WORTMANN FX 082-512 AIRFOIL (fx082512-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: WORTMANN FX 082-512 AIRFOIL (fx082512-il) Reynolds number: 500,000 Max Cl/Cd: 75.3 at α=-0.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx082512-il-500000-n5.txt Download as CSV file: xf-fx082512-il-500000-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 = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-17.500 -0.6609 0.16358 0.16100 -0.0216 1.0000 0.0074
-17.250 -0.6861 0.15230 0.14963 -0.0264 1.0000 0.0075
-17.000 -0.7022 0.14404 0.14131 -0.0300 1.0000 0.0074
-16.750 -0.7222 0.13509 0.13227 -0.0339 1.0000 0.0075
-16.500 -0.7410 0.12667 0.12376 -0.0376 1.0000 0.0075
-16.250 -0.7594 0.11868 0.11567 -0.0411 1.0000 0.0075
-16.000 -0.7745 0.11171 0.10861 -0.0442 1.0000 0.0074
-15.750 -0.7906 0.10483 0.10162 -0.0474 1.0000 0.0075
-15.500 -0.8040 0.09878 0.09547 -0.0501 1.0000 0.0075
-15.250 -0.8143 0.09353 0.09013 -0.0523 1.0000 0.0075
-15.000 -0.8279 0.08802 0.08456 -0.0547 1.0000 0.0077
-14.750 -0.8367 0.08348 0.07995 -0.0565 1.0000 0.0077
-14.500 -0.8461 0.07905 0.07545 -0.0581 1.0000 0.0078
-14.250 -0.8541 0.07501 0.07134 -0.0595 1.0000 0.0079
-14.000 -0.8617 0.07127 0.06754 -0.0605 1.0000 0.0079
-13.750 -0.8694 0.06771 0.06391 -0.0614 1.0000 0.0080
-13.500 -0.8751 0.06446 0.06062 -0.0622 0.9999 0.0082
-13.250 -0.8704 0.06076 0.05684 -0.0657 0.9988 0.0083
-13.000 -0.8633 0.05757 0.05358 -0.0689 0.9974 0.0086
-12.750 -0.8563 0.05434 0.05027 -0.0723 0.9958 0.0088
-12.500 -0.8465 0.05148 0.04734 -0.0757 0.9943 0.0091
-12.250 -0.8410 0.04870 0.04449 -0.0781 0.9916 0.0094
-12.000 -0.8357 0.04583 0.04153 -0.0810 0.9886 0.0095
-11.750 -0.8247 0.04334 0.03894 -0.0842 0.9862 0.0099
-11.500 -0.8244 0.04093 0.03647 -0.0853 0.9810 0.0101
-11.250 -0.8118 0.03833 0.03378 -0.0888 0.9771 0.0103
-11.000 -0.7922 0.03440 0.02976 -0.0962 0.9744 0.0109
-10.750 -0.7828 0.03136 0.02665 -0.0998 0.9681 0.0113
-10.500 -0.7557 0.02824 0.02345 -0.1066 0.9653 0.0120
-10.250 -0.7226 0.02541 0.02050 -0.1138 0.9638 0.0127
-10.000 -0.6866 0.02279 0.01774 -0.1208 0.9629 0.0138
-9.750 -0.6492 0.02051 0.01530 -0.1271 0.9623 0.0152
-9.500 -0.6122 0.01882 0.01350 -0.1322 0.9617 0.0181
-9.250 -0.5855 0.01775 0.01234 -0.1339 0.9586 0.0204
-9.000 -0.5544 0.01679 0.01132 -0.1363 0.9567 0.0253
-8.750 -0.5220 0.01596 0.01054 -0.1387 0.9552 0.0362
-8.500 -0.4906 0.01556 0.01013 -0.1402 0.9537 0.0443
-8.250 -0.4590 0.01527 0.00981 -0.1414 0.9524 0.0491
-8.000 -0.4268 0.01495 0.00946 -0.1429 0.9513 0.0523
-7.750 -0.3945 0.01471 0.00917 -0.1442 0.9503 0.0553
-7.500 -0.3618 0.01447 0.00885 -0.1455 0.9494 0.0576
-7.250 -0.3278 0.01400 0.00833 -0.1475 0.9487 0.0603
-7.000 -0.2936 0.01359 0.00788 -0.1493 0.9480 0.0630
-6.750 -0.2600 0.01331 0.00755 -0.1509 0.9474 0.0664
-6.500 -0.2335 0.01308 0.00726 -0.1510 0.9443 0.0683
-6.250 -0.2037 0.01275 0.00687 -0.1518 0.9419 0.0692
-6.000 -0.1721 0.01243 0.00649 -0.1529 0.9401 0.0700
-5.750 -0.1394 0.01210 0.00609 -0.1542 0.9386 0.0707
-5.500 -0.1053 0.01164 0.00559 -0.1560 0.9374 0.0725
-5.250 -0.0714 0.01128 0.00518 -0.1576 0.9363 0.0742
-5.000 -0.0372 0.01095 0.00483 -0.1592 0.9352 0.0762
-4.750 -0.0027 0.01067 0.00450 -0.1608 0.9342 0.0783
-4.500 0.0320 0.01040 0.00419 -0.1624 0.9333 0.0800
-4.250 0.0676 0.01010 0.00387 -0.1643 0.9324 0.0826
-4.000 0.1037 0.00982 0.00357 -0.1662 0.9316 0.0863
-3.750 0.1303 0.00967 0.00342 -0.1661 0.9276 0.0916
-3.500 0.1687 0.00857 0.00282 -0.1696 0.9261 0.2489
-3.250 0.2007 0.00845 0.00276 -0.1705 0.9228 0.2754
-3.000 0.2372 0.00831 0.00263 -0.1722 0.9191 0.2866
-2.750 0.2782 0.00815 0.00245 -0.1749 0.9163 0.2935
-2.500 0.3103 0.00810 0.00241 -0.1758 0.9115 0.2985
-2.250 0.3405 0.00807 0.00236 -0.1761 0.9050 0.3033
-2.000 0.3782 0.00800 0.00229 -0.1782 0.9012 0.3074
-1.750 0.4142 0.00796 0.00226 -0.1799 0.8956 0.3109
-1.500 0.4449 0.00793 0.00223 -0.1803 0.8868 0.3137
-1.250 0.4811 0.00790 0.00217 -0.1820 0.8771 0.3169
-1.000 0.5170 0.00788 0.00212 -0.1836 0.8663 0.3191
-0.750 0.5502 0.00785 0.00209 -0.1846 0.8498 0.3213
-0.500 0.5827 0.00790 0.00206 -0.1854 0.8210 0.3244
-0.250 0.6114 0.00812 0.00205 -0.1853 0.7710 0.3272
0.000 0.6291 0.00859 0.00214 -0.1828 0.6967 0.3297
0.250 0.6403 0.00927 0.00235 -0.1790 0.6030 0.3317
0.500 0.6516 0.01015 0.00265 -0.1756 0.4835 0.3333
0.750 0.6652 0.01123 0.00308 -0.1729 0.3363 0.3345
1.000 0.6842 0.01203 0.00342 -0.1713 0.2317 0.3357
1.250 0.7017 0.01304 0.00389 -0.1695 0.0943 0.3369
1.500 0.7273 0.01323 0.00408 -0.1690 0.0876 0.3383
1.750 0.7529 0.01344 0.00428 -0.1685 0.0835 0.3397
2.000 0.7787 0.01361 0.00447 -0.1680 0.0814 0.3412
2.250 0.8043 0.01379 0.00469 -0.1675 0.0793 0.3428
2.500 0.8296 0.01401 0.00491 -0.1669 0.0775 0.3444
2.750 0.8545 0.01426 0.00517 -0.1662 0.0758 0.3461
3.000 0.8791 0.01453 0.00546 -0.1655 0.0742 0.3477
3.250 0.9044 0.01472 0.00570 -0.1650 0.0730 0.3494
3.500 0.9294 0.01494 0.00598 -0.1643 0.0718 0.3511
3.750 0.9541 0.01518 0.00627 -0.1636 0.0702 0.3528
4.000 0.9789 0.01539 0.00653 -0.1630 0.0672 0.3546
4.250 1.0025 0.01571 0.00685 -0.1621 0.0635 0.3564
4.500 1.0267 0.01594 0.00713 -0.1614 0.0615 0.3583
4.750 1.0513 0.01610 0.00735 -0.1606 0.0591 0.3602
5.000 1.0756 0.01628 0.00756 -0.1599 0.0562 0.3621
5.250 1.0989 0.01652 0.00780 -0.1590 0.0532 0.3637
5.500 1.1232 0.01668 0.00804 -0.1582 0.0496 0.3659
5.750 1.1470 0.01687 0.00825 -0.1574 0.0443 0.3681
6.000 1.1700 0.01713 0.00849 -0.1564 0.0355 0.3706
6.250 1.1911 0.01758 0.00891 -0.1552 0.0267 0.3733
6.500 1.2115 0.01808 0.00941 -0.1537 0.0219 0.3760
6.750 1.2317 0.01860 0.00997 -0.1522 0.0182 0.3785
7.250 1.2724 0.01957 0.01110 -0.1493 0.0155 0.3834
7.500 1.2918 0.02016 0.01174 -0.1478 0.0143 0.3862
7.750 1.3101 0.02086 0.01251 -0.1460 0.0131 0.3892
8.000 1.3287 0.02152 0.01325 -0.1443 0.0123 0.3925
8.250 1.3476 0.02211 0.01392 -0.1427 0.0117 0.3957
8.500 1.3660 0.02274 0.01467 -0.1411 0.0111 0.3990
8.750 1.3841 0.02342 0.01543 -0.1394 0.0105 0.4033
9.000 1.4015 0.02416 0.01625 -0.1377 0.0100 0.4082
9.250 1.4178 0.02502 0.01718 -0.1358 0.0096 0.4133
9.500 1.4314 0.02615 0.01842 -0.1336 0.0091 0.4190
9.750 1.4477 0.02700 0.01939 -0.1318 0.0089 0.4262
10.000 1.4635 0.02791 0.02044 -0.1299 0.0086 0.4338
10.250 1.4784 0.02890 0.02156 -0.1280 0.0084 0.4438
10.500 1.4931 0.02991 0.02270 -0.1261 0.0081 0.4568
10.750 1.5075 0.03094 0.02391 -0.1243 0.0078 0.4754
11.000 1.5216 0.03200 0.02513 -0.1226 0.0075 0.5053
11.250 1.5361 0.03309 0.02642 -0.1210 0.0072 0.5613
11.500 1.5508 0.03430 0.02793 -0.1197 0.0070 0.6685
11.750 1.5532 0.03512 0.02927 -0.1159 0.0069 1.0000
12.000 1.5593 0.03693 0.03119 -0.1134 0.0067 1.0000
12.250 1.5648 0.03885 0.03324 -0.1110 0.0065 1.0000
12.500 1.5723 0.04057 0.03512 -0.1089 0.0064 1.0000
12.750 1.5782 0.04248 0.03718 -0.1068 0.0063 1.0000
13.000 1.5822 0.04462 0.03948 -0.1047 0.0062 1.0000
13.250 1.5848 0.04694 0.04196 -0.1027 0.0061 1.0000
13.500 1.5862 0.04942 0.04460 -0.1008 0.0060 1.0000
13.750 1.5855 0.05222 0.04758 -0.0991 0.0059 1.0000
14.000 1.5837 0.05521 0.05074 -0.0975 0.0058 1.0000
14.250 1.5799 0.05854 0.05425 -0.0963 0.0057 1.0000
14.500 1.5747 0.06219 0.05808 -0.0953 0.0057 1.0000
14.750 1.5681 0.06620 0.06226 -0.0948 0.0056 1.0000
15.000 1.5579 0.07093 0.06719 -0.0948 0.0056 1.0000
15.250 1.5489 0.07575 0.07218 -0.0953 0.0055 1.0000
15.500 1.5362 0.08145 0.07807 -0.0966 0.0055 1.0000
15.750 1.5228 0.08762 0.08444 -0.0986 0.0054 1.0000
16.000 1.5032 0.09541 0.09244 -0.1018 0.0054 1.0000
16.250 1.4839 0.10376 0.10100 -0.1061 0.0054 1.0000
16.500 1.4602 0.11377 0.11123 -0.1119 0.0054 1.0000
16.750 1.4332 0.12546 0.12315 -0.1195 0.0054 1.0000
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