WORTMANN FX 082-512 AIRFOIL (fx082512-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: WORTMANN FX 082-512 AIRFOIL (fx082512-il) Reynolds number: 1,000,000 Max Cl/Cd: 99.08 at α=-0.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx082512-il-1000000.txt Download as CSV file: xf-fx082512-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 082-512 AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 1.000 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-17.500 -0.7967 0.13053 0.12834 -0.0362 1.0000 0.0098
-17.250 -0.8234 0.12090 0.11858 -0.0408 1.0000 0.0098
-17.000 -0.8398 0.11379 0.11137 -0.0442 1.0000 0.0098
-16.750 -0.8560 0.10702 0.10450 -0.0475 1.0000 0.0099
-16.500 -0.8682 0.10122 0.09861 -0.0502 1.0000 0.0099
-16.250 -0.8789 0.09593 0.09324 -0.0526 1.0000 0.0099
-15.750 -0.9045 0.08532 0.08244 -0.0574 1.0000 0.0101
-15.500 -0.9157 0.08065 0.07769 -0.0592 1.0000 0.0102
-15.250 -0.9249 0.07643 0.07339 -0.0608 1.0000 0.0103
-15.000 -0.9352 0.07231 0.06921 -0.0622 1.0000 0.0105
-14.750 -0.9430 0.06869 0.06554 -0.0632 1.0000 0.0107
-14.500 -0.9469 0.06572 0.06254 -0.0638 1.0000 0.0109
-14.250 -0.9538 0.06267 0.05943 -0.0641 1.0000 0.0109
-14.000 -0.9585 0.06006 0.05679 -0.0641 1.0000 0.0112
-13.750 -0.9675 0.05725 0.05393 -0.0639 1.0000 0.0112
-13.500 -0.9611 0.05451 0.05114 -0.0663 0.9992 0.0115
-13.250 -0.9522 0.05123 0.04777 -0.0704 0.9975 0.0117
-13.000 -0.9405 0.04848 0.04496 -0.0742 0.9958 0.0120
-12.750 -0.9315 0.04571 0.04212 -0.0776 0.9936 0.0122
-12.500 -0.9250 0.04306 0.03940 -0.0805 0.9901 0.0125
-12.250 -0.9135 0.04049 0.03675 -0.0844 0.9875 0.0127
-12.000 -0.8975 0.03805 0.03424 -0.0881 0.9846 0.0129
-11.750 -0.8846 0.03332 0.02941 -0.0961 0.9796 0.0134
-11.500 -0.8554 0.02908 0.02507 -0.1061 0.9780 0.0141
-11.250 -0.8209 0.02592 0.02182 -0.1145 0.9773 0.0148
-11.000 -0.7960 0.02315 0.01896 -0.1196 0.9738 0.0154
-10.750 -0.7614 0.02058 0.01627 -0.1260 0.9723 0.0162
-10.500 -0.7245 0.01836 0.01390 -0.1321 0.9713 0.0175
-10.250 -0.6893 0.01704 0.01251 -0.1360 0.9705 0.0189
-10.000 -0.6549 0.01616 0.01155 -0.1389 0.9698 0.0202
-9.750 -0.6192 0.01512 0.01045 -0.1423 0.9693 0.0228
-9.500 -0.5845 0.01440 0.00969 -0.1448 0.9687 0.0256
-9.250 -0.5497 0.01370 0.00900 -0.1474 0.9683 0.0315
-9.000 -0.5157 0.01331 0.00866 -0.1493 0.9678 0.0382
-8.750 -0.4820 0.01302 0.00841 -0.1510 0.9674 0.0429
-8.500 -0.4488 0.01292 0.00830 -0.1522 0.9669 0.0462
-8.250 -0.4255 0.01289 0.00826 -0.1514 0.9637 0.0476
-8.000 -0.3947 0.01241 0.00775 -0.1526 0.9619 0.0508
-7.750 -0.3636 0.01223 0.00760 -0.1536 0.9605 0.0532
-7.500 -0.3312 0.01204 0.00738 -0.1547 0.9594 0.0551
-7.250 -0.2986 0.01188 0.00720 -0.1559 0.9585 0.0569
-7.000 -0.2655 0.01174 0.00705 -0.1571 0.9578 0.0580
-6.750 -0.2304 0.01128 0.00652 -0.1591 0.9572 0.0598
-6.500 -0.1947 0.01075 0.00595 -0.1614 0.9568 0.0630
-6.250 -0.1602 0.01048 0.00569 -0.1630 0.9563 0.0657
-6.000 -0.1254 0.01020 0.00538 -0.1647 0.9558 0.0677
-5.750 -0.0903 0.00990 0.00504 -0.1665 0.9554 0.0691
-5.500 -0.0628 0.00969 0.00480 -0.1665 0.9525 0.0700
-5.250 -0.0332 0.00948 0.00456 -0.1670 0.9501 0.0707
-5.000 -0.0004 0.00920 0.00425 -0.1682 0.9488 0.0718
-4.750 0.0339 0.00882 0.00381 -0.1698 0.9478 0.0755
-4.500 0.0681 0.00852 0.00349 -0.1712 0.9469 0.0787
-4.250 0.1027 0.00825 0.00322 -0.1728 0.9460 0.0814
-4.000 0.1377 0.00802 0.00297 -0.1743 0.9452 0.0840
-3.750 0.1748 0.00772 0.00267 -0.1763 0.9441 0.0893
-3.500 0.2188 0.00648 0.00196 -0.1809 0.9432 0.2580
-3.250 0.2576 0.00632 0.00187 -0.1833 0.9421 0.2861
-3.000 0.2835 0.00631 0.00189 -0.1827 0.9371 0.2947
-2.750 0.3193 0.00622 0.00178 -0.1843 0.9332 0.3003
-2.500 0.3607 0.00612 0.00170 -0.1871 0.9306 0.3058
-2.250 0.4066 0.00607 0.00164 -0.1910 0.9276 0.3100
-2.000 0.4306 0.00610 0.00166 -0.1899 0.9196 0.3127
-1.750 0.4754 0.00604 0.00160 -0.1936 0.9147 0.3163
-1.500 0.5040 0.00604 0.00161 -0.1936 0.9052 0.3194
-1.250 0.5395 0.00605 0.00160 -0.1951 0.8949 0.3220
-1.000 0.5693 0.00607 0.00158 -0.1953 0.8798 0.3240
-0.750 0.5967 0.00613 0.00155 -0.1949 0.8539 0.3258
-0.500 0.6212 0.00627 0.00154 -0.1939 0.8176 0.3273
-0.250 0.6403 0.00657 0.00159 -0.1917 0.7647 0.3284
0.000 0.6559 0.00696 0.00168 -0.1888 0.6997 0.3305
0.250 0.6682 0.00761 0.00190 -0.1853 0.6011 0.3331
0.500 0.6775 0.00889 0.00237 -0.1816 0.4173 0.3353
0.750 0.6900 0.01026 0.00289 -0.1787 0.2256 0.3372
1.000 0.7082 0.01119 0.00332 -0.1769 0.0914 0.3389
1.250 0.7342 0.01137 0.00347 -0.1764 0.0853 0.3403
1.500 0.7600 0.01157 0.00366 -0.1759 0.0797 0.3416
1.750 0.7862 0.01173 0.00382 -0.1754 0.0779 0.3427
2.000 0.8124 0.01188 0.00398 -0.1750 0.0767 0.3437
2.250 0.8385 0.01202 0.00415 -0.1745 0.0752 0.3451
2.500 0.8648 0.01216 0.00433 -0.1742 0.0735 0.3476
2.750 0.8905 0.01234 0.00454 -0.1736 0.0714 0.3496
3.000 0.9157 0.01258 0.00479 -0.1730 0.0686 0.3513
3.250 0.9394 0.01297 0.00521 -0.1721 0.0647 0.3530
3.500 0.9656 0.01306 0.00532 -0.1717 0.0639 0.3547
3.750 0.9914 0.01321 0.00549 -0.1712 0.0626 0.3564
4.000 1.0169 0.01337 0.00566 -0.1706 0.0607 0.3580
4.250 1.0423 0.01354 0.00583 -0.1700 0.0586 0.3593
4.500 1.0674 0.01373 0.00602 -0.1694 0.0563 0.3612
4.750 1.0906 0.01412 0.00646 -0.1684 0.0528 0.3637
5.000 1.1173 0.01414 0.00650 -0.1681 0.0516 0.3660
5.250 1.1431 0.01422 0.00661 -0.1677 0.0492 0.3683
5.500 1.1682 0.01436 0.00671 -0.1670 0.0458 0.3707
5.750 1.1922 0.01456 0.00692 -0.1662 0.0418 0.3731
6.000 1.2158 0.01477 0.00706 -0.1653 0.0356 0.3750
6.250 1.2384 0.01507 0.00733 -0.1642 0.0297 0.3776
6.500 1.2602 0.01544 0.00772 -0.1630 0.0258 0.3806
6.750 1.2806 0.01595 0.00823 -0.1614 0.0225 0.3833
7.000 1.3022 0.01631 0.00865 -0.1601 0.0212 0.3862
7.250 1.3228 0.01675 0.00911 -0.1587 0.0197 0.3889
7.500 1.3407 0.01744 0.00982 -0.1567 0.0179 0.3911
7.750 1.3620 0.01780 0.01026 -0.1554 0.0173 0.3952
8.000 1.3821 0.01826 0.01079 -0.1539 0.0165 0.3991
8.250 1.4017 0.01876 0.01134 -0.1523 0.0157 0.4030
8.500 1.4199 0.01938 0.01200 -0.1505 0.0150 0.4067
8.750 1.4341 0.02041 0.01312 -0.1480 0.0141 0.4121
9.000 1.4535 0.02090 0.01369 -0.1465 0.0138 0.4182
9.250 1.4719 0.02148 0.01436 -0.1448 0.0134 0.4248
9.500 1.4901 0.02209 0.01506 -0.1431 0.0130 0.4335
9.750 1.5082 0.02272 0.01576 -0.1414 0.0125 0.4448
10.000 1.5259 0.02337 0.01651 -0.1398 0.0120 0.4625
10.250 1.5424 0.02416 0.01741 -0.1380 0.0116 0.4952
10.500 1.5543 0.02557 0.01906 -0.1357 0.0111 0.5636
10.750 1.5727 0.02656 0.02044 -0.1345 0.0108 0.7153
11.000 1.5827 0.02694 0.02129 -0.1314 0.0107 1.0000
11.250 1.5974 0.02783 0.02226 -0.1294 0.0104 1.0000
11.500 1.6106 0.02886 0.02337 -0.1273 0.0102 1.0000
11.750 1.6234 0.02993 0.02452 -0.1252 0.0100 1.0000
12.000 1.6357 0.03103 0.02570 -0.1231 0.0097 1.0000
12.250 1.6464 0.03227 0.02702 -0.1208 0.0095 1.0000
12.500 1.6571 0.03351 0.02834 -0.1187 0.0093 1.0000
12.750 1.6667 0.03484 0.02975 -0.1165 0.0091 1.0000
13.000 1.6752 0.03629 0.03127 -0.1143 0.0089 1.0000
13.250 1.6805 0.03811 0.03318 -0.1119 0.0087 1.0000
13.500 1.6821 0.04037 0.03557 -0.1093 0.0086 1.0000
13.750 1.6727 0.04402 0.03944 -0.1061 0.0083 1.0000
14.000 1.6696 0.04700 0.04260 -0.1037 0.0082 1.0000
14.250 1.6721 0.04928 0.04500 -0.1019 0.0082 1.0000
14.500 1.6726 0.05187 0.04772 -0.1002 0.0081 1.0000
14.750 1.6746 0.05431 0.05028 -0.0988 0.0080 1.0000
15.000 1.6720 0.05746 0.05360 -0.0975 0.0080 1.0000
15.250 1.6666 0.06112 0.05741 -0.0966 0.0079 1.0000
15.500 1.6669 0.06408 0.06048 -0.0960 0.0078 1.0000
15.750 1.6597 0.06829 0.06484 -0.0957 0.0077 1.0000
16.000 1.6552 0.07226 0.06895 -0.0958 0.0076 1.0000
16.250 1.6429 0.07772 0.07457 -0.0966 0.0075 1.0000
16.500 1.6306 0.08345 0.08047 -0.0980 0.0075 1.0000
16.750 1.6181 0.08954 0.08672 -0.1000 0.0074 1.0000
17.000 1.5985 0.09739 0.09476 -0.1033 0.0074 1.0000
17.250 1.5794 0.10562 0.10318 -0.1074 0.0074 1.0000
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