WORTMANN FX 082-512 AIRFOIL (fx082512-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: WORTMANN FX 082-512 AIRFOIL (fx082512-il) Reynolds number: 500,000 Max Cl/Cd: 83.67 at α=0.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx082512-il-500000.txt Download as CSV file: xf-fx082512-il-500000.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 = 0.500 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-15.500 -0.7323 0.11199 0.10929 -0.0456 1.0000 0.0162
-15.250 -0.7707 0.10032 0.09746 -0.0516 1.0000 0.0160
-15.000 -0.7945 0.09228 0.08927 -0.0558 1.0000 0.0160
-14.750 -0.8134 0.08562 0.08248 -0.0590 1.0000 0.0160
-14.500 -0.8277 0.08011 0.07685 -0.0615 1.0000 0.0161
-14.250 -0.8382 0.07550 0.07213 -0.0634 1.0000 0.0162
-14.000 -0.8506 0.07085 0.06736 -0.0652 1.0000 0.0163
-13.750 -0.8593 0.06702 0.06342 -0.0665 1.0000 0.0164
-13.500 -0.8672 0.06363 0.05993 -0.0672 1.0000 0.0164
-13.250 -0.8823 0.05987 0.05607 -0.0674 1.0000 0.0166
-13.000 -0.8942 0.05692 0.05304 -0.0668 1.0000 0.0169
-12.750 -0.9034 0.05449 0.05057 -0.0660 1.0000 0.0170
-12.500 -0.9144 0.05218 0.04822 -0.0649 1.0000 0.0172
-12.250 -0.9261 0.05004 0.04604 -0.0634 1.0000 0.0174
-12.000 -0.9400 0.04800 0.04399 -0.0615 1.0000 0.0176
-11.750 -0.9595 0.04618 0.04213 -0.0584 1.0000 0.0176
-11.500 -0.9501 0.04352 0.03941 -0.0621 0.9968 0.0181
-11.250 -0.9301 0.04078 0.03659 -0.0674 0.9939 0.0188
-11.000 -0.9098 0.03807 0.03378 -0.0723 0.9903 0.0195
-10.750 -0.8833 0.03544 0.03100 -0.0780 0.9879 0.0203
-10.500 -0.8513 0.03235 0.02780 -0.0857 0.9863 0.0215
-10.250 -0.8259 0.02938 0.02478 -0.0914 0.9825 0.0225
-10.000 -0.7910 0.02687 0.02217 -0.0980 0.9808 0.0239
-9.750 -0.7532 0.02465 0.01979 -0.1044 0.9797 0.0255
-9.500 -0.7120 0.02211 0.01717 -0.1119 0.9791 0.0285
-9.250 -0.6752 0.02115 0.01611 -0.1156 0.9782 0.0314
-9.000 -0.6373 0.02008 0.01504 -0.1197 0.9776 0.0358
-8.750 -0.6006 0.01944 0.01433 -0.1228 0.9770 0.0406
-8.500 -0.5757 0.01922 0.01413 -0.1227 0.9737 0.0445
-8.250 -0.5445 0.01906 0.01388 -0.1239 0.9716 0.0483
-8.000 -0.5102 0.01856 0.01338 -0.1262 0.9703 0.0524
-7.750 -0.4759 0.01838 0.01313 -0.1280 0.9690 0.0559
-7.500 -0.4409 0.01836 0.01302 -0.1298 0.9680 0.0582
-7.250 -0.4035 0.01733 0.01196 -0.1332 0.9674 0.0624
-7.000 -0.3671 0.01694 0.01154 -0.1356 0.9668 0.0655
-6.750 -0.3411 0.01661 0.01116 -0.1357 0.9633 0.0681
-6.500 -0.3096 0.01634 0.01083 -0.1369 0.9610 0.0702
-6.250 -0.2738 0.01569 0.01010 -0.1393 0.9598 0.0734
-6.000 -0.2368 0.01503 0.00942 -0.1420 0.9587 0.0769
-5.750 -0.2004 0.01459 0.00892 -0.1443 0.9577 0.0796
-5.500 -0.1634 0.01419 0.00846 -0.1466 0.9569 0.0819
-5.250 -0.1264 0.01382 0.00803 -0.1489 0.9561 0.0837
-5.000 -0.0894 0.01352 0.00766 -0.1510 0.9554 0.0852
-4.750 -0.0603 0.01311 0.00720 -0.1517 0.9521 0.0889
-4.500 -0.0280 0.01275 0.00680 -0.1529 0.9495 0.0930
-4.250 0.0069 0.01243 0.00644 -0.1546 0.9478 0.0974
-4.000 0.0425 0.01212 0.00610 -0.1564 0.9464 0.1059
-3.750 0.0833 0.01105 0.00561 -0.1604 0.9461 0.2751
-3.500 0.1184 0.01108 0.00563 -0.1617 0.9448 0.2966
-3.250 0.1542 0.01110 0.00568 -0.1632 0.9437 0.3071
-3.000 0.1907 0.01111 0.00562 -0.1649 0.9428 0.3142
-2.750 0.2178 0.01109 0.00565 -0.1645 0.9378 0.3188
-2.500 0.2534 0.01093 0.00548 -0.1658 0.9343 0.3235
-2.250 0.2908 0.01075 0.00527 -0.1676 0.9325 0.3274
-2.000 0.3281 0.01050 0.00505 -0.1694 0.9313 0.3311
-1.750 0.3676 0.01028 0.00488 -0.1715 0.9300 0.3356
-1.500 0.4141 0.00984 0.00445 -0.1751 0.9285 0.3390
-1.250 0.4393 0.00976 0.00438 -0.1742 0.9215 0.3412
-1.000 0.4777 0.00955 0.00415 -0.1762 0.9182 0.3434
-0.750 0.5226 0.00918 0.00380 -0.1797 0.9152 0.3459
-0.500 0.5562 0.00899 0.00366 -0.1806 0.9073 0.3484
-0.250 0.6042 0.00883 0.00355 -0.1846 0.8985 0.3533
0.000 0.6358 0.00874 0.00343 -0.1849 0.8799 0.3568
0.250 0.6681 0.00864 0.00326 -0.1855 0.8546 0.3586
0.500 0.7013 0.00864 0.00313 -0.1863 0.8214 0.3598
0.750 0.7288 0.00871 0.00300 -0.1859 0.7688 0.3616
1.000 0.7442 0.00918 0.00306 -0.1828 0.6846 0.3630
1.250 0.7465 0.01019 0.00337 -0.1772 0.5437 0.3641
1.500 0.7485 0.01191 0.00403 -0.1722 0.3223 0.3652
1.750 0.7585 0.01355 0.00471 -0.1691 0.1103 0.3665
2.000 0.7831 0.01383 0.00496 -0.1684 0.0992 0.3682
2.250 0.8077 0.01412 0.00525 -0.1676 0.0930 0.3701
2.500 0.8331 0.01433 0.00549 -0.1670 0.0909 0.3722
2.750 0.8579 0.01458 0.00577 -0.1663 0.0885 0.3741
3.000 0.8823 0.01488 0.00608 -0.1655 0.0858 0.3756
3.250 0.9063 0.01516 0.00641 -0.1647 0.0827 0.3778
3.500 0.9280 0.01567 0.00697 -0.1635 0.0792 0.3797
3.750 0.9523 0.01593 0.00728 -0.1627 0.0769 0.3817
4.000 0.9767 0.01616 0.00756 -0.1619 0.0742 0.3839
4.250 1.0003 0.01646 0.00790 -0.1610 0.0713 0.3861
4.500 1.0227 0.01684 0.00829 -0.1599 0.0683 0.3883
4.750 1.0406 0.01770 0.00918 -0.1580 0.0647 0.3902
5.000 1.0662 0.01770 0.00925 -0.1575 0.0626 0.3928
5.250 1.0907 0.01782 0.00944 -0.1568 0.0594 0.3958
5.500 1.1145 0.01800 0.00964 -0.1560 0.0561 0.3987
5.750 1.1350 0.01851 0.01018 -0.1546 0.0521 0.4016
6.000 1.1614 0.01843 0.01014 -0.1542 0.0480 0.4047
6.250 1.1840 0.01872 0.01038 -0.1532 0.0430 0.4074
6.500 1.2094 0.01878 0.01052 -0.1526 0.0388 0.4110
6.750 1.2303 0.01925 0.01096 -0.1513 0.0345 0.4145
7.000 1.2522 0.01960 0.01137 -0.1501 0.0315 0.4183
7.250 1.2712 0.02021 0.01196 -0.1485 0.0286 0.4219
7.500 1.2902 0.02087 0.01274 -0.1468 0.0269 0.4261
7.750 1.3095 0.02147 0.01342 -0.1452 0.0253 0.4310
8.000 1.3276 0.02216 0.01415 -0.1434 0.0240 0.4364
8.250 1.3407 0.02347 0.01554 -0.1409 0.0225 0.4418
8.500 1.3601 0.02411 0.01632 -0.1394 0.0217 0.4489
8.750 1.3787 0.02485 0.01716 -0.1379 0.0206 0.4568
9.000 1.3965 0.02565 0.01806 -0.1362 0.0197 0.4674
9.250 1.4134 0.02659 0.01911 -0.1345 0.0190 0.4817
9.500 1.4283 0.02823 0.02089 -0.1327 0.0182 0.5040
9.750 1.4472 0.02963 0.02259 -0.1315 0.0176 0.5603
10.000 1.4704 0.03060 0.02418 -0.1311 0.0171 0.7735
10.250 1.4748 0.03128 0.02519 -0.1268 0.0168 1.0000
10.500 1.4899 0.03258 0.02661 -0.1250 0.0162 1.0000
10.750 1.5036 0.03384 0.02797 -0.1230 0.0157 1.0000
11.000 1.5160 0.03512 0.02933 -0.1209 0.0153 1.0000
11.250 1.5269 0.03646 0.03073 -0.1188 0.0148 1.0000
11.500 1.5363 0.03862 0.03300 -0.1167 0.0144 1.0000
11.750 1.5408 0.04205 0.03671 -0.1142 0.0140 1.0000
12.000 1.5458 0.04391 0.03879 -0.1115 0.0138 1.0000
12.250 1.5482 0.04631 0.04142 -0.1088 0.0137 1.0000
12.500 1.5480 0.04895 0.04429 -0.1061 0.0135 1.0000
12.750 1.5443 0.05203 0.04763 -0.1034 0.0133 1.0000
13.000 1.5377 0.05545 0.05130 -0.1009 0.0131 1.0000
13.250 1.5266 0.05952 0.05564 -0.0986 0.0130 1.0000
13.500 1.5124 0.06408 0.06047 -0.0967 0.0129 1.0000
13.750 1.4956 0.06911 0.06576 -0.0955 0.0128 1.0000
14.000 1.4738 0.07518 0.07211 -0.0952 0.0127 1.0000
14.250 1.4465 0.08256 0.07979 -0.0962 0.0128 1.0000
14.500 1.4124 0.09187 0.08940 -0.0991 0.0129 1.0000
14.750 1.3785 0.10226 0.10007 -0.1041 0.0130 1.0000
15.000 1.3358 0.11628 0.11439 -0.1130 0.0131 1.0000
15.250 1.2376 0.15194 0.15045 -0.1386 0.0140 1.0000
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