GEMINI (smoothed) (geminism-il) Xfoil prediction polar at RE=50,000 Ncrit=5
| Details | Polar file |
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Airfoil: GEMINI (smoothed) (geminism-il) Reynolds number: 50,000 Max Cl/Cd: 28.33 at α=8.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-geminism-il-50000-n5.txt Download as CSV file: xf-geminism-il-50000-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 = 0.050 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-12.000 -0.5131 0.09824 0.09071 -0.0542 1.0000 0.0645
-11.750 -0.5344 0.09013 0.08261 -0.0589 1.0000 0.0643
-11.500 -0.5596 0.08261 0.07508 -0.0632 1.0000 0.0639
-11.250 -0.5869 0.07621 0.06863 -0.0664 1.0000 0.0636
-11.000 -0.6146 0.07109 0.06343 -0.0677 1.0000 0.0633
-10.750 -0.6420 0.06713 0.05937 -0.0667 1.0000 0.0632
-10.500 -0.6690 0.06413 0.05628 -0.0635 1.0000 0.0632
-10.250 -0.6932 0.06138 0.05338 -0.0595 1.0000 0.0633
-10.000 -0.7133 0.05864 0.05043 -0.0556 1.0000 0.0637
-9.750 -0.7298 0.05603 0.04755 -0.0514 1.0000 0.0641
-9.500 -0.7411 0.05355 0.04483 -0.0473 1.0000 0.0647
-9.250 -0.7416 0.05129 0.04248 -0.0443 1.0000 0.0656
-9.000 -0.7416 0.04927 0.04033 -0.0412 1.0000 0.0665
-8.750 -0.7404 0.04747 0.03839 -0.0380 1.0000 0.0678
-8.500 -0.7383 0.04584 0.03661 -0.0349 1.0000 0.0697
-8.250 -0.7355 0.04419 0.03475 -0.0318 1.0000 0.0719
-8.000 -0.7313 0.04249 0.03273 -0.0288 1.0000 0.0741
-7.750 -0.7246 0.04082 0.03065 -0.0259 1.0000 0.0761
-7.500 -0.7132 0.03919 0.02891 -0.0238 1.0000 0.0780
-7.250 -0.7018 0.03796 0.02768 -0.0218 1.0000 0.0809
-7.000 -0.6802 0.03665 0.02619 -0.0216 0.9973 0.0856
-6.750 -0.6461 0.03509 0.02435 -0.0233 0.9911 0.0910
-6.500 -0.6132 0.03376 0.02302 -0.0250 0.9846 0.0971
-6.250 -0.5789 0.03256 0.02167 -0.0269 0.9783 0.1061
-6.000 -0.5479 0.03146 0.02052 -0.0281 0.9705 0.1159
-5.750 -0.5185 0.03041 0.01949 -0.0292 0.9625 0.1300
-5.500 -0.4873 0.02932 0.01850 -0.0308 0.9551 0.1514
-5.250 -0.4602 0.02826 0.01764 -0.0316 0.9463 0.1881
-5.000 -0.4340 0.02721 0.01689 -0.0322 0.9376 0.2477
-4.750 -0.4044 0.02632 0.01630 -0.0334 0.9300 0.3221
-4.500 -0.3814 0.02576 0.01603 -0.0330 0.9202 0.3888
-4.250 -0.3493 0.02535 0.01586 -0.0338 0.9133 0.4628
-4.000 -0.3288 0.02518 0.01589 -0.0322 0.9028 0.5281
-3.750 -0.3020 0.02513 0.01600 -0.0313 0.8946 0.5925
-3.500 -0.2732 0.02513 0.01602 -0.0308 0.8862 0.6398
-3.250 -0.2427 0.02511 0.01590 -0.0307 0.8779 0.6754
-3.000 -0.2095 0.02509 0.01581 -0.0311 0.8700 0.7075
-2.750 -0.1775 0.02514 0.01577 -0.0313 0.8616 0.7363
-2.500 -0.1418 0.02516 0.01567 -0.0321 0.8539 0.7641
-2.250 -0.1099 0.02522 0.01562 -0.0323 0.8452 0.7911
-2.000 -0.0678 0.02531 0.01558 -0.0342 0.8379 0.8154
-1.750 -0.0320 0.02540 0.01555 -0.0353 0.8294 0.8408
-1.500 0.0170 0.02551 0.01553 -0.0386 0.8221 0.8626
-1.250 0.0649 0.02561 0.01547 -0.0419 0.8144 0.8836
-1.000 0.1133 0.02564 0.01536 -0.0456 0.8062 0.9024
-0.750 0.1644 0.02561 0.01519 -0.0500 0.7979 0.9175
-0.500 0.2147 0.02552 0.01496 -0.0544 0.7893 0.9311
-0.250 0.2601 0.02546 0.01481 -0.0581 0.7795 0.9449
0.000 0.3097 0.02524 0.01446 -0.0624 0.7713 0.9572
0.250 0.3529 0.02520 0.01436 -0.0660 0.7601 0.9702
0.500 0.3992 0.02503 0.01410 -0.0700 0.7506 0.9823
0.750 0.4440 0.02488 0.01390 -0.0739 0.7404 0.9948
1.000 0.4719 0.02489 0.01387 -0.0748 0.7289 1.0000
1.250 0.4896 0.02487 0.01378 -0.0734 0.7187 1.0000
1.500 0.5063 0.02491 0.01378 -0.0718 0.7081 1.0000
1.750 0.5191 0.02511 0.01395 -0.0696 0.6966 1.0000
2.000 0.5378 0.02516 0.01395 -0.0681 0.6870 1.0000
2.250 0.5542 0.02532 0.01407 -0.0664 0.6766 1.0000
2.500 0.5679 0.02560 0.01434 -0.0642 0.6656 1.0000
2.750 0.5912 0.02560 0.01428 -0.0633 0.6572 1.0000
3.000 0.6039 0.02598 0.01466 -0.0609 0.6459 1.0000
3.250 0.6201 0.02628 0.01495 -0.0591 0.6358 1.0000
3.500 0.6435 0.02635 0.01501 -0.0581 0.6272 1.0000
3.750 0.6561 0.02684 0.01551 -0.0558 0.6162 1.0000
4.000 0.6776 0.02703 0.01569 -0.0546 0.6074 1.0000
4.250 0.6952 0.02739 0.01607 -0.0529 0.5975 1.0000
4.500 0.7109 0.02784 0.01656 -0.0510 0.5875 1.0000
4.750 0.7366 0.02793 0.01664 -0.0504 0.5794 1.0000
5.000 0.7481 0.02858 0.01735 -0.0479 0.5686 1.0000
5.250 0.7710 0.02881 0.01761 -0.0469 0.5602 1.0000
5.500 0.7873 0.02930 0.01816 -0.0451 0.5503 1.0000
5.750 0.8034 0.02984 0.01876 -0.0433 0.5408 1.0000
6.000 0.8282 0.03003 0.01898 -0.0425 0.5325 1.0000
6.250 0.8391 0.03080 0.01987 -0.0401 0.5223 1.0000
6.500 0.8677 0.03087 0.01997 -0.0398 0.5147 1.0000
6.750 0.8766 0.03176 0.02098 -0.0372 0.5042 1.0000
7.000 0.8959 0.03226 0.02156 -0.0358 0.4955 1.0000
7.250 0.9151 0.03275 0.02216 -0.0345 0.4865 1.0000
7.500 0.9270 0.03360 0.02313 -0.0323 0.4771 1.0000
7.750 0.9540 0.03378 0.02340 -0.0319 0.4692 1.0000
8.000 0.9590 0.03497 0.02474 -0.0290 0.4592 1.0000
8.250 0.9910 0.03498 0.02485 -0.0291 0.4520 1.0000
8.500 0.9905 0.03643 0.02648 -0.0257 0.4418 1.0000
8.750 1.0126 0.03692 0.02710 -0.0247 0.4340 1.0000
9.000 1.0215 0.03791 0.02825 -0.0223 0.4244 1.0000
9.250 1.0285 0.03878 0.02924 -0.0196 0.4133 1.0000
9.500 1.0409 0.03888 0.02943 -0.0169 0.3996 1.0000
9.750 1.0475 0.03908 0.02968 -0.0136 0.3845 1.0000
10.000 1.0505 0.03956 0.03021 -0.0102 0.3695 1.0000
10.250 1.0532 0.04029 0.03100 -0.0072 0.3550 1.0000
10.500 1.0538 0.04128 0.03207 -0.0044 0.3405 1.0000
10.750 1.0527 0.04258 0.03346 -0.0018 0.3258 1.0000
11.000 1.0472 0.04439 0.03539 0.0005 0.3098 1.0000
11.250 1.0391 0.04666 0.03777 0.0024 0.2922 1.0000
11.500 1.0314 0.04908 0.04026 0.0039 0.2715 1.0000
11.750 1.0238 0.05174 0.04295 0.0050 0.2480 1.0000
12.000 1.0162 0.05463 0.04582 0.0058 0.2218 1.0000
12.250 1.0063 0.05805 0.04918 0.0064 0.1910 1.0000
12.500 0.9947 0.06178 0.05272 0.0067 0.1552 1.0000
12.750 0.9804 0.06606 0.05673 0.0068 0.1262 1.0000
13.000 0.9659 0.07066 0.06111 0.0065 0.1079 1.0000
13.250 0.9531 0.07527 0.06556 0.0061 0.0964 1.0000
13.500 0.9429 0.07970 0.06990 0.0055 0.0882 1.0000
13.750 0.9354 0.08384 0.07398 0.0050 0.0821 1.0000
14.000 0.9300 0.08778 0.07790 0.0045 0.0771 1.0000
14.250 0.9261 0.09144 0.08149 0.0041 0.0733 1.0000
14.500 0.9262 0.09467 0.08483 0.0039 0.0691 1.0000
14.750 0.9262 0.09786 0.08801 0.0036 0.0656 1.0000
15.000 0.9284 0.10063 0.09073 0.0035 0.0627 1.0000
15.250 0.9336 0.10320 0.09346 0.0036 0.0601 1.0000
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