 -0.1146 0.7932 0.0062 -12.500 -0.7558 0.02143 0.01653 -0.1131 0.7885 0.0063 -12.250 -0.7438 0.02070 0.01569 -0.1116 0.7841 0.0064 -12.000 -0.7317 0.02001 0.01491 -0.1100 0.7802 0.0065 -11.750 -0.7220 0.01924 0.01404 -0.1078 0.7759 0.0065 -11.500 -0.7127 0.01848 0.01317 -0.1055 0.7717 0.0068 -11.000 -0.6797 0.01717 0.01167 -0.1031 0.7652 0.0073 -10.750 -0.6604 0.01664 0.01108 -0.1022 0.7620 0.0075 -10.500 -0.6404 0.01615 0.01052 -0.1015 0.7588 0.0077 -10.250 -0.6197 0.01571 0.01001 -0.1007 0.7557 0.0080 -10.000 -0.5983 0.01528 0.00951 -0.1001 0.7529 0.0084 -9.750 -0.5764 0.01484 0.00901 -0.0995 0.7500 0.0086 -9.500 -0.5540 0.01443 0.00854 -0.0990 0.7472 0.0090 -9.250 -0.5311 0.01405 0.00808 -0.0986 0.7445 0.0092 -9.000 -0.5086 0.01362 0.00759 -0.0980 0.7418 0.0097 -8.500 -0.4615 0.01291 0.00681 -0.0973 0.7369 0.0109 -8.250 -0.4369 0.01262 0.00649 -0.0971 0.7342 0.0118 -8.000 -0.4121 0.01234 0.00618 -0.0969 0.7316 0.0125 -7.750 -0.3871 0.01209 0.00588 -0.0967 0.7292 0.0130 -7.500 -0.3627 0.01176 0.00551 -0.0964 0.7268 0.0143 -7.250 -0.3375 0.01152 0.00525 -0.0963 0.7244 0.0153 -7.000 -0.3115 0.01128 0.00500 -0.0962 0.7222 0.0164 -6.750 -0.2855 0.01106 0.00475 -0.0962 0.7197 0.0173 -6.500 -0.2595 0.01084 0.00450 -0.0962 0.7174 0.0181 -6.250 -0.2336 0.01059 0.00423 -0.0961 0.7150 0.0198 -6.000 -0.2073 0.01041 0.00404 -0.0961 0.7126 0.0214 -5.750 -0.1808 0.01026 0.00385 -0.0962 0.7103 0.0228 -5.500 -0.1536 0.01010 0.00368 -0.0963 0.7083 0.0238 -5.250 -0.1270 0.00986 0.00343 -0.0964 0.7060 0.0259 -5.000 -0.1000 0.00968 0.00324 -0.0965 0.7036 0.0280 -4.750 -0.0729 0.00952 0.00308 -0.0966 0.7012 0.0298 -4.500 -0.0456 0.00939 0.00292 -0.0968 0.6989 0.0315 -4.250 -0.0183 0.00926 0.00275 -0.0969 0.6968 0.0336 -4.000 0.0091 0.00910 0.00260 -0.0971 0.6948 0.0372 -3.750 0.0369 0.00895 0.00246 -0.0974 0.6925 0.0409 -3.500 0.0647 0.00882 0.00234 -0.0976 0.6902 0.0461 -3.250 0.0925 0.00868 0.00222 -0.0978 0.6879 0.0533 -3.000 0.1201 0.00854 0.00210 -0.0981 0.6855 0.0654 -2.750 0.1476 0.00838 0.00199 -0.0983 0.6832 0.0859 -2.500 0.1749 0.00813 0.00188 -0.0986 0.6810 0.1271 -2.250 0.2025 0.00785 0.00177 -0.0990 0.6788 0.1824 -2.000 0.2303 0.00757 0.00168 -0.0995 0.6763 0.2418 -1.750 0.2580 0.00725 0.00158 -0.0999 0.6736 0.3141 -1.500 0.2852 0.00662 0.00140 -0.1006 0.6710 0.4643 -1.250 0.3126 0.00601 0.00133 -0.1013 0.6684 0.6406 -1.000 0.3414 0.00603 0.00144 -0.1016 0.6656 0.6866 -0.750 0.3702 0.00611 0.00154 -0.1018 0.6621 0.7058 -0.500 0.3992 0.00617 0.00155 -0.1022 0.6580 0.7125 -0.250 0.4274 0.00622 0.00159 -0.1024 0.6539 0.7172 0.000 0.4562 0.00627 0.00164 -0.1027 0.6501 0.7225 0.250 0.4852 0.00631 0.00166 -0.1031 0.6462 0.7254 0.500 0.5139 0.00634 0.00166 -0.1035 0.6425 0.7265 0.750 0.5425 0.00639 0.00166 -0.1039 0.6390 0.7274 1.000 0.5714 0.00640 0.00168 -0.1043 0.6354 0.7283 1.250 0.6000 0.00642 0.00169 -0.1046 0.6312 0.7292 1.500 0.6283 0.00645 0.00172 -0.1049 0.6269 0.7300 1.750 0.6567 0.00649 0.00175 -0.1052 0.6226 0.7308 2.000 0.6852 0.00652 0.00179 -0.1056 0.6179 0.7316 2.250 0.7132 0.00657 0.00184 -0.1058 0.6126 0.7325 2.500 0.7414 0.00662 0.00189 -0.1061 0.6078 0.7333 2.750 0.7695 0.00667 0.00194 -0.1064 0.6020 0.7344 3.250 0.8251 0.00680 0.00208 -0.1068 0.5900 0.7364 3.500 0.8522 0.00689 0.00216 -0.1069 0.5828 0.7374 3.750 0.8797 0.00697 0.00224 -0.1071 0.5745 0.7383 4.000 0.9063 0.00708 0.00234 -0.1071 0.5652 0.7392 4.250 0.9325 0.00720 0.00245 -0.1070 0.5539 0.7401 4.500 0.9577 0.00737 0.00257 -0.1067 0.5383 0.7410 4.750 0.9794 0.00769 0.00277 -0.1058 0.5065 0.7419 5.000 0.9968 0.00821 0.00308 -0.1041 0.4603 0.7429 5.250 1.0122 0.00880 0.00345 -0.1021 0.4128 0.7440 5.500 1.0249 0.00950 0.00389 -0.0996 0.3603 0.7453 5.750 1.0359 0.01022 0.00436 -0.0969 0.3089 0.7466 6.000 1.0405 0.01113 0.00494 -0.0930 0.2458 0.7480 6.250 1.0395 0.01198 0.00552 -0.0880 0.1927 0.7495 6.500 1.0410 0.01285 0.00618 -0.0837 0.1478 0.7510 6.750 1.0419 0.01381 0.00694 -0.0794 0.1043 0.7524 7.000 1.0444 0.01479 0.00774 -0.0757 0.0680 0.7539 7.500 1.0538 0.01683 0.00951 -0.0695 0.0141 0.7566 7.750 1.0686 0.01743 0.01012 -0.0680 0.0112 0.7578 8.000 1.0831 0.01806 0.01077 -0.0665 0.0096 0.7592 8.250 1.0975 0.01872 0.01148 -0.0651 0.0085 0.7606 8.500 1.1127 0.01936 0.01215 -0.0638 0.0080 0.7620 8.750 1.1275 0.02005 0.01288 -0.0625 0.0076 0.7636 9.000 1.1420 0.02076 0.01364 -0.0613 0.0072 0.7653 9.250 1.1555 0.02156 0.01447 -0.0599 0.0068 0.7671 9.500 1.1686 0.02241 0.01535 -0.0586 0.0064 0.7688 9.750 1.1795 0.02343 0.01643 -0.0571 0.0059 0.7703 10.000 1.1926 0.02432 0.01735 -0.0559 0.0057 0.7717 10.250 1.2061 0.02519 0.01828 -0.0547 0.0055 0.7734 10.500 1.2186 0.02615 0.01930 -0.0536 0.0054 0.7751 10.750 1.2303 0.02719 0.02039 -0.0523 0.0051 0.7769 11.000 1.2416 0.02827 0.02153 -0.0512 0.0050 0.7788 11.250 1.2531 0.02937 0.02268 -0.0501 0.0049 0.7808 11.500 1.2635 0.03057 0.02395 -0.0489 0.0047 0.7828 11.750 1.2736 0.03183 0.02526 -0.0478 0.0045 0.7848 12.250 1.2929 0.03451 0.02805 -0.0458 0.0042 0.7888 12.500 1.3006 0.03605 0.02966 -0.0447 0.0041 0.7912 12.750 1.3054 0.03791 0.03160 -0.0435 0.0039 0.7937 13.000 1.3084 0.04000 0.03379 -0.0423 0.0038 0.7965 13.250 1.3167 0.04166 0.03551 -0.0416 0.0037 0.7992 13.500 1.3244 0.04341 0.03734 -0.0409 0.0037 0.8019 13.750 1.3336 0.04504 0.03906 -0.0404 0.0036 0.8048 14.000 1.3377 0.04723 0.04135 -0.0397 0.0036 0.8079 14.250 1.3465 0.04900 0.04319 -0.0393 0.0035 0.8113 14.500 1.3536 0.05100 0.04526 -0.0389 0.0034 0.8146 14.750 1.3591 0.05320 0.04756 -0.0385 0.0033 0.8181 15.000 1.3653 0.05535 0.04980 -0.0383 0.0032 0.8221 15.250 1.3697 0.05778 0.05233 -0.0381 0.0031 0.8264 15.750 1.3760 0.06312 0.05787 -0.0380 0.0030 0.8361 16.000 1.3798 0.06580 0.06065 -0.0381 0.0029 0.8420 16.250 1.3813 0.06882 0.06378 -0.0383 0.0029 0.8485 16.500 1.3817 0.07205 0.06715 -0.0386 0.0028 0.8566 16.750 1.3847 0.07497 0.07019 -0.0390 0.0028 0.8678 17.000 1.3850 0.07825 0.07361 -0.0394 0.0027 0.8859 17.250 1.3837 0.08128 0.07688 -0.0395 0.0027 1.0000 17.500 1.3839 0.08484 0.08054 -0.0404 0.0026 1.0000 17.750 1.3836 0.08857 0.08436 -0.0415 0.0026 1.0000 18.000 1.3816 0.09264 0.08852 -0.0427 0.0026 1.0000 18.250 1.3807 0.09659 0.09257 -0.0440 0.0025 1.0000 18.500 1.3777 0.10095 0.09702 -0.0456 0.0025 1.0000 18.750 1.3742 0.10543 0.10161 -0.0473 0.0025 1.0000 19.000 1.3707 0.11001 0.10629 -0.0491 0.0024 1.0000 19.250 1.3664 0.11479 0.11117 -0.0512 0.0024 1.0000