XFOIL Version 6.96 Calculated polar for: AH 85-L-120/17 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 ------ -------- --------- --------- -------- -------- -------- -16.000 -0.8896 0.11410 0.11257 -0.0035 1.0000 0.0033 -15.750 -0.8622 0.11613 0.11465 -0.0030 1.0000 0.0034 -15.500 -1.0333 0.07034 0.06822 -0.0280 1.0000 0.0031 -15.000 -1.0835 0.05380 0.05122 -0.0375 0.9572 0.0031 -14.750 -1.0763 0.04995 0.04719 -0.0413 0.9412 0.0031 -14.500 -1.0895 0.04423 0.04113 -0.0441 0.9284 0.0031 -14.250 -1.0993 0.03966 0.03629 -0.0455 0.9195 0.0032 -14.000 -1.0991 0.03637 0.03271 -0.0463 0.9132 0.0031 -13.750 -1.0715 0.03646 0.03286 -0.0476 0.9085 0.0034 -13.500 -1.0833 0.03221 0.02822 -0.0468 0.9028 0.0034 -13.250 -1.0713 0.03066 0.02652 -0.0468 0.8987 0.0034 -13.000 -1.0401 0.03135 0.02733 -0.0481 0.8954 0.0037 -12.750 -1.0396 0.02852 0.02419 -0.0469 0.8912 0.0036 -12.500 -1.0274 0.02693 0.02243 -0.0465 0.8881 0.0037 -12.250 -1.0033 0.02688 0.02239 -0.0470 0.8858 0.0040 -12.000 -0.9944 0.02501 0.02030 -0.0458 0.8829 0.0040 -11.750 -0.9801 0.02375 0.01889 -0.0451 0.8803 0.0041 -11.500 -0.9552 0.02379 0.01894 -0.0456 0.8781 0.0044 -11.250 -0.9402 0.02249 0.01745 -0.0448 0.8757 0.0044 -11.000 -0.9216 0.02158 0.01642 -0.0443 0.8735 0.0046 -10.750 -0.9049 0.02056 0.01527 -0.0434 0.8713 0.0047 -10.500 -0.8846 0.02007 0.01472 -0.0429 0.8694 0.0049 -10.250 -0.8676 0.01909 0.01361 -0.0419 0.8674 0.0050 -10.000 -0.8484 0.01841 0.01284 -0.0411 0.8654 0.0051 -9.750 -0.8325 0.01739 0.01169 -0.0398 0.8634 0.0050 -9.500 -0.8101 0.01711 0.01136 -0.0394 0.8616 0.0052 -9.250 -0.7967 0.01594 0.01004 -0.0375 0.8596 0.0056 -9.000 -0.7769 0.01550 0.00953 -0.0365 0.8578 0.0054 -8.750 -0.7590 0.01493 0.00895 -0.0352 0.8561 0.0062 -8.500 -0.7393 0.01452 0.00850 -0.0340 0.8544 0.0064 -8.250 -0.7222 0.01396 0.00787 -0.0324 0.8526 0.0066 -8.000 -0.7030 0.01361 0.00749 -0.0311 0.8508 0.0068 -7.750 -0.6832 0.01330 0.00713 -0.0298 0.8489 0.0073 -7.500 -0.6644 0.01287 0.00663 -0.0284 0.8472 0.0074 -7.250 -0.6441 0.01248 0.00616 -0.0273 0.8457 0.0077 -7.000 -0.6222 0.01220 0.00584 -0.0264 0.8443 0.0080 -6.750 -0.6003 0.01192 0.00554 -0.0255 0.8428 0.0081 -6.500 -0.5801 0.01153 0.00510 -0.0243 0.8411 0.0087 -6.250 -0.5595 0.01114 0.00470 -0.0231 0.8393 0.0099 -6.000 -0.5369 0.01089 0.00443 -0.0223 0.8377 0.0106 -5.750 -0.5139 0.01068 0.00419 -0.0216 0.8360 0.0117 -5.500 -0.4908 0.01046 0.00394 -0.0209 0.8344 0.0126 -5.250 -0.4683 0.01018 0.00366 -0.0200 0.8329 0.0162 -5.000 -0.4445 0.01000 0.00346 -0.0194 0.8313 0.0179 -4.750 -0.4212 0.00977 0.00325 -0.0187 0.8298 0.0237 -4.500 -0.3980 0.00955 0.00305 -0.0180 0.8282 0.0323 -4.250 -0.3758 0.00925 0.00285 -0.0171 0.8263 0.0524 -4.000 -0.3551 0.00888 0.00264 -0.0160 0.8243 0.0910 -3.750 -0.3335 0.00855 0.00245 -0.0150 0.8223 0.1268 -3.500 -0.3157 0.00802 0.00221 -0.0133 0.8202 0.2026 -3.250 -0.2949 0.00766 0.00203 -0.0122 0.8182 0.2557 -3.000 -0.2810 0.00696 0.00177 -0.0098 0.8160 0.3713 -2.750 -0.2698 0.00619 0.00153 -0.0068 0.8133 0.5027 -2.500 -0.2535 0.00571 0.00137 -0.0046 0.8104 0.5855 -2.250 -0.2325 0.00545 0.00126 -0.0033 0.8077 0.6330 -2.000 -0.2113 0.00522 0.00120 -0.0019 0.8053 0.6799 -1.750 -0.1864 0.00513 0.00116 -0.0013 0.8033 0.7051 -1.500 -0.1610 0.00508 0.00116 -0.0009 0.8012 0.7260 -1.250 -0.1351 0.00505 0.00117 -0.0005 0.7987 0.7440 -1.000 -0.1086 0.00504 0.00118 -0.0003 0.7959 0.7553 -0.750 -0.0818 0.00503 0.00120 -0.0001 0.7930 0.7656 -0.500 -0.0548 0.00504 0.00119 0.0000 0.7903 0.7746 -0.250 -0.0273 0.00505 0.00120 0.0000 0.7875 0.7795 0.000 0.0000 0.00505 0.00121 0.0000 0.7836 0.7837 0.250 0.0273 0.00505 0.00120 0.0000 0.7793 0.7875 0.500 0.0548 0.00504 0.00119 0.0000 0.7742 0.7902 0.750 0.0818 0.00503 0.00119 0.0002 0.7651 0.7930 1.000 0.1086 0.00503 0.00118 0.0003 0.7555 0.7958 1.250 0.1351 0.00505 0.00117 0.0005 0.7436 0.7987 1.500 0.1611 0.00508 0.00116 0.0009 0.7268 0.8012 1.750 0.1866 0.00513 0.00117 0.0013 0.7058 0.8032 2.000 0.2113 0.00522 0.00120 0.0019 0.6798 0.8053 2.250 0.2329 0.00543 0.00126 0.0032 0.6352 0.8077 2.500 0.2537 0.00570 0.00137 0.0045 0.5867 0.8104 2.750 0.2732 0.00604 0.00150 0.0061 0.5289 0.8132 3.000 0.2830 0.00686 0.00175 0.0094 0.3884 0.8159 3.250 0.2959 0.00761 0.00201 0.0120 0.2636 0.8181 3.500 0.3159 0.00800 0.00220 0.0133 0.2047 0.8202 3.750 0.3349 0.00847 0.00243 0.0148 0.1395 0.8223 4.000 0.3562 0.00881 0.00262 0.0158 0.0998 0.8243 4.250 0.3767 0.00920 0.00284 0.0170 0.0584 0.8262 4.500 0.3984 0.00952 0.00305 0.0179 0.0347 0.8281 4.750 0.4212 0.00977 0.00326 0.0187 0.0238 0.8299 5.000 0.4446 0.00999 0.00346 0.0194 0.0189 0.8314 5.250 0.4680 0.01020 0.00368 0.0201 0.0155 0.8329 5.500 0.4908 0.01045 0.00393 0.0209 0.0127 0.8344 5.750 0.5140 0.01067 0.00418 0.0216 0.0118 0.8361 6.000 0.5369 0.01089 0.00441 0.0223 0.0105 0.8377 6.250 0.5588 0.01118 0.00473 0.0232 0.0095 0.8393 6.500 0.5801 0.01151 0.00508 0.0243 0.0086 0.8410 6.750 0.6011 0.01185 0.00546 0.0253 0.0082 0.8427 7.000 0.6232 0.01211 0.00574 0.0262 0.0077 0.8442 7.250 0.6433 0.01252 0.00621 0.0274 0.0077 0.8457 7.500 0.6640 0.01287 0.00664 0.0285 0.0075 0.8472 7.750 0.6833 0.01328 0.00711 0.0298 0.0074 0.8489 8.000 0.7026 0.01362 0.00749 0.0312 0.0066 0.8508 8.250 0.7227 0.01390 0.00780 0.0323 0.0063 0.8525 8.500 0.7414 0.01434 0.00828 0.0336 0.0061 0.8543 8.750 0.7590 0.01491 0.00889 0.0351 0.0056 0.8561 9.000 0.7728 0.01583 0.00991 0.0372 0.0052 0.8580 9.250 0.7954 0.01602 0.01012 0.0377 0.0054 0.8597 9.500 0.8082 0.01728 0.01156 0.0397 0.0052 0.8618 9.750 0.8293 0.01771 0.01206 0.0403 0.0051 0.8636 10.000 0.8471 0.01857 0.01302 0.0414 0.0050 0.8655 10.250 0.8675 0.01906 0.01358 0.0419 0.0049 0.8674 10.500 0.8861 0.01984 0.01447 0.0428 0.0047 0.8694 10.750 0.9033 0.02076 0.01550 0.0437 0.0047 0.8714 11.000 0.9179 0.02209 0.01698 0.0448 0.0047 0.8736 11.250 0.9374 0.02284 0.01786 0.0451 0.0044 0.8758 11.500 0.9545 0.02387 0.01904 0.0457 0.0044 0.8782 11.750 0.9695 0.02512 0.02044 0.0464 0.0042 0.8807 12.000 0.9780 0.02712 0.02267 0.0476 0.0042 0.8835 12.250 0.9935 0.02808 0.02373 0.0480 0.0041 0.8862 12.500 1.0222 0.02755 0.02312 0.0470 0.0037 0.8884 12.750 1.0295 0.02970 0.02551 0.0478 0.0037 0.8918 13.000 1.0403 0.03133 0.02730 0.0480 0.0037 0.8957 13.250 1.0584 0.03206 0.02808 0.0477 0.0035 0.8995 13.500 1.0545 0.03543 0.03176 0.0484 0.0035 0.9042 13.750 1.0822 0.03530 0.03158 0.0471 0.0033 0.9083 14.000 1.0797 0.03861 0.03517 0.0470 0.0034 0.9143 14.250 1.0881 0.04105 0.03778 0.0456 0.0033 0.9206 14.750 1.0920 0.04807 0.04521 0.0415 0.0031 0.9415 15.000 1.0728 0.05564 0.05314 0.0364 0.0031 0.9597 15.250 1.0432 0.06468 0.06244 0.0314 0.0030 1.0000 15.500 1.0393 0.06935 0.06720 0.0285 0.0031 1.0000 16.000 0.9137 0.10848 0.10691 0.0058 0.0033 1.0000