XFOIL Version 6.96 Calculated polar for: GEMINI (smoothed) 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 ------ -------- --------- --------- -------- -------- -------- -19.750 -0.8632 0.14087 0.13854 -0.0204 1.0000 0.0092 -19.500 -0.9075 0.12804 0.12556 -0.0271 1.0000 0.0092 -19.250 -0.9511 0.11589 0.11326 -0.0335 1.0000 0.0092 -19.000 -0.9950 0.10425 0.10147 -0.0396 1.0000 0.0091 -18.750 -1.0375 0.09317 0.09023 -0.0455 1.0000 0.0091 -18.500 -1.0746 0.08330 0.08019 -0.0507 1.0000 0.0090 -18.250 -1.1061 0.07452 0.07125 -0.0555 1.0000 0.0090 -18.000 -1.1316 0.06693 0.06352 -0.0596 1.0000 0.0090 -17.750 -1.1515 0.06045 0.05690 -0.0631 1.0000 0.0090 -17.500 -1.1668 0.05492 0.05124 -0.0659 1.0000 0.0091 -17.250 -1.1778 0.05017 0.04636 -0.0683 1.0000 0.0092 -17.000 -1.1858 0.04606 0.04213 -0.0701 1.0000 0.0092 -16.750 -1.1906 0.04249 0.03845 -0.0715 1.0000 0.0093 -16.500 -1.1930 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0.00721 0.00143 -0.0414 0.5790 0.4367 -1.250 0.0724 0.00706 0.00140 -0.0406 0.5702 0.4806 -1.000 0.0969 0.00701 0.00138 -0.0399 0.5613 0.5035 -0.750 0.1221 0.00698 0.00136 -0.0393 0.5521 0.5240 -0.500 0.1473 0.00697 0.00136 -0.0388 0.5431 0.5409 -0.250 0.1725 0.00697 0.00136 -0.0382 0.5330 0.5562 0.000 0.1979 0.00696 0.00136 -0.0377 0.5242 0.5723 0.250 0.2228 0.00698 0.00138 -0.0371 0.5149 0.5894 0.500 0.2482 0.00698 0.00139 -0.0366 0.5054 0.6050 0.750 0.2732 0.00700 0.00142 -0.0360 0.4967 0.6217 1.000 0.2984 0.00701 0.00145 -0.0355 0.4876 0.6369 1.250 0.3236 0.00704 0.00148 -0.0349 0.4789 0.6509 1.500 0.3485 0.00707 0.00152 -0.0343 0.4698 0.6667 2.000 0.3952 0.00705 0.00163 -0.0324 0.4528 0.7262 2.250 0.4186 0.00703 0.00169 -0.0315 0.4447 0.7547 2.500 0.4427 0.00707 0.00176 -0.0307 0.4362 0.7747 2.750 0.4674 0.00708 0.00182 -0.0301 0.4286 0.7944 3.000 0.4914 0.00713 0.00191 -0.0293 0.4205 0.8153 3.250 0.5165 0.00716 0.00199 -0.0287 0.4131 0.8373 3.500 0.5415 0.00722 0.00208 -0.0282 0.4050 0.8584 3.750 0.5687 0.00726 0.00218 -0.0281 0.3977 0.8791 4.000 0.5973 0.00735 0.00230 -0.0284 0.3895 0.8993 4.250 0.6299 0.00743 0.00241 -0.0295 0.3820 0.9161 4.500 0.6652 0.00758 0.00255 -0.0314 0.3735 0.9302 4.750 0.7032 0.00773 0.00269 -0.0339 0.3623 0.9412 5.000 0.7428 0.00793 0.00285 -0.0369 0.3489 0.9502 5.250 0.7859 0.00816 0.00304 -0.0406 0.3349 0.9547 5.500 0.8271 0.00841 0.00324 -0.0440 0.3193 0.9587 5.750 0.8643 0.00869 0.00346 -0.0464 0.3023 0.9635 6.000 0.9007 0.00900 0.00369 -0.0486 0.2850 0.9670 6.250 0.9351 0.00934 0.00395 -0.0505 0.2672 0.9704 6.500 0.9653 0.00984 0.00430 -0.0515 0.2360 0.9750 6.750 0.9924 0.01042 0.00470 -0.0520 0.2016 0.9821 7.250 1.0355 0.01198 0.00579 -0.0509 0.1220 0.9996 7.500 1.0331 0.01341 0.00679 -0.0457 0.0458 1.0000 7.750 1.0477 0.01385 0.00719 -0.0434 0.0365 1.0000 8.000 1.0644 0.01420 0.00753 -0.0415 0.0325 1.0000 8.250 1.0798 0.01458 0.00789 -0.0393 0.0291 1.0000 8.500 1.0933 0.01488 0.00822 -0.0367 0.0272 1.0000 8.750 1.1052 0.01522 0.00855 -0.0338 0.0252 1.0000 9.000 1.1168 0.01561 0.00895 -0.0310 0.0230 1.0000 9.250 1.1307 0.01597 0.00932 -0.0287 0.0217 1.0000 9.500 1.1442 0.01639 0.00976 -0.0265 0.0200 1.0000 9.750 1.1571 0.01689 0.01026 -0.0242 0.0184 1.0000 10.000 1.1717 0.01735 0.01075 -0.0223 0.0174 1.0000 10.250 1.1856 0.01788 0.01130 -0.0204 0.0162 1.0000 10.500 1.1987 0.01849 0.01192 -0.0186 0.0150 1.0000 10.750 1.2121 0.01912 0.01258 -0.0168 0.0142 1.0000 11.000 1.2257 0.01979 0.01328 -0.0152 0.0135 1.0000 11.250 1.2385 0.02053 0.01404 -0.0136 0.0127 1.0000 11.500 1.2505 0.02136 0.01490 -0.0120 0.0120 1.0000 11.750 1.2617 0.02229 0.01586 -0.0105 0.0114 1.0000 12.000 1.2738 0.02321 0.01682 -0.0092 0.0110 1.0000 12.250 1.2853 0.02420 0.01786 -0.0079 0.0106 1.0000 12.500 1.2960 0.02530 0.01900 -0.0067 0.0101 1.0000 12.750 1.3060 0.02649 0.02023 -0.0056 0.0097 1.0000 13.000 1.3149 0.02781 0.02160 -0.0044 0.0094 1.0000 13.250 1.3223 0.02930 0.02313 -0.0034 0.0090 1.0000 13.500 1.3290 0.03091 0.02479 -0.0024 0.0088 1.0000 13.750 1.3367 0.03249 0.02643 -0.0015 0.0086 1.0000 14.000 1.3433 0.03419 0.02820 -0.0008 0.0085 1.0000 14.250 1.3490 0.03603 0.03011 -0.0001 0.0083 1.0000 14.500 1.3538 0.03800 0.03215 0.0005 0.0082 1.0000 14.750 1.3579 0.04010 0.03432 0.0010 0.0080 1.0000 15.000 1.3610 0.04234 0.03663 0.0014 0.0078 1.0000 15.250 1.3634 0.04474 0.03910 0.0017 0.0077 1.0000 15.500 1.3648 0.04731 0.04173 0.0019 0.0076 1.0000 15.750 1.3655 0.05002 0.04451 0.0020 0.0074 1.0000 16.000 1.3650 0.05291 0.04748 0.0020 0.0073 1.0000 16.250 1.3636 0.05600 0.05064 0.0019 0.0072 1.0000 16.500 1.3611 0.05929 0.05401 0.0016 0.0071 1.0000 16.750 1.3572 0.06279 0.05760 0.0012 0.0070 1.0000 17.000 1.3520 0.06653 0.06142 0.0007 0.0068 1.0000 17.250 1.3452 0.07056 0.06553 0.0000 0.0067 1.0000 17.500 1.3382 0.07468 0.06975 -0.0008 0.0066 1.0000 17.750 1.3341 0.07844 0.07359 -0.0015 0.0066 1.0000 18.000 1.3292 0.08236 0.07760 -0.0024 0.0065 1.0000 18.250 1.3243 0.08635 0.08167 -0.0034 0.0065 1.0000 18.500 1.3185 0.09050 0.08590 -0.0045 0.0064 1.0000 18.750 1.3124 0.09471 0.09020 -0.0056 0.0064 1.0000 19.000 1.3061 0.09898 0.09456 -0.0068 0.0063 1.0000 19.250 1.2999 0.10330 0.09896 -0.0082 0.0062 1.0000