GEMINI (smoothed) (geminism-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: GEMINI (smoothed) (geminism-il) Reynolds number: 1,000,000 Max Cl/Cd: 100.12 at α=6.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-geminism-il-1000000-n5.txt Download as CSV file: xf-geminism-il-1000000-n5.csv |
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 0.03939 0.03525 -0.0724 1.0000 0.0094
-16.250 -1.1935 0.03668 0.03243 -0.0730 1.0000 0.0095
-16.000 -1.1922 0.03430 0.02996 -0.0732 1.0000 0.0096
-15.750 -1.1896 0.03222 0.02778 -0.0730 1.0000 0.0097
-15.500 -1.1856 0.03041 0.02588 -0.0726 1.0000 0.0098
-15.250 -1.1820 0.02872 0.02411 -0.0717 1.0000 0.0099
-15.000 -1.1793 0.02711 0.02242 -0.0704 1.0000 0.0101
-14.750 -1.1744 0.02580 0.02104 -0.0689 1.0000 0.0103
-14.500 -1.1682 0.02470 0.01988 -0.0671 1.0000 0.0105
-14.250 -1.1613 0.02374 0.01887 -0.0650 1.0000 0.0107
-14.000 -1.1544 0.02291 0.01799 -0.0626 1.0000 0.0110
-13.750 -1.1478 0.02220 0.01722 -0.0599 1.0000 0.0112
-13.500 -1.1424 0.02159 0.01656 -0.0567 1.0000 0.0114
-13.250 -1.1398 0.02109 0.01602 -0.0526 1.0000 0.0117
-12.750 -1.1017 0.01982 0.01463 -0.0510 0.9899 0.0123
-12.500 -1.0757 0.01918 0.01393 -0.0515 0.9846 0.0125
-12.250 -1.0478 0.01843 0.01312 -0.0525 0.9821 0.0130
-11.750 -0.9866 0.01716 0.01179 -0.0553 0.9777 0.0140
-11.500 -0.9571 0.01663 0.01122 -0.0563 0.9722 0.0145
-11.000 -0.8922 0.01563 0.01011 -0.0595 0.9599 0.0155
-10.750 -0.8577 0.01516 0.00959 -0.0615 0.9518 0.0159
-10.500 -0.8235 0.01460 0.00899 -0.0635 0.9426 0.0167
-10.250 -0.7917 0.01418 0.00853 -0.0649 0.9316 0.0175
-10.000 -0.7639 0.01384 0.00813 -0.0653 0.9185 0.0183
-9.750 -0.7382 0.01354 0.00775 -0.0652 0.9039 0.0189
-9.500 -0.7137 0.01327 0.00739 -0.0647 0.8880 0.0195
-9.250 -0.6902 0.01301 0.00704 -0.0641 0.8723 0.0199
-9.000 -0.6679 0.01270 0.00666 -0.0632 0.8574 0.0208
-8.750 -0.6450 0.01245 0.00635 -0.0623 0.8439 0.0218
-8.500 -0.6219 0.01223 0.00607 -0.0615 0.8314 0.0227
-8.250 -0.5985 0.01203 0.00579 -0.0608 0.8195 0.0236
-8.000 -0.5746 0.01184 0.00553 -0.0601 0.8087 0.0242
-7.750 -0.5514 0.01160 0.00524 -0.0593 0.7982 0.0253
-7.500 -0.5281 0.01138 0.00498 -0.0585 0.7876 0.0267
-7.250 -0.5041 0.01118 0.00474 -0.0578 0.7776 0.0280
-7.000 -0.4800 0.01101 0.00451 -0.0571 0.7677 0.0291
-6.750 -0.4556 0.01085 0.00429 -0.0565 0.7577 0.0300
-6.500 -0.4316 0.01064 0.00406 -0.0558 0.7484 0.0322
-6.000 -0.3826 0.01033 0.00367 -0.0546 0.7293 0.0361
-5.750 -0.3583 0.01017 0.00348 -0.0539 0.7203 0.0390
-5.500 -0.3336 0.01001 0.00330 -0.0533 0.7111 0.0424
-5.250 -0.3089 0.00987 0.00314 -0.0527 0.7030 0.0463
-5.000 -0.2842 0.00972 0.00297 -0.0522 0.6943 0.0520
-4.750 -0.2595 0.00957 0.00282 -0.0516 0.6864 0.0582
-4.500 -0.2346 0.00943 0.00267 -0.0510 0.6779 0.0653
-4.250 -0.2101 0.00927 0.00253 -0.0504 0.6703 0.0766
-4.000 -0.1861 0.00907 0.00237 -0.0496 0.6618 0.0937
-3.750 -0.1630 0.00882 0.00221 -0.0488 0.6539 0.1220
-3.500 -0.1400 0.00858 0.00207 -0.0479 0.6455 0.1586
-3.250 -0.1162 0.00838 0.00196 -0.0471 0.6377 0.1880
-3.000 -0.0915 0.00826 0.00187 -0.0465 0.6292 0.2089
-2.750 -0.0667 0.00814 0.00179 -0.0459 0.6214 0.2276
-2.500 -0.0425 0.00801 0.00171 -0.0453 0.6128 0.2531
-2.250 -0.0191 0.00781 0.00162 -0.0444 0.6049 0.2917
-2.000 0.0038 0.00761 0.00154 -0.0435 0.5960 0.3356
-1.750 0.0263 0.00738 0.00148 -0.0425 0.5878 0.3885
-1.500 0.0489 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
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