GEMINI (smoothed) (geminism-il) Xfoil prediction polar at RE=200,000 Ncrit=9
| Details | Polar file |
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Airfoil: GEMINI (smoothed) (geminism-il) Reynolds number: 200,000 Max Cl/Cd: 66.92 at α=7.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-geminism-il-200000.txt Download as CSV file: xf-geminism-il-200000.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 = 0.200 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-12.000 -0.6326 0.06869 0.06473 -0.0713 1.0000 0.0459
-11.750 -0.6831 0.06211 0.05781 -0.0737 1.0000 0.0438
-11.500 -0.7056 0.05818 0.05378 -0.0725 1.0000 0.0435
-11.250 -0.7297 0.05511 0.05059 -0.0694 1.0000 0.0432
-11.000 -0.7549 0.05277 0.04815 -0.0643 1.0000 0.0430
-10.750 -0.7774 0.05040 0.04565 -0.0589 1.0000 0.0428
-10.500 -0.7977 0.04814 0.04323 -0.0533 1.0000 0.0427
-10.250 -0.8164 0.04606 0.04097 -0.0476 1.0000 0.0427
-10.000 -0.8330 0.04411 0.03883 -0.0418 1.0000 0.0427
-9.750 -0.8465 0.04222 0.03672 -0.0363 1.0000 0.0428
-9.500 -0.8563 0.04037 0.03462 -0.0314 1.0000 0.0430
-9.250 -0.8371 0.03780 0.03155 -0.0318 0.9959 0.0439
-9.000 -0.8140 0.03410 0.02748 -0.0331 0.9911 0.0455
-8.750 -0.7810 0.03219 0.02546 -0.0354 0.9872 0.0472
-8.500 -0.7494 0.03044 0.02353 -0.0371 0.9819 0.0488
-8.250 -0.7135 0.02879 0.02162 -0.0394 0.9786 0.0510
-8.000 -0.6822 0.02773 0.02026 -0.0405 0.9718 0.0532
-7.750 -0.6459 0.02538 0.01777 -0.0429 0.9690 0.0556
-7.500 -0.6140 0.02419 0.01657 -0.0442 0.9625 0.0580
-7.250 -0.5758 0.02320 0.01549 -0.0466 0.9584 0.0617
-7.000 -0.5397 0.02242 0.01452 -0.0484 0.9532 0.0645
-6.750 -0.5064 0.02072 0.01292 -0.0501 0.9480 0.0687
-6.500 -0.4657 0.01982 0.01199 -0.0530 0.9448 0.0744
-6.250 -0.4341 0.01873 0.01091 -0.0541 0.9386 0.0801
-6.000 -0.4001 0.01789 0.01006 -0.0556 0.9327 0.0880
-5.750 -0.3642 0.01685 0.00907 -0.0576 0.9288 0.1010
-5.500 -0.3430 0.01607 0.00837 -0.0565 0.9182 0.1193
-5.250 -0.3195 0.01492 0.00769 -0.0561 0.9105 0.1897
-5.000 -0.2971 0.01415 0.00726 -0.0553 0.9015 0.2722
-4.750 -0.2746 0.01363 0.00694 -0.0544 0.8924 0.3260
-4.500 -0.2489 0.01313 0.00662 -0.0540 0.8845 0.3815
-4.250 -0.2288 0.01280 0.00645 -0.0523 0.8745 0.4336
-4.000 -0.2026 0.01243 0.00623 -0.0518 0.8673 0.4881
-3.750 -0.1830 0.01227 0.00616 -0.0499 0.8567 0.5319
-3.500 -0.1570 0.01207 0.00602 -0.0492 0.8493 0.5729
-3.250 -0.1357 0.01197 0.00597 -0.0475 0.8392 0.6084
-3.000 -0.1122 0.01188 0.00591 -0.0462 0.8308 0.6443
-2.750 -0.0887 0.01180 0.00588 -0.0448 0.8218 0.6772
-2.500 -0.0647 0.01175 0.00587 -0.0436 0.8129 0.7038
-2.250 -0.0384 0.01168 0.00575 -0.0429 0.8045 0.7262
-2.000 -0.0135 0.01165 0.00573 -0.0420 0.7952 0.7453
-1.750 0.0153 0.01159 0.00564 -0.0418 0.7874 0.7648
-1.500 0.0398 0.01158 0.00564 -0.0408 0.7775 0.7840
-1.000 0.0941 0.01156 0.00557 -0.0399 0.7598 0.8220
-0.750 0.1230 0.01158 0.00554 -0.0397 0.7515 0.8404
-0.500 0.1521 0.01161 0.00555 -0.0396 0.7420 0.8578
-0.250 0.1835 0.01168 0.00559 -0.0400 0.7329 0.8747
0.000 0.2180 0.01177 0.00563 -0.0410 0.7239 0.8916
0.250 0.2538 0.01193 0.00577 -0.0422 0.7139 0.9083
0.500 0.2925 0.01208 0.00581 -0.0440 0.7053 0.9225
0.750 0.3370 0.01223 0.00592 -0.0474 0.6943 0.9302
1.000 0.3771 0.01234 0.00597 -0.0498 0.6842 0.9399
1.250 0.4229 0.01246 0.00599 -0.0535 0.6745 0.9463
1.500 0.4633 0.01257 0.00607 -0.0561 0.6629 0.9546
1.750 0.5053 0.01268 0.00612 -0.0592 0.6521 0.9624
2.000 0.5493 0.01276 0.00609 -0.0626 0.6420 0.9688
2.250 0.5896 0.01284 0.00616 -0.0655 0.6298 0.9772
2.500 0.6324 0.01292 0.00621 -0.0689 0.6182 0.9845
2.750 0.6756 0.01297 0.00620 -0.0724 0.6071 0.9915
3.000 0.7193 0.01299 0.00617 -0.0761 0.5955 0.9980
3.250 0.7472 0.01301 0.00619 -0.0767 0.5840 1.0000
3.500 0.7672 0.01307 0.00622 -0.0756 0.5742 1.0000
3.750 0.7873 0.01314 0.00624 -0.0744 0.5643 1.0000
4.000 0.8067 0.01323 0.00634 -0.0731 0.5538 1.0000
4.250 0.8273 0.01335 0.00641 -0.0719 0.5446 1.0000
4.500 0.8465 0.01348 0.00655 -0.0704 0.5344 1.0000
4.750 0.8660 0.01364 0.00671 -0.0690 0.5248 1.0000
5.000 0.8867 0.01382 0.00682 -0.0678 0.5159 1.0000
5.250 0.9050 0.01400 0.00705 -0.0661 0.5058 1.0000
5.500 0.9254 0.01421 0.00724 -0.0648 0.4971 1.0000
5.750 0.9442 0.01441 0.00746 -0.0632 0.4873 1.0000
6.000 0.9627 0.01462 0.00768 -0.0615 0.4767 1.0000
6.250 0.9813 0.01482 0.00785 -0.0598 0.4654 1.0000
6.500 0.9988 0.01501 0.00802 -0.0579 0.4533 1.0000
6.750 1.0156 0.01522 0.00828 -0.0558 0.4414 1.0000
7.000 1.0333 0.01546 0.00853 -0.0540 0.4301 1.0000
7.250 1.0506 0.01570 0.00876 -0.0520 0.4182 1.0000
7.500 1.0672 0.01595 0.00901 -0.0500 0.4062 1.0000
7.750 1.0828 0.01619 0.00931 -0.0477 0.3934 1.0000
8.000 1.0979 0.01646 0.00961 -0.0454 0.3802 1.0000
8.250 1.1116 0.01674 0.00991 -0.0428 0.3653 1.0000
8.500 1.1244 0.01705 0.01024 -0.0401 0.3497 1.0000
8.750 1.1353 0.01740 0.01059 -0.0371 0.3324 1.0000
9.000 1.1422 0.01784 0.01098 -0.0334 0.3100 1.0000
9.250 1.1443 0.01839 0.01146 -0.0290 0.2825 1.0000
9.500 1.1389 0.01922 0.01210 -0.0234 0.2417 1.0000
9.750 1.1245 0.02076 0.01323 -0.0172 0.1821 1.0000
10.000 1.1033 0.02314 0.01508 -0.0111 0.1076 1.0000
10.250 1.0878 0.02560 0.01721 -0.0065 0.0705 1.0000
10.500 1.0841 0.02754 0.01914 -0.0035 0.0609 1.0000
10.750 1.0823 0.02949 0.02114 -0.0010 0.0558 1.0000
11.000 1.0780 0.03177 0.02349 0.0012 0.0521 1.0000
11.250 1.0788 0.03378 0.02561 0.0028 0.0491 1.0000
11.500 1.0766 0.03614 0.02805 0.0043 0.0467 1.0000
11.750 1.0698 0.03900 0.03096 0.0058 0.0448 1.0000
12.000 1.0623 0.04200 0.03399 0.0072 0.0433 1.0000
12.250 1.0651 0.04418 0.03627 0.0081 0.0420 1.0000
12.500 1.0672 0.04643 0.03860 0.0090 0.0406 1.0000
12.750 1.0700 0.04863 0.04086 0.0099 0.0392 1.0000
13.000 1.0733 0.05078 0.04303 0.0108 0.0378 1.0000
13.250 1.0783 0.05270 0.04489 0.0120 0.0363 1.0000
13.500 1.0891 0.05411 0.04630 0.0136 0.0349 1.0000
13.750 1.0989 0.05578 0.04807 0.0144 0.0339 1.0000
14.000 1.1108 0.05727 0.04964 0.0153 0.0330 1.0000
14.250 1.1236 0.05875 0.05121 0.0163 0.0321 1.0000
14.500 1.1369 0.06025 0.05277 0.0173 0.0313 1.0000
14.750 1.1499 0.06186 0.05446 0.0182 0.0307 1.0000
15.000 1.1641 0.06348 0.05612 0.0190 0.0299 1.0000
15.250 1.2046 0.06480 0.05739 0.0208 0.0286 1.0000
15.500 1.1973 0.06772 0.06053 0.0211 0.0283 1.0000
15.750 1.1916 0.07084 0.06387 0.0212 0.0281 1.0000
16.000 1.1870 0.07416 0.06740 0.0212 0.0278 1.0000
16.250 1.1825 0.07771 0.07118 0.0211 0.0277 1.0000
16.500 1.1761 0.08159 0.07527 0.0208 0.0276 1.0000
16.750 1.1676 0.08581 0.07970 0.0202 0.0276 1.0000
17.000 1.1573 0.09037 0.08447 0.0193 0.0276 1.0000
17.250 1.1451 0.09527 0.08958 0.0180 0.0277 1.0000
17.500 1.1317 0.10054 0.09504 0.0164 0.0278 1.0000
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