WORTMANN FX 05-191 AIRFOIL (fx05191-il) Xfoil prediction polar at RE=50,000 Ncrit=5
| Details | Polar file |
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Airfoil: WORTMANN FX 05-191 AIRFOIL (fx05191-il) Reynolds number: 50,000 Max Cl/Cd: 13.99 at α=13° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx05191-il-50000-n5.txt Download as CSV file: xf-fx05191-il-50000-n5.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 05-191 AIRFOIL
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
------ -------- --------- --------- -------- -------- --------
-13.000 -0.5024 0.12076 0.11384 -0.0617 1.0000 0.0605
-12.750 -0.5188 0.11550 0.10860 -0.0627 1.0000 0.0602
-12.500 -0.5395 0.10975 0.10286 -0.0641 0.9999 0.0598
-12.250 -0.5597 0.10200 0.09503 -0.0688 0.9971 0.0593
-12.000 -0.5859 0.09467 0.08758 -0.0730 0.9939 0.0588
-11.750 -0.6116 0.08865 0.08141 -0.0756 0.9902 0.0584
-11.500 -0.6360 0.08348 0.07605 -0.0773 0.9862 0.0582
-11.250 -0.6580 0.07913 0.07148 -0.0780 0.9820 0.0580
-11.000 -0.6786 0.07555 0.06768 -0.0773 0.9770 0.0578
-10.750 -0.6955 0.07222 0.06410 -0.0767 0.9725 0.0578
-10.500 -0.7139 0.06977 0.06143 -0.0740 0.9667 0.0578
-10.250 -0.7266 0.06721 0.05859 -0.0719 0.9613 0.0580
-10.000 -0.7329 0.06464 0.05572 -0.0700 0.9562 0.0581
-9.750 -0.7361 0.06215 0.05291 -0.0678 0.9509 0.0585
-9.500 -0.7298 0.05958 0.04992 -0.0671 0.9466 0.0593
-9.250 -0.7295 0.05759 0.04754 -0.0645 0.9412 0.0603
-8.750 -0.6919 0.05377 0.04343 -0.0645 0.9336 0.0636
-8.500 -0.6723 0.05219 0.04166 -0.0640 0.9296 0.0654
-8.250 -0.6525 0.05074 0.04000 -0.0631 0.9252 0.0669
-8.000 -0.6194 0.04932 0.03833 -0.0639 0.9220 0.0691
-7.750 -0.5766 0.04814 0.03692 -0.0658 0.9197 0.0728
-7.500 -0.5295 0.04729 0.03612 -0.0683 0.9180 0.0785
-7.250 -0.4888 0.04677 0.03540 -0.0690 0.9149 0.0836
-7.000 -0.4675 0.04615 0.03485 -0.0679 0.9100 0.0880
-6.750 -0.4467 0.04545 0.03410 -0.0674 0.9056 0.0950
-6.500 -0.4353 0.04469 0.03334 -0.0657 0.9006 0.1018
-6.250 -0.4370 0.04404 0.03269 -0.0619 0.8933 0.1076
-6.000 -0.4259 0.04297 0.03166 -0.0607 0.8885 0.1192
-5.750 -0.4318 0.04221 0.03093 -0.0565 0.8806 0.1294
-5.500 -0.4290 0.04088 0.02980 -0.0542 0.8747 0.1524
-5.250 -0.4342 0.03939 0.02869 -0.0506 0.8679 0.1939
-5.000 -0.4466 0.03743 0.02768 -0.0462 0.8604 0.3015
-4.750 -0.4276 0.03827 0.02971 -0.0418 0.8566 0.5288
-4.500 -0.4230 0.03908 0.03051 -0.0370 0.8487 0.5758
-4.250 -0.4033 0.04054 0.03183 -0.0337 0.8432 0.6216
-4.000 -0.3590 0.04509 0.03622 -0.0298 0.8401 0.6694
-3.750 -0.3334 0.04778 0.03878 -0.0256 0.8338 0.6926
-3.500 -0.3180 0.04795 0.03875 -0.0237 0.8278 0.7056
-3.250 -0.2848 0.04802 0.03857 -0.0248 0.8241 0.7125
-3.000 -0.2905 0.04775 0.03821 -0.0203 0.8157 0.7221
-2.750 -0.2674 0.04774 0.03801 -0.0200 0.8105 0.7290
-2.500 -0.2439 0.04737 0.03744 -0.0203 0.8068 0.7376
-2.250 -0.2438 0.04746 0.03746 -0.0163 0.7982 0.7445
-2.000 -0.2285 0.04709 0.03694 -0.0153 0.7930 0.7534
-1.750 -0.1944 0.04709 0.03675 -0.0167 0.7899 0.7588
-1.500 -0.2074 0.04686 0.03648 -0.0114 0.7804 0.7691
-1.250 -0.1792 0.04689 0.03637 -0.0118 0.7763 0.7742
-1.000 -0.1727 0.04663 0.03600 -0.0096 0.7702 0.7840
-0.750 -0.1575 0.04675 0.03603 -0.0080 0.7638 0.7894
-0.500 -0.1344 0.04660 0.03576 -0.0080 0.7598 0.7970
-0.250 -0.1254 0.04663 0.03571 -0.0059 0.7534 0.8043
0.000 -0.1111 0.04663 0.03564 -0.0045 0.7475 0.8116
0.250 -0.0867 0.04649 0.03538 -0.0047 0.7437 0.8188
0.750 -0.0639 0.04663 0.03541 -0.0012 0.7315 0.8336
1.000 -0.0355 0.04663 0.03532 -0.0017 0.7281 0.8395
1.250 -0.0338 0.04682 0.03548 0.0011 0.7208 0.8481
1.500 -0.0122 0.04695 0.03555 0.0014 0.7160 0.8541
1.750 0.0126 0.04685 0.03537 0.0012 0.7126 0.8619
2.000 0.0179 0.04728 0.03580 0.0037 0.7052 0.8683
2.250 0.0365 0.04737 0.03585 0.0043 0.7005 0.8759
2.500 0.0651 0.04739 0.03583 0.0037 0.6974 0.8818
2.750 0.0680 0.04789 0.03633 0.0061 0.6897 0.8896
3.000 0.0886 0.04805 0.03647 0.0064 0.6851 0.8963
3.250 0.1180 0.04813 0.03652 0.0056 0.6821 0.9024
3.500 0.1199 0.04875 0.03715 0.0080 0.6744 0.9104
3.750 0.1437 0.04902 0.03742 0.0077 0.6697 0.9166
4.000 0.1718 0.04910 0.03750 0.0070 0.6666 0.9233
4.250 0.1795 0.04995 0.03838 0.0081 0.6589 0.9301
4.500 0.2026 0.05030 0.03876 0.0078 0.6540 0.9367
4.750 0.2380 0.05053 0.03901 0.0057 0.6508 0.9419
5.000 0.2457 0.05155 0.04009 0.0066 0.6429 0.9489
5.250 0.2761 0.05212 0.04071 0.0047 0.6378 0.9540
5.500 0.3121 0.05239 0.04103 0.0025 0.6345 0.9594
6.000 0.3556 0.05430 0.04311 0.0000 0.6209 0.9706
6.250 0.3949 0.05459 0.04349 -0.0027 0.6176 0.9755
6.500 0.4037 0.05620 0.04520 -0.0031 0.6078 0.9818
6.750 0.4389 0.05669 0.04579 -0.0055 0.6031 0.9870
7.000 0.4591 0.05777 0.04697 -0.0068 0.5958 0.9935
7.250 0.4743 0.05849 0.04780 -0.0066 0.5886 1.0000
7.500 0.4960 0.05840 0.04777 -0.0060 0.5847 1.0000
7.750 0.4870 0.05981 0.04924 -0.0032 0.5741 1.0000
8.000 0.5122 0.06001 0.04952 -0.0034 0.5694 1.0000
8.500 0.5416 0.06175 0.05147 -0.0030 0.5538 1.0000
8.750 0.5505 0.06312 0.05295 -0.0026 0.5440 1.0000
9.000 0.5782 0.06345 0.05341 -0.0034 0.5376 1.0000
9.250 0.5885 0.06485 0.05492 -0.0033 0.5269 1.0000
9.500 0.6203 0.06487 0.05511 -0.0042 0.5206 1.0000
9.750 0.6297 0.06635 0.05672 -0.0040 0.5086 1.0000
10.000 0.6683 0.06573 0.05629 -0.0051 0.5031 1.0000
10.250 0.6760 0.06732 0.05803 -0.0049 0.4897 1.0000
10.500 0.6913 0.06825 0.05912 -0.0049 0.4771 1.0000
11.000 0.7524 0.06608 0.05731 -0.0045 0.4510 1.0000
11.500 0.7889 0.06565 0.05722 -0.0033 0.4143 1.0000
11.750 0.8075 0.06577 0.05752 -0.0031 0.3976 1.0000
12.000 0.8259 0.06599 0.05795 -0.0028 0.3797 1.0000
12.250 0.8497 0.06544 0.05758 -0.0024 0.3592 1.0000
12.500 0.8645 0.06617 0.05844 -0.0022 0.3322 1.0000
12.750 0.8921 0.06509 0.05732 -0.0015 0.2966 1.0000
13.000 0.9111 0.06511 0.05708 -0.0007 0.2524 1.0000
13.250 0.9185 0.06676 0.05832 -0.0001 0.2158 1.0000
13.500 0.9206 0.06943 0.06076 0.0000 0.1892 1.0000
13.750 0.9237 0.07212 0.06323 -0.0001 0.1703 1.0000
14.000 0.9284 0.07476 0.06575 -0.0003 0.1548 1.0000
14.250 0.9356 0.07724 0.06820 -0.0007 0.1419 1.0000
14.500 0.9440 0.07962 0.07060 -0.0011 0.1310 1.0000
14.750 0.9538 0.08183 0.07278 -0.0014 0.1220 1.0000
15.000 0.9642 0.08401 0.07498 -0.0019 0.1137 1.0000
15.250 0.9766 0.08606 0.07713 -0.0022 0.1065 1.0000
15.500 0.9898 0.08790 0.07897 -0.0026 0.1001 1.0000
15.750 1.0041 0.08985 0.08108 -0.0029 0.0944 1.0000
16.000 1.0180 0.09184 0.08321 -0.0033 0.0892 1.0000
16.250 1.0378 0.09306 0.08440 -0.0034 0.0844 1.0000
16.500 1.0441 0.09634 0.08803 -0.0043 0.0807 1.0000
16.750 1.0530 0.09918 0.09107 -0.0051 0.0773 1.0000
17.000 1.0747 0.10026 0.09210 -0.0053 0.0735 1.0000
17.250 1.0688 0.10513 0.09729 -0.0070 0.0715 1.0000
17.500 1.0583 0.11077 0.10330 -0.0093 0.0699 1.0000
17.750 1.0458 0.11691 0.10975 -0.0121 0.0686 1.0000
18.000 1.0291 0.12398 0.11711 -0.0157 0.0677 1.0000
18.250 1.0042 0.13292 0.12631 -0.0208 0.0672 1.0000
18.500 0.9618 0.14643 0.14009 -0.0290 0.0676 1.0000
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