FX 75-VG-166/22 (fx75vg166-il) Xfoil prediction polar at RE=200,000 Ncrit=9
| Details | Polar file |
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Airfoil: FX 75-VG-166/22 (fx75vg166-il) Reynolds number: 200,000 Max Cl/Cd: 43.08 at α=9.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx75vg166-il-200000.txt Download as CSV file: xf-fx75vg166-il-200000.csv |
XFOIL Version 6.96
Calculated polar for: FX 75-VG-166/22
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
------ -------- --------- --------- -------- -------- --------
-13.000 -0.1398 0.10241 0.09830 -0.1020 0.8337 0.0666
-12.750 -0.1668 0.09637 0.09230 -0.1076 0.8335 0.0677
-12.500 -0.1674 0.09095 0.08690 -0.1085 0.8328 0.0688
-12.250 -0.1466 0.08968 0.08561 -0.1068 0.8317 0.0703
-12.000 -0.1387 0.08707 0.08300 -0.1070 0.8311 0.0721
-11.750 -0.1383 0.08354 0.07948 -0.1081 0.8304 0.0739
-11.500 -0.1455 0.07885 0.07481 -0.1102 0.8301 0.0761
-11.250 -0.1937 0.06803 0.06403 -0.1185 0.8299 0.0793
-11.000 -0.2214 0.06183 0.05779 -0.1214 0.8295 0.0792
-10.750 -0.2696 0.05673 0.05259 -0.1221 0.8290 0.0797
-10.500 -0.2983 0.05331 0.04909 -0.1206 0.8283 0.0797
-10.250 -0.3235 0.05054 0.04624 -0.1182 0.8276 0.0798
-10.000 -0.3671 0.04971 0.04528 -0.1121 0.8266 0.0803
-9.750 -0.3963 0.04895 0.04441 -0.1060 0.8254 0.0806
-9.000 -0.4941 0.04043 0.03358 -0.0937 0.8230 0.0390
-8.750 -0.4784 0.03761 0.03059 -0.0925 0.8215 0.0382
-8.500 -0.4652 0.03527 0.02800 -0.0907 0.8202 0.0380
-8.250 -0.4488 0.03340 0.02586 -0.0892 0.8191 0.0380
-8.000 -0.4328 0.03220 0.02436 -0.0875 0.8180 0.0385
-7.750 -0.4050 0.02996 0.02200 -0.0881 0.8170 0.0403
-7.500 -0.3818 0.02917 0.02119 -0.0878 0.8160 0.0424
-7.250 -0.3537 0.02814 0.02003 -0.0879 0.8150 0.0439
-7.000 -0.3245 0.02727 0.01900 -0.0882 0.8140 0.0459
-6.750 -0.2876 0.02608 0.01781 -0.0900 0.8130 0.0492
-6.500 -0.2643 0.02551 0.01729 -0.0896 0.8113 0.0527
-6.250 -0.2413 0.02503 0.01678 -0.0891 0.8100 0.0557
-6.000 -0.2234 0.02440 0.01623 -0.0879 0.8087 0.0598
-5.750 -0.2131 0.02430 0.01616 -0.0854 0.8067 0.0645
-5.500 -0.2055 0.02411 0.01597 -0.0822 0.8046 0.0694
-5.250 -0.2002 0.02397 0.01588 -0.0788 0.8029 0.0764
-5.000 -0.1931 0.02378 0.01574 -0.0755 0.8010 0.0883
-4.750 -0.1871 0.02350 0.01561 -0.0720 0.7990 0.1160
-4.500 -0.1965 0.02315 0.01578 -0.0665 0.7969 0.1987
-4.250 -0.2182 0.02306 0.01625 -0.0594 0.7943 0.2998
-4.000 -0.2393 0.02288 0.01663 -0.0521 0.7909 0.4121
-3.750 -0.2583 0.02266 0.01728 -0.0444 0.7889 0.5662
-3.500 -0.2302 0.02562 0.02085 -0.0396 0.7874 0.7287
-3.250 -0.1978 0.02699 0.02206 -0.0392 0.7856 0.7589
-3.000 -0.2151 0.02802 0.02307 -0.0320 0.7809 0.7715
-2.750 -0.2618 0.02852 0.02357 -0.0213 0.7768 0.7799
-2.500 -0.2370 0.02982 0.02478 -0.0190 0.7736 0.7963
-2.250 -0.2893 0.03123 0.02628 -0.0092 0.7885 0.7982
-2.000 -0.2183 0.03186 0.02674 -0.0103 0.7640 0.8185
-1.750 -0.2089 0.03272 0.02757 -0.0063 0.7610 0.8319
-1.250 0.0011 0.03514 0.02968 -0.0279 0.7592 0.8716
-1.000 0.0954 0.03502 0.02940 -0.0402 0.7588 0.8727
-0.750 0.1664 0.03487 0.02916 -0.0482 0.7580 0.8758
-0.500 0.2094 0.03474 0.02895 -0.0510 0.7567 0.8807
0.000 0.1465 0.03584 0.03009 -0.0314 0.7426 0.9008
0.250 0.2221 0.03564 0.02981 -0.0404 0.7420 0.9024
0.500 0.2813 0.03540 0.02951 -0.0462 0.7411 0.9046
0.750 0.3281 0.03523 0.02931 -0.0497 0.7399 0.9076
1.250 0.0962 0.03560 0.02974 0.0000 0.7119 0.9285
1.500 0.1441 0.03560 0.02970 -0.0039 0.7108 0.9288
1.750 0.2016 0.03563 0.02970 -0.0094 0.7101 0.9292
2.000 0.2598 0.03564 0.02969 -0.0152 0.7094 0.9295
2.250 0.1026 0.03522 0.02928 0.0153 0.6881 0.9400
2.500 0.1052 0.03478 0.02881 0.0198 0.6840 0.9427
2.750 0.1426 0.03455 0.02854 0.0182 0.6821 0.9431
3.000 0.1797 0.03435 0.02832 0.0167 0.6809 0.9433
3.250 0.1625 0.03441 0.02839 0.0226 0.6695 0.9454
3.500 0.1980 0.03411 0.02808 0.0215 0.6677 0.9457
3.750 0.2370 0.03382 0.02779 0.0198 0.6665 0.9461
4.000 0.2225 0.03414 0.02811 0.0251 0.6551 0.9487
4.250 0.2560 0.03384 0.02781 0.0243 0.6533 0.9490
4.500 0.2917 0.03352 0.02752 0.0231 0.6521 0.9492
4.750 0.2821 0.03397 0.02797 0.0276 0.6407 0.9510
5.000 0.3165 0.03362 0.02764 0.0266 0.6389 0.9517
5.250 0.3534 0.03318 0.02723 0.0254 0.6377 0.9522
5.500 0.3518 0.03361 0.02769 0.0287 0.6263 0.9536
5.750 0.3869 0.03315 0.02726 0.0277 0.6245 0.9541
6.000 0.4247 0.03255 0.02671 0.0265 0.6232 0.9546
6.250 0.4683 0.03159 0.02581 0.0248 0.6223 0.9547
6.500 0.4726 0.03195 0.02621 0.0271 0.6100 0.9557
6.750 0.5180 0.03067 0.02499 0.0254 0.6087 0.9557
7.000 0.5611 0.02936 0.02377 0.0240 0.6065 0.9557
7.250 0.5768 0.02939 0.02385 0.0249 0.5956 0.9565
7.500 0.6192 0.02820 0.02275 0.0235 0.5942 0.9566
7.750 0.6622 0.02687 0.02154 0.0219 0.5931 0.9568
8.000 0.7071 0.02533 0.02010 0.0203 0.5916 0.9570
8.250 0.7232 0.02554 0.02040 0.0210 0.5793 0.9584
8.500 0.7656 0.02421 0.01919 0.0195 0.5752 0.9588
8.750 0.7944 0.02358 0.01865 0.0193 0.5629 0.9595
9.000 0.8295 0.02257 0.01771 0.0186 0.5473 0.9598
9.250 0.8607 0.02180 0.01692 0.0184 0.5194 0.9604
9.500 0.8962 0.02085 0.01581 0.0181 0.4820 0.9608
9.750 0.9129 0.02119 0.01597 0.0190 0.4393 0.9615
10.000 0.9197 0.02220 0.01671 0.0206 0.3917 0.9625
10.250 0.9213 0.02369 0.01795 0.0223 0.3458 0.9636
10.500 0.9221 0.02539 0.01942 0.0237 0.3047 0.9645
10.750 0.9225 0.02725 0.02105 0.0249 0.2611 0.9654
11.000 0.9235 0.02918 0.02276 0.0258 0.2248 0.9662
11.250 0.9281 0.03102 0.02444 0.0264 0.1937 0.9670
11.500 0.9349 0.03287 0.02615 0.0265 0.1648 0.9677
11.750 0.9417 0.03482 0.02797 0.0266 0.1361 0.9685
12.000 0.9467 0.03700 0.02998 0.0267 0.1070 0.9695
12.250 0.9507 0.03935 0.03217 0.0268 0.0821 0.9707
12.500 0.9565 0.04160 0.03433 0.0268 0.0690 0.9719
12.750 0.9648 0.04367 0.03641 0.0266 0.0602 0.9731
13.000 0.9711 0.04587 0.03856 0.0266 0.0550 0.9741
13.250 0.9836 0.04761 0.04039 0.0263 0.0507 0.9752
13.500 0.9908 0.04965 0.04237 0.0264 0.0468 0.9765
13.750 1.0040 0.05122 0.04406 0.0262 0.0442 0.9780
14.000 1.0168 0.05277 0.04569 0.0261 0.0419 0.9813
14.250 1.0293 0.05423 0.04714 0.0262 0.0401 0.9856
14.500 1.0462 0.05527 0.04817 0.0268 0.0381 0.9936
14.750 1.0634 0.05707 0.05015 0.0259 0.0362 0.9953
15.000 1.0747 0.05900 0.05214 0.0264 0.0345 1.0000
15.250 1.0920 0.06024 0.05346 0.0268 0.0338 1.0000
15.500 1.1131 0.06130 0.05444 0.0272 0.0321 1.0000
15.750 1.1268 0.06327 0.05659 0.0276 0.0314 1.0000
16.000 1.1325 0.06585 0.05942 0.0276 0.0308 1.0000
16.250 1.1395 0.06844 0.06222 0.0277 0.0306 1.0000
16.500 1.1380 0.07180 0.06585 0.0276 0.0299 1.0000
16.750 1.1387 0.07512 0.06940 0.0274 0.0299 1.0000
17.000 1.1337 0.07902 0.07355 0.0269 0.0295 1.0000
17.250 1.1249 0.08347 0.07826 0.0261 0.0291 1.0000
17.500 1.1177 0.08768 0.08268 0.0249 0.0288 1.0000
17.750 1.1033 0.09316 0.08842 0.0234 0.0287 1.0000
18.000 1.0894 0.09872 0.09420 0.0213 0.0285 1.0000
18.250 1.0667 0.10592 0.10168 0.0183 0.0288 1.0000
18.500 1.0423 0.11383 0.10986 0.0144 0.0290 1.0000
18.750 1.0153 0.12279 0.11907 0.0094 0.0291 1.0000
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