GOE 114 (MVA MK.1) AIRFOIL (goe114-il) Xfoil prediction polar at RE=200,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 114 (MVA MK.1) AIRFOIL (goe114-il) Reynolds number: 200,000 Max Cl/Cd: 60.91 at α=2.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe114-il-200000.txt Download as CSV file: xf-goe114-il-200000.csv |
XFOIL Version 6.96
Calculated polar for: GOE 114 (MVA MK.1) AIRFOIL
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
------ -------- --------- --------- -------- -------- --------
-8.750 -0.3872 0.08887 0.08562 -0.0451 1.0000 0.0349
-8.500 -0.3886 0.08617 0.08297 -0.0450 1.0000 0.0365
-8.250 -0.3944 0.08326 0.08013 -0.0449 1.0000 0.0377
-8.000 -0.4047 0.08068 0.07764 -0.0440 1.0000 0.0382
-7.750 -0.4233 0.07885 0.07592 -0.0413 1.0000 0.0384
-7.500 -0.4502 0.07801 0.07519 -0.0366 1.0000 0.0376
-7.250 -0.4734 0.07647 0.07374 -0.0337 1.0000 0.0370
-7.000 -0.4576 0.06932 0.06659 -0.0444 0.9947 0.0391
-6.750 -0.4335 0.05681 0.05388 -0.0633 0.9862 0.0402
-6.500 -0.4120 0.04694 0.04295 -0.0792 0.9758 0.0445
-6.250 -0.3876 0.04324 0.03959 -0.0808 0.9725 0.0515
-4.500 -0.1569 0.02042 0.01343 -0.0952 0.9424 0.0380
-4.000 -0.0898 0.01771 0.01038 -0.0957 0.9325 0.0280
-3.750 -0.0520 0.01647 0.00907 -0.0975 0.9299 0.0299
-3.500 -0.0247 0.01569 0.00821 -0.0973 0.9231 0.0315
-3.250 0.0092 0.01480 0.00711 -0.0984 0.9187 0.0318
-3.000 0.0466 0.01407 0.00607 -0.1000 0.9157 0.0351
-2.750 0.0718 0.01354 0.00546 -0.0993 0.9077 0.0621
-2.500 0.1034 0.01279 0.00558 -0.1004 0.9035 0.3299
-2.250 0.1302 0.01311 0.00576 -0.1000 0.8960 0.3596
-2.000 0.1604 0.01337 0.00607 -0.1003 0.8908 0.3952
-1.750 0.1870 0.01338 0.00603 -0.1000 0.8837 0.4111
-1.500 0.2172 0.01315 0.00571 -0.1004 0.8780 0.4172
-1.250 0.2447 0.01304 0.00554 -0.1003 0.8711 0.4241
-1.000 0.2736 0.01285 0.00532 -0.1005 0.8648 0.4300
-0.750 0.3007 0.01274 0.00520 -0.1003 0.8576 0.4370
-0.500 0.3292 0.01257 0.00503 -0.1004 0.8510 0.4437
-0.250 0.3556 0.01248 0.00495 -0.1001 0.8433 0.4498
0.000 0.3844 0.01232 0.00478 -0.1002 0.8369 0.4557
0.250 0.4102 0.01223 0.00476 -0.0998 0.8284 0.4615
0.500 0.4394 0.01209 0.00463 -0.0999 0.8224 0.4685
0.750 0.4643 0.01202 0.00466 -0.0994 0.8131 0.4762
1.000 0.4913 0.01191 0.00468 -0.0992 0.8054 0.4845
1.250 0.5168 0.01165 0.00447 -0.0982 0.7904 0.4946
1.500 0.5396 0.01113 0.00393 -0.0961 0.7611 0.5067
1.750 0.5645 0.01091 0.00385 -0.0952 0.7451 0.5238
2.000 0.5877 0.01064 0.00378 -0.0939 0.7238 0.5553
2.250 0.6018 0.00988 0.00340 -0.0900 0.6560 0.7180
2.500 0.6328 0.01048 0.00341 -0.0902 0.4684 1.0000
2.750 0.6209 0.01363 0.00455 -0.0839 0.0527 1.0000
3.000 0.6433 0.01413 0.00503 -0.0827 0.0350 1.0000
3.250 0.6651 0.01469 0.00574 -0.0813 0.0308 1.0000
3.500 0.6860 0.01528 0.00645 -0.0799 0.0263 1.0000
3.750 0.7049 0.01603 0.00735 -0.0781 0.0260 1.0000
4.000 0.7210 0.01699 0.00839 -0.0758 0.0264 1.0000
4.250 0.7358 0.01810 0.00954 -0.0733 0.0277 1.0000
4.500 0.7507 0.01950 0.01098 -0.0708 0.0296 1.0000
4.750 0.7720 0.02098 0.01239 -0.0693 0.0322 1.0000
5.000 0.8003 0.02173 0.01331 -0.0681 0.0396 1.0000
6.500 0.9841 0.03466 0.02722 -0.0644 0.0514 1.0000
6.750 0.9963 0.03757 0.03041 -0.0627 0.0398 1.0000
7.000 1.0125 0.03997 0.03293 -0.0614 0.0337 1.0000
7.250 1.0209 0.04304 0.03642 -0.0586 0.0284 1.0000
7.500 1.0337 0.04499 0.03870 -0.0560 0.0253 1.0000
7.750 1.0440 0.04799 0.04189 -0.0541 0.0230 1.0000
8.000 1.0559 0.05291 0.04681 -0.0535 0.0214 1.0000
8.250 1.0497 0.06217 0.05634 -0.0513 0.0202 1.0000
8.500 1.0502 0.06424 0.05874 -0.0480 0.0201 1.0000
8.750 1.0475 0.06457 0.05945 -0.0438 0.0196 1.0000
9.000 1.0455 0.06571 0.06091 -0.0400 0.0189 1.0000
9.250 1.0396 0.06796 0.06341 -0.0365 0.0184 1.0000
9.500 1.0282 0.07042 0.06607 -0.0328 0.0181 1.0000
9.750 1.0135 0.07313 0.06894 -0.0295 0.0179 1.0000
10.000 0.9979 0.07621 0.07218 -0.0272 0.0178 1.0000
10.250 0.9809 0.07974 0.07585 -0.0259 0.0178 1.0000
10.500 0.9633 0.08374 0.07998 -0.0255 0.0179 1.0000
10.750 0.9444 0.08832 0.08469 -0.0262 0.0179 1.0000
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Polar data table (+)
Polar graphs
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