FX 84-W-150 (fx84w150-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: FX 84-W-150 (fx84w150-il) Reynolds number: 500,000 Max Cl/Cd: 116.02 at α=6.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx84w150-il-500000.txt Download as CSV file: xf-fx84w150-il-500000.csv |
XFOIL Version 6.96
Calculated polar for: FX 84-W-150
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.500 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-13.000 -0.5402 0.05156 0.04872 -0.1090 0.9470 0.0209
-12.750 -0.5741 0.04355 0.04038 -0.1157 0.9247 0.0207
-12.500 -0.6011 0.03903 0.03557 -0.1170 0.9083 0.0206
-12.250 -0.6212 0.03593 0.03221 -0.1162 0.8955 0.0207
-12.000 -0.6381 0.03337 0.02939 -0.1140 0.8842 0.0208
-11.750 -0.6496 0.03152 0.02731 -0.1109 0.8746 0.0210
-11.500 -0.6526 0.03004 0.02554 -0.1081 0.8670 0.0213
-11.250 -0.6485 0.02851 0.02374 -0.1062 0.8601 0.0216
-11.000 -0.6422 0.02645 0.02152 -0.1047 0.8538 0.0222
-10.500 -0.6075 0.02495 0.01988 -0.1029 0.8431 0.0232
-10.250 -0.5897 0.02406 0.01885 -0.1020 0.8377 0.0238
-10.000 -0.5721 0.02301 0.01759 -0.1011 0.8330 0.0245
-9.750 -0.5525 0.02202 0.01642 -0.1003 0.8279 0.0251
-9.500 -0.5314 0.02125 0.01544 -0.0996 0.8228 0.0257
-9.250 -0.5128 0.01976 0.01382 -0.0989 0.8183 0.0266
-9.000 -0.4898 0.01919 0.01321 -0.0985 0.8139 0.0274
-8.750 -0.4657 0.01873 0.01269 -0.0982 0.8089 0.0284
-8.500 -0.4416 0.01818 0.01203 -0.0978 0.8044 0.0296
-8.250 -0.4169 0.01775 0.01141 -0.0973 0.8003 0.0305
-8.000 -0.3947 0.01664 0.01027 -0.0969 0.7957 0.0318
-7.750 -0.3696 0.01619 0.00981 -0.0967 0.7910 0.0331
-7.500 -0.3442 0.01578 0.00931 -0.0964 0.7868 0.0346
-7.250 -0.3179 0.01551 0.00890 -0.0962 0.7830 0.0360
-7.000 -0.2941 0.01471 0.00812 -0.0958 0.7783 0.0380
-6.750 -0.2679 0.01438 0.00776 -0.0957 0.7736 0.0399
-6.500 -0.2414 0.01406 0.00735 -0.0955 0.7696 0.0418
-6.250 -0.2163 0.01352 0.00675 -0.0952 0.7656 0.0440
-6.000 -0.1898 0.01320 0.00645 -0.0952 0.7611 0.0466
-5.750 -0.1627 0.01296 0.00615 -0.0951 0.7565 0.0493
-5.500 -0.1370 0.01250 0.00563 -0.0949 0.7524 0.0523
-5.250 -0.1101 0.01225 0.00538 -0.0948 0.7482 0.0558
-5.000 -0.0824 0.01208 0.00516 -0.0949 0.7434 0.0590
-4.750 -0.0564 0.01164 0.00474 -0.0947 0.7389 0.0643
-4.500 -0.0287 0.01150 0.00452 -0.0947 0.7349 0.0691
-4.250 -0.0020 0.01116 0.00423 -0.0946 0.7304 0.0765
-4.000 0.0253 0.01091 0.00399 -0.0947 0.7258 0.0848
-3.750 0.0529 0.01072 0.00378 -0.0947 0.7216 0.0949
-3.500 0.0804 0.01052 0.00359 -0.0947 0.7176 0.1086
-3.250 0.1077 0.01027 0.00343 -0.0948 0.7129 0.1275
-3.000 0.1352 0.01005 0.00329 -0.0949 0.7085 0.1520
-2.750 0.1626 0.00983 0.00314 -0.0950 0.7045 0.1845
-2.500 0.1898 0.00958 0.00304 -0.0951 0.7002 0.2295
-2.250 0.2166 0.00924 0.00294 -0.0952 0.6955 0.2948
-2.000 0.2428 0.00880 0.00283 -0.0952 0.6912 0.3956
-1.750 0.2685 0.00835 0.00276 -0.0951 0.6872 0.5237
-1.500 0.2944 0.00807 0.00280 -0.0949 0.6826 0.6213
-1.250 0.3212 0.00794 0.00283 -0.0946 0.6779 0.6811
-1.000 0.3485 0.00790 0.00285 -0.0944 0.6737 0.7211
-0.750 0.3761 0.00792 0.00289 -0.0942 0.6695 0.7503
-0.500 0.4033 0.00792 0.00294 -0.0940 0.6646 0.7736
-0.250 0.4308 0.00794 0.00296 -0.0938 0.6598 0.7931
0.000 0.4583 0.00800 0.00298 -0.0936 0.6555 0.8099
0.250 0.4852 0.00803 0.00304 -0.0934 0.6505 0.8246
0.500 0.5120 0.00806 0.00309 -0.0931 0.6456 0.8387
0.750 0.5388 0.00812 0.00312 -0.0927 0.6412 0.8521
1.000 0.5656 0.00819 0.00318 -0.0925 0.6368 0.8651
1.250 0.5908 0.00823 0.00325 -0.0918 0.6318 0.8793
1.500 0.6144 0.00828 0.00332 -0.0907 0.6270 0.8957
1.750 0.6378 0.00837 0.00337 -0.0895 0.6227 0.9093
2.000 0.6617 0.00838 0.00343 -0.0886 0.6180 0.9192
2.250 0.6863 0.00841 0.00347 -0.0879 0.6131 0.9296
2.500 0.7105 0.00846 0.00348 -0.0871 0.6085 0.9393
2.750 0.7351 0.00849 0.00353 -0.0864 0.6036 0.9491
3.000 0.7611 0.00851 0.00357 -0.0861 0.5984 0.9595
3.250 0.7911 0.00857 0.00359 -0.0866 0.5933 0.9686
3.500 0.8254 0.00864 0.00367 -0.0881 0.5879 0.9757
3.750 0.8602 0.00870 0.00374 -0.0898 0.5820 0.9832
4.000 0.8987 0.00881 0.00380 -0.0923 0.5766 0.9877
4.250 0.9360 0.00890 0.00392 -0.0946 0.5707 0.9933
4.500 0.9743 0.00899 0.00401 -0.0971 0.5649 0.9988
4.750 0.9960 0.00913 0.00410 -0.0963 0.5597 1.0000
5.000 1.0160 0.00920 0.00422 -0.0951 0.5533 1.0000
5.250 1.0402 0.00933 0.00432 -0.0947 0.5466 1.0000
5.500 1.0653 0.00947 0.00447 -0.0944 0.5399 1.0000
5.750 1.0907 0.00960 0.00461 -0.0942 0.5330 1.0000
6.000 1.1164 0.00979 0.00477 -0.0941 0.5271 1.0000
6.250 1.1414 0.00992 0.00495 -0.0939 0.5199 1.0000
6.500 1.1664 0.01012 0.00511 -0.0936 0.5133 1.0000
6.750 1.1904 0.01026 0.00532 -0.0931 0.5049 1.0000
7.000 1.2118 0.01045 0.00549 -0.0922 0.4921 1.0000
7.250 1.2320 0.01068 0.00568 -0.0910 0.4779 1.0000
7.500 1.2517 0.01094 0.00592 -0.0898 0.4654 1.0000
7.750 1.2710 0.01120 0.00618 -0.0886 0.4525 1.0000
8.000 1.2896 0.01149 0.00646 -0.0872 0.4401 1.0000
8.250 1.3048 0.01180 0.00677 -0.0852 0.4279 1.0000
8.500 1.3179 0.01219 0.00714 -0.0829 0.4153 1.0000
8.750 1.3298 0.01264 0.00756 -0.0805 0.4009 1.0000
9.000 1.3410 0.01317 0.00806 -0.0780 0.3851 1.0000
9.250 1.3504 0.01380 0.00866 -0.0755 0.3667 1.0000
9.500 1.3574 0.01460 0.00939 -0.0728 0.3467 1.0000
9.750 1.3625 0.01555 0.01026 -0.0700 0.3258 1.0000
10.000 1.3663 0.01664 0.01126 -0.0672 0.3005 1.0000
10.250 1.3668 0.01800 0.01249 -0.0641 0.2741 1.0000
10.500 1.3657 0.01954 0.01390 -0.0612 0.2471 1.0000
10.750 1.3635 0.02126 0.01547 -0.0583 0.2192 1.0000
11.000 1.3608 0.02312 0.01720 -0.0557 0.1932 1.0000
11.250 1.3587 0.02504 0.01899 -0.0532 0.1676 1.0000
11.500 1.3551 0.02716 0.02098 -0.0509 0.1420 1.0000
11.750 1.3503 0.02945 0.02314 -0.0487 0.1176 1.0000
12.000 1.3463 0.03182 0.02539 -0.0467 0.0972 1.0000
12.250 1.3452 0.03406 0.02756 -0.0452 0.0822 1.0000
12.500 1.3452 0.03632 0.02977 -0.0438 0.0703 1.0000
12.750 1.3457 0.03861 0.03203 -0.0426 0.0614 1.0000
13.000 1.3481 0.04082 0.03424 -0.0417 0.0549 1.0000
13.250 1.3511 0.04302 0.03647 -0.0408 0.0498 1.0000
13.500 1.3525 0.04546 0.03891 -0.0401 0.0460 1.0000
13.750 1.3554 0.04783 0.04134 -0.0395 0.0429 1.0000
14.000 1.3595 0.05011 0.04367 -0.0390 0.0404 1.0000
14.250 1.3588 0.05296 0.04654 -0.0385 0.0381 1.0000
14.500 1.3621 0.05546 0.04912 -0.0382 0.0362 1.0000
14.750 1.3669 0.05785 0.05158 -0.0380 0.0345 1.0000
15.000 1.3690 0.06058 0.05436 -0.0379 0.0331 1.0000
15.250 1.3662 0.06395 0.05778 -0.0379 0.0317 1.0000
15.500 1.3669 0.06698 0.06089 -0.0379 0.0306 1.0000
15.750 1.3710 0.06963 0.06362 -0.0381 0.0296 1.0000
16.000 1.3742 0.07245 0.06652 -0.0383 0.0285 1.0000
16.250 1.3757 0.07550 0.06964 -0.0387 0.0277 1.0000
16.500 1.3744 0.07897 0.07314 -0.0391 0.0267 1.0000
16.750 1.3699 0.08292 0.07715 -0.0397 0.0258 1.0000
17.000 1.3738 0.08582 0.08016 -0.0402 0.0251 1.0000
17.250 1.3765 0.08891 0.08334 -0.0409 0.0244 1.0000
17.500 1.3779 0.09220 0.08671 -0.0416 0.0237 1.0000
17.750 1.3798 0.09547 0.09004 -0.0424 0.0230 1.0000
18.000 1.3796 0.09905 0.09368 -0.0434 0.0225 1.0000
18.250 1.3781 0.10276 0.09742 -0.0444 0.0219 1.0000
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