WORTMANN FX 082-512 AIRFOIL (fx082512-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: WORTMANN FX 082-512 AIRFOIL (fx082512-il) Reynolds number: 1,000,000 Max Cl/Cd: 82.08 at α=5.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx082512-il-1000000-n5.txt Download as CSV file: xf-fx082512-il-1000000-n5.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 = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-17.250 -0.8140 0.12409 0.12169 -0.0382 1.0000 0.0051
-17.000 -0.8462 0.11362 0.11108 -0.0431 1.0000 0.0051
-16.750 -0.8708 0.10524 0.10258 -0.0471 1.0000 0.0051
-16.500 -0.8912 0.09807 0.09530 -0.0506 1.0000 0.0050
-16.250 -0.9048 0.09240 0.08954 -0.0532 1.0000 0.0050
-16.000 -0.9124 0.08794 0.08501 -0.0551 1.0000 0.0051
-15.750 -0.9216 0.08337 0.08036 -0.0570 1.0000 0.0051
-15.500 -0.9273 0.07882 0.07572 -0.0596 0.9998 0.0052
-15.250 -0.9259 0.07475 0.07157 -0.0628 0.9993 0.0052
-15.000 -0.9247 0.07065 0.06739 -0.0661 0.9986 0.0053
-14.750 -0.9217 0.06689 0.06355 -0.0693 0.9978 0.0053
-14.500 -0.9224 0.06264 0.05922 -0.0729 0.9969 0.0055
-14.250 -0.9203 0.05880 0.05530 -0.0764 0.9959 0.0056
-14.000 -0.9151 0.05539 0.05182 -0.0798 0.9951 0.0056
-13.750 -0.9098 0.05207 0.04842 -0.0832 0.9942 0.0057
-13.500 -0.9055 0.04920 0.04551 -0.0853 0.9922 0.0060
-13.250 -0.8994 0.04630 0.04255 -0.0882 0.9900 0.0061
-13.000 -0.8902 0.04376 0.03996 -0.0911 0.9881 0.0063
-12.750 -0.8804 0.04099 0.03713 -0.0948 0.9864 0.0065
-12.500 -0.8795 0.03846 0.03454 -0.0963 0.9822 0.0066
-12.250 -0.8709 0.03565 0.03168 -0.0995 0.9775 0.0067
-12.000 -0.8504 0.03258 0.02853 -0.1053 0.9753 0.0069
-11.750 -0.8383 0.02987 0.02575 -0.1087 0.9700 0.0071
-11.500 -0.8156 0.02703 0.02281 -0.1143 0.9665 0.0074
-11.250 -0.7855 0.02412 0.01980 -0.1211 0.9646 0.0076
-11.000 -0.7500 0.02074 0.01632 -0.1296 0.9635 0.0083
-10.750 -0.7139 0.01839 0.01387 -0.1360 0.9627 0.0089
-10.500 -0.6800 0.01714 0.01254 -0.1397 0.9621 0.0096
-10.250 -0.6464 0.01619 0.01151 -0.1427 0.9616 0.0101
-10.000 -0.6225 0.01535 0.01061 -0.1434 0.9576 0.0109
-9.750 -0.5913 0.01447 0.00968 -0.1457 0.9559 0.0121
-9.500 -0.5596 0.01375 0.00892 -0.1477 0.9545 0.0134
-9.250 -0.5277 0.01318 0.00827 -0.1494 0.9533 0.0146
-9.000 -0.4949 0.01250 0.00756 -0.1515 0.9522 0.0184
-8.750 -0.4622 0.01191 0.00694 -0.1533 0.9513 0.0227
-8.500 -0.4289 0.01125 0.00634 -0.1554 0.9505 0.0355
-8.250 -0.3967 0.01089 0.00599 -0.1568 0.9496 0.0431
-8.000 -0.3641 0.01061 0.00572 -0.1582 0.9488 0.0475
-7.750 -0.3313 0.01037 0.00545 -0.1595 0.9481 0.0500
-7.500 -0.2980 0.01009 0.00517 -0.1610 0.9475 0.0527
-7.250 -0.2678 0.00990 0.00497 -0.1617 0.9456 0.0549
-7.000 -0.2391 0.00973 0.00478 -0.1621 0.9430 0.0565
-6.750 -0.2088 0.00961 0.00463 -0.1627 0.9410 0.0579
-6.500 -0.1760 0.00932 0.00430 -0.1641 0.9395 0.0605
-6.250 -0.1421 0.00903 0.00399 -0.1656 0.9382 0.0625
-6.000 -0.1078 0.00878 0.00370 -0.1672 0.9369 0.0637
-5.750 -0.0729 0.00854 0.00344 -0.1689 0.9356 0.0650
-5.500 -0.0374 0.00832 0.00318 -0.1708 0.9344 0.0662
-5.250 -0.0011 0.00812 0.00295 -0.1727 0.9331 0.0674
-5.000 0.0358 0.00793 0.00274 -0.1748 0.9319 0.0686
-4.750 0.0669 0.00780 0.00259 -0.1756 0.9292 0.0696
-4.500 0.0968 0.00769 0.00246 -0.1761 0.9258 0.0703
-4.250 0.1323 0.00752 0.00226 -0.1779 0.9223 0.0719
-4.000 0.1746 0.00733 0.00205 -0.1812 0.9177 0.0746
-3.500 0.2423 0.00710 0.00181 -0.1839 0.9100 0.0800
-3.250 0.2766 0.00697 0.00169 -0.1854 0.9040 0.0866
-3.000 0.3235 0.00596 0.00118 -0.1907 0.8995 0.2581
-2.750 0.3533 0.00591 0.00116 -0.1911 0.8923 0.2730
-2.500 0.3871 0.00591 0.00114 -0.1924 0.8829 0.2805
-2.250 0.4159 0.00591 0.00114 -0.1925 0.8733 0.2872
-2.000 0.4463 0.00594 0.00112 -0.1930 0.8617 0.2908
-1.750 0.4744 0.00599 0.00111 -0.1929 0.8397 0.2942
-1.500 0.4999 0.00612 0.00112 -0.1922 0.8092 0.2981
-1.250 0.5209 0.00636 0.00116 -0.1905 0.7663 0.3011
-1.000 0.5375 0.00676 0.00126 -0.1878 0.7031 0.3034
-0.750 0.5518 0.00737 0.00144 -0.1848 0.6086 0.3046
-0.500 0.5677 0.00818 0.00170 -0.1824 0.4855 0.3063
-0.250 0.5840 0.00919 0.00206 -0.1802 0.3316 0.3082
0.000 0.6057 0.00977 0.00230 -0.1790 0.2463 0.3102
0.250 0.6238 0.01073 0.00270 -0.1772 0.0892 0.3120
0.500 0.6503 0.01088 0.00282 -0.1769 0.0821 0.3143
0.750 0.6768 0.01101 0.00294 -0.1765 0.0785 0.3168
1.000 0.7030 0.01117 0.00307 -0.1761 0.0751 0.3190
1.250 0.7298 0.01128 0.00320 -0.1758 0.0738 0.3216
1.500 0.7565 0.01139 0.00333 -0.1755 0.0726 0.3230
1.750 0.7830 0.01152 0.00347 -0.1751 0.0713 0.3244
2.000 0.8093 0.01166 0.00363 -0.1747 0.0700 0.3258
2.250 0.8355 0.01181 0.00378 -0.1743 0.0687 0.3272
2.500 0.8615 0.01197 0.00395 -0.1739 0.0672 0.3286
2.750 0.8872 0.01215 0.00414 -0.1734 0.0653 0.3299
3.000 0.9127 0.01236 0.00437 -0.1728 0.0635 0.3312
3.250 0.9383 0.01253 0.00456 -0.1722 0.0621 0.3325
3.500 0.9645 0.01264 0.00469 -0.1718 0.0606 0.3340
3.750 0.9905 0.01277 0.00484 -0.1714 0.0584 0.3360
4.000 1.0160 0.01293 0.00502 -0.1709 0.0562 0.3377
4.250 1.0412 0.01313 0.00522 -0.1703 0.0537 0.3394
4.500 1.0666 0.01329 0.00540 -0.1697 0.0517 0.3411
4.750 1.0918 0.01346 0.00558 -0.1691 0.0482 0.3429
5.000 1.1166 0.01366 0.00578 -0.1684 0.0444 0.3446
5.250 1.1409 0.01390 0.00598 -0.1677 0.0367 0.3461
5.500 1.1636 0.01428 0.00629 -0.1667 0.0254 0.3475
5.750 1.1862 0.01464 0.00664 -0.1656 0.0192 0.3489
6.000 1.2090 0.01494 0.00699 -0.1645 0.0170 0.3511
6.250 1.2310 0.01529 0.00737 -0.1633 0.0151 0.3532
6.500 1.2522 0.01569 0.00779 -0.1619 0.0132 0.3553
6.750 1.2739 0.01604 0.00818 -0.1607 0.0122 0.3576
7.000 1.2954 0.01640 0.00857 -0.1594 0.0114 0.3600
7.250 1.3163 0.01681 0.00901 -0.1580 0.0106 0.3621
7.500 1.3365 0.01727 0.00948 -0.1565 0.0098 0.3639
7.750 1.3563 0.01777 0.01003 -0.1549 0.0091 0.3665
8.000 1.3768 0.01818 0.01052 -0.1535 0.0088 0.3692
8.250 1.3968 0.01863 0.01103 -0.1520 0.0084 0.3719
8.500 1.4165 0.01911 0.01156 -0.1505 0.0080 0.3747
8.750 1.4359 0.01962 0.01212 -0.1489 0.0077 0.3774
9.000 1.4547 0.02017 0.01270 -0.1473 0.0073 0.3798
9.250 1.4727 0.02079 0.01337 -0.1455 0.0069 0.3830
9.500 1.4899 0.02148 0.01413 -0.1437 0.0065 0.3867
9.750 1.5081 0.02204 0.01476 -0.1420 0.0064 0.3908
10.000 1.5258 0.02266 0.01545 -0.1403 0.0062 0.3951
10.250 1.5431 0.02332 0.01621 -0.1385 0.0060 0.4002
10.500 1.5597 0.02402 0.01698 -0.1367 0.0058 0.4066
10.750 1.5758 0.02475 0.01779 -0.1348 0.0056 0.4128
11.000 1.5919 0.02551 0.01864 -0.1330 0.0054 0.4209
11.500 1.6219 0.02720 0.02051 -0.1291 0.0051 0.4438
11.750 1.6361 0.02815 0.02157 -0.1272 0.0050 0.4629
12.000 1.6490 0.02925 0.02281 -0.1252 0.0048 0.4927
12.250 1.6605 0.03055 0.02431 -0.1231 0.0046 0.5452
12.500 1.6753 0.03167 0.02569 -0.1217 0.0046 0.6482
13.000 1.6945 0.03368 0.02839 -0.1170 0.0045 1.0000
13.250 1.7040 0.03504 0.02985 -0.1149 0.0044 1.0000
13.500 1.7124 0.03649 0.03140 -0.1128 0.0043 1.0000
13.750 1.7193 0.03812 0.03313 -0.1106 0.0043 1.0000
14.000 1.7263 0.03976 0.03488 -0.1085 0.0042 1.0000
14.250 1.7321 0.04155 0.03677 -0.1065 0.0041 1.0000
14.500 1.7363 0.04353 0.03885 -0.1045 0.0040 1.0000
14.750 1.7394 0.04567 0.04112 -0.1026 0.0040 1.0000
15.000 1.7431 0.04780 0.04335 -0.1009 0.0039 1.0000
15.250 1.7439 0.05032 0.04599 -0.0993 0.0038 1.0000
15.500 1.7444 0.05295 0.04873 -0.0979 0.0038 1.0000
15.750 1.7431 0.05589 0.05180 -0.0966 0.0037 1.0000
16.000 1.7430 0.05880 0.05481 -0.0957 0.0036 1.0000
16.250 1.7404 0.06215 0.05828 -0.0950 0.0036 1.0000
16.500 1.7348 0.06604 0.06230 -0.0946 0.0036 1.0000
16.750 1.7288 0.07018 0.06657 -0.0946 0.0035 1.0000
17.000 1.7195 0.07502 0.07156 -0.0951 0.0035 1.0000
17.250 1.7084 0.08042 0.07711 -0.0962 0.0035 1.0000
17.500 1.6972 0.08610 0.08294 -0.0978 0.0034 1.0000
17.750 1.6804 0.09310 0.09011 -0.1005 0.0034 1.0000
18.000 1.6607 0.10112 0.09831 -0.1042 0.0034 1.0000
18.250 1.6391 0.11006 0.10743 -0.1089 0.0034 1.0000
18.500 1.6114 0.12092 0.11850 -0.1155 0.0034 1.0000
18.750 1.5729 0.13516 0.13299 -0.1250 0.0034 1.0000
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