GEMINI (smoothed) (geminism-il) Xfoil prediction polar at RE=100,000 Ncrit=9
| Details | Polar file |
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Airfoil: GEMINI (smoothed) (geminism-il) Reynolds number: 100,000 Max Cl/Cd: 47.28 at α=9.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-geminism-il-100000.txt Download as CSV file: xf-geminism-il-100000.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 = 0.100 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-10.750 -0.4029 0.10952 0.10435 -0.0368 1.0000 0.1689
-10.500 -0.5807 0.07263 0.06762 -0.0655 1.0000 0.0922
-10.250 -0.6141 0.06772 0.06262 -0.0644 1.0000 0.0873
-10.000 -0.6415 0.06461 0.05950 -0.0606 1.0000 0.0859
-9.750 -0.6726 0.06148 0.05630 -0.0558 1.0000 0.0843
-9.500 -0.7082 0.05812 0.05277 -0.0500 1.0000 0.0822
-9.250 -0.7778 0.05477 0.04861 -0.0389 1.0000 0.0773
-9.000 -0.7875 0.05315 0.04672 -0.0342 1.0000 0.0768
-8.750 -0.7957 0.05035 0.04368 -0.0301 1.0000 0.0769
-8.500 -0.8008 0.04705 0.04016 -0.0265 1.0000 0.0774
-8.250 -0.8002 0.04423 0.03717 -0.0235 1.0000 0.0784
-8.000 -0.7962 0.04198 0.03474 -0.0207 1.0000 0.0793
-7.750 -0.7904 0.03983 0.03233 -0.0180 1.0000 0.0799
-7.500 -0.7818 0.03786 0.03011 -0.0155 1.0000 0.0807
-7.250 -0.7703 0.03630 0.02834 -0.0135 1.0000 0.0826
-7.000 -0.7556 0.03483 0.02661 -0.0120 0.9995 0.0853
-6.750 -0.7181 0.03292 0.02418 -0.0143 0.9940 0.0885
-6.500 -0.6805 0.03074 0.02174 -0.0166 0.9886 0.0918
-6.250 -0.6425 0.02937 0.02035 -0.0193 0.9823 0.0981
-6.000 -0.6027 0.02826 0.01893 -0.0217 0.9762 0.1038
-5.750 -0.5648 0.02678 0.01765 -0.0242 0.9701 0.1124
-5.500 -0.5302 0.02569 0.01657 -0.0259 0.9629 0.1226
-5.250 -0.4912 0.02464 0.01565 -0.0285 0.9569 0.1386
-5.000 -0.4629 0.02375 0.01491 -0.0290 0.9479 0.1637
-4.750 -0.4324 0.02236 0.01411 -0.0302 0.9412 0.2395
-4.500 -0.4101 0.02122 0.01368 -0.0298 0.9321 0.3584
-4.250 -0.3844 0.02079 0.01361 -0.0296 0.9233 0.4433
-4.000 -0.3513 0.02053 0.01359 -0.0304 0.9157 0.5176
-3.750 -0.3276 0.02048 0.01367 -0.0294 0.9059 0.5733
-3.500 -0.2898 0.02039 0.01369 -0.0306 0.8997 0.6303
-3.250 -0.2683 0.02048 0.01385 -0.0288 0.8893 0.6748
-3.000 -0.2286 0.02051 0.01396 -0.0297 0.8840 0.7266
-2.750 -0.2051 0.02069 0.01419 -0.0279 0.8740 0.7615
-2.500 -0.1603 0.02063 0.01407 -0.0300 0.8689 0.7927
-2.250 -0.1287 0.02078 0.01418 -0.0299 0.8600 0.8169
-2.000 -0.0854 0.02074 0.01405 -0.0318 0.8540 0.8418
-1.750 -0.0343 0.02078 0.01398 -0.0352 0.8486 0.8614
-1.500 0.0104 0.02093 0.01404 -0.0378 0.8401 0.8795
-1.250 0.0739 0.02082 0.01378 -0.0436 0.8359 0.8945
-1.000 0.1239 0.02098 0.01385 -0.0474 0.8267 0.9097
-0.750 0.1907 0.02084 0.01357 -0.0540 0.8209 0.9232
-0.500 0.2500 0.02085 0.01349 -0.0598 0.8119 0.9367
-0.250 0.3136 0.02055 0.01307 -0.0663 0.8043 0.9471
0.000 0.3625 0.02043 0.01289 -0.0707 0.7931 0.9594
0.250 0.4147 0.02010 0.01246 -0.0755 0.7841 0.9704
0.500 0.4639 0.01985 0.01215 -0.0801 0.7727 0.9817
0.750 0.5127 0.01962 0.01187 -0.0848 0.7607 0.9929
1.000 0.5556 0.01931 0.01150 -0.0884 0.7497 1.0000
1.250 0.5746 0.01917 0.01128 -0.0873 0.7392 1.0000
1.500 0.5900 0.01921 0.01130 -0.0857 0.7268 1.0000
1.750 0.6073 0.01922 0.01127 -0.0843 0.7156 1.0000
2.000 0.6292 0.01908 0.01106 -0.0834 0.7064 1.0000
2.250 0.6445 0.01922 0.01120 -0.0816 0.6941 1.0000
2.500 0.6620 0.01932 0.01128 -0.0801 0.6832 1.0000
2.750 0.6852 0.01925 0.01113 -0.0792 0.6744 1.0000
3.000 0.6999 0.01949 0.01139 -0.0772 0.6624 1.0000
3.250 0.7179 0.01967 0.01156 -0.0756 0.6521 1.0000
3.500 0.7413 0.01968 0.01149 -0.0747 0.6430 1.0000
3.750 0.7562 0.01999 0.01185 -0.0726 0.6316 1.0000
4.000 0.7765 0.02016 0.01201 -0.0712 0.6221 1.0000
4.250 0.7980 0.02029 0.01211 -0.0700 0.6123 1.0000
4.500 0.8140 0.02065 0.01251 -0.0680 0.6017 1.0000
4.750 0.8393 0.02073 0.01254 -0.0674 0.5932 1.0000
5.000 0.8556 0.02108 0.01295 -0.0654 0.5824 1.0000
5.250 0.8743 0.02141 0.01331 -0.0638 0.5726 1.0000
5.500 0.8999 0.02152 0.01339 -0.0632 0.5637 1.0000
5.750 0.9147 0.02200 0.01396 -0.0609 0.5531 1.0000
6.000 0.9385 0.02223 0.01417 -0.0601 0.5442 1.0000
6.250 0.9582 0.02257 0.01456 -0.0586 0.5342 1.0000
6.500 0.9759 0.02303 0.01511 -0.0569 0.5244 1.0000
6.750 1.0041 0.02316 0.01520 -0.0567 0.5159 1.0000
7.000 1.0172 0.02374 0.01593 -0.0542 0.5051 1.0000
7.250 1.0380 0.02397 0.01618 -0.0528 0.4939 1.0000
7.500 1.0613 0.02392 0.01611 -0.0516 0.4809 1.0000
7.750 1.0828 0.02384 0.01599 -0.0500 0.4665 1.0000
8.000 1.1030 0.02385 0.01599 -0.0483 0.4525 1.0000
8.250 1.1164 0.02412 0.01635 -0.0457 0.4392 1.0000
8.500 1.1311 0.02430 0.01662 -0.0432 0.4252 1.0000
8.750 1.1452 0.02442 0.01679 -0.0406 0.4106 1.0000
9.000 1.1580 0.02458 0.01701 -0.0378 0.3960 1.0000
9.250 1.1678 0.02470 0.01718 -0.0345 0.3797 1.0000
9.500 1.1746 0.02486 0.01740 -0.0307 0.3627 1.0000
9.750 1.1762 0.02504 0.01758 -0.0261 0.3424 1.0000
10.000 1.1691 0.02549 0.01812 -0.0203 0.3188 1.0000
10.250 1.1590 0.02619 0.01879 -0.0144 0.2913 1.0000
10.500 1.1449 0.02749 0.01993 -0.0088 0.2518 1.0000
10.750 1.1258 0.02972 0.02182 -0.0039 0.1953 1.0000
11.000 1.1033 0.03285 0.02451 0.0002 0.1407 1.0000
11.250 1.0839 0.03628 0.02763 0.0032 0.1105 1.0000
11.500 1.0699 0.03961 0.03082 0.0053 0.0966 1.0000
11.750 1.0591 0.04287 0.03405 0.0068 0.0884 1.0000
12.000 1.0502 0.04611 0.03731 0.0080 0.0828 1.0000
12.250 1.0434 0.04927 0.04051 0.0090 0.0781 1.0000
12.500 1.0349 0.05256 0.04378 0.0099 0.0748 1.0000
12.750 1.0357 0.05497 0.04626 0.0110 0.0716 1.0000
13.000 1.0393 0.05709 0.04841 0.0121 0.0682 1.0000
13.250 1.0471 0.05862 0.04983 0.0137 0.0646 1.0000
13.500 1.0649 0.05938 0.05055 0.0157 0.0612 1.0000
13.750 1.0845 0.06030 0.05153 0.0172 0.0586 1.0000
14.000 1.1108 0.06100 0.05222 0.0189 0.0563 1.0000
14.250 1.1747 0.06137 0.05238 0.0204 0.0528 1.0000
14.500 1.1756 0.06391 0.05520 0.0213 0.0520 1.0000
14.750 1.1774 0.06668 0.05823 0.0220 0.0511 1.0000
15.000 1.1794 0.06971 0.06151 0.0227 0.0506 1.0000
15.250 1.1786 0.07309 0.06515 0.0232 0.0503 1.0000
15.500 1.1731 0.07686 0.06918 0.0235 0.0503 1.0000
15.750 1.1637 0.08099 0.07358 0.0235 0.0503 1.0000
16.000 1.1507 0.08551 0.07835 0.0231 0.0505 1.0000
16.250 1.1349 0.09045 0.08354 0.0222 0.0507 1.0000
16.500 1.1169 0.09585 0.08916 0.0208 0.0510 1.0000
16.750 1.0972 0.10170 0.09524 0.0189 0.0513 1.0000
17.000 1.0767 0.10805 0.10179 0.0164 0.0517 1.0000
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