WORTMANN FX 3 AIRFOIL (fx3-il) Xfoil prediction polar at RE=500,000 Ncrit=0
| Details | Polar file |
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Airfoil: WORTMANN FX 3 AIRFOIL (fx3-il) Reynolds number: 500,000 Max Cl/Cd: 40.93 at α=7.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx3-il-500000.txt Download as CSV file: xf-fx3-il-500000.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 3 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
------ -------- --------- --------- -------- -------- --------
-17.750 -0.4499 0.11374 0.11061 -0.1246 0.8401 0.0147
-17.500 -0.4948 0.09957 0.09624 -0.1325 0.8405 0.0144
-17.250 -0.5371 0.08763 0.08408 -0.1394 0.8410 0.0142
-17.000 -0.5638 0.07949 0.07575 -0.1442 0.8414 0.0141
-16.750 -0.5825 0.07319 0.06927 -0.1477 0.8419 0.0141
-16.500 -0.5963 0.06807 0.06398 -0.1504 0.8424 0.0142
-16.250 -0.6059 0.06384 0.05958 -0.1524 0.8429 0.0143
-16.000 -0.6122 0.06027 0.05585 -0.1539 0.8434 0.0144
-15.750 -0.6191 0.05689 0.05230 -0.1549 0.8439 0.0145
-15.500 -0.6331 0.05287 0.04805 -0.1551 0.8445 0.0147
-15.250 -0.6376 0.05004 0.04507 -0.1552 0.8451 0.0150
-15.000 -0.6357 0.04800 0.04292 -0.1552 0.8457 0.0153
-14.750 -0.6307 0.04635 0.04120 -0.1551 0.8462 0.0156
-14.500 -0.6238 0.04491 0.03968 -0.1551 0.8464 0.0159
-14.250 -0.6161 0.04361 0.03830 -0.1549 0.8467 0.0163
-14.000 -0.6074 0.04250 0.03710 -0.1546 0.8473 0.0167
-13.750 -0.5984 0.04154 0.03602 -0.1541 0.8478 0.0171
-13.500 -0.5895 0.04095 0.03533 -0.1533 0.8487 0.0176
-13.250 -0.5749 0.03967 0.03395 -0.1534 0.8493 0.0181
-13.000 -0.5542 0.03947 0.03376 -0.1570 0.8571 0.0186
-12.750 -0.5478 0.03874 0.03296 -0.1557 0.8603 0.0195
-12.500 -0.5387 0.03838 0.03257 -0.1544 0.8622 0.0203
-11.500 -0.7522 0.04425 0.03849 -0.1028 0.8738 0.0185
-11.250 -0.7527 0.04324 0.03739 -0.0992 0.8710 0.0191
-11.000 -0.7477 0.04236 0.03647 -0.0967 0.8694 0.0200
-10.750 -0.7379 0.04179 0.03587 -0.0950 0.8683 0.0207
-10.500 -0.7258 0.04132 0.03536 -0.0936 0.8675 0.0216
-10.250 -0.7117 0.04088 0.03486 -0.0925 0.8668 0.0226
-10.000 -0.6953 0.04052 0.03440 -0.0917 0.8661 0.0235
-9.750 -0.6822 0.04000 0.03382 -0.0904 0.8656 0.0248
-9.500 -0.7416 0.03969 0.03348 -0.0755 0.8563 0.0238
-9.250 -0.7418 0.03887 0.03263 -0.0717 0.8544 0.0250
-9.000 -0.7356 0.03836 0.03212 -0.0691 0.8530 0.0265
-8.750 -0.7244 0.03808 0.03180 -0.0671 0.8520 0.0281
-8.500 -0.7138 0.03786 0.03153 -0.0650 0.8512 0.0298
-8.250 -0.7011 0.03749 0.03112 -0.0635 0.8506 0.0320
-8.000 -0.6808 0.03739 0.03105 -0.0633 0.8502 0.0348
-7.750 -0.7308 0.03616 0.02979 -0.0510 0.8412 0.0339
-7.500 -0.7107 0.03592 0.02952 -0.0508 0.8398 0.0369
-7.250 -0.6894 0.03551 0.02908 -0.0509 0.8386 0.0403
-7.000 -0.6632 0.03542 0.02901 -0.0518 0.8377 0.0442
-6.750 -0.6349 0.03553 0.02906 -0.0528 0.8370 0.0472
-6.500 -0.6090 0.03509 0.02867 -0.0539 0.8365 0.0517
-6.250 -0.5789 0.03518 0.02874 -0.0554 0.8360 0.0553
-6.000 -0.5476 0.03540 0.02891 -0.0570 0.8355 0.0576
-5.750 -0.5174 0.03503 0.02856 -0.0591 0.8352 0.0625
-5.500 -0.5358 0.03418 0.02771 -0.0528 0.8269 0.0632
-5.250 -0.5068 0.03406 0.02757 -0.0543 0.8252 0.0666
-5.000 -0.4759 0.03405 0.02752 -0.0559 0.8240 0.0694
-4.750 -0.4419 0.03382 0.02726 -0.0585 0.8232 0.0735
-4.500 -0.4072 0.03372 0.02719 -0.0612 0.8225 0.0792
-4.250 -0.3725 0.03379 0.02723 -0.0636 0.8219 0.0839
-4.000 -0.3348 0.03377 0.02722 -0.0668 0.8214 0.0916
-3.750 -0.2960 0.03382 0.02732 -0.0702 0.8210 0.1050
-3.500 -0.2215 0.03301 0.02918 -0.0845 0.8212 0.5999
-3.000 -0.1891 0.03391 0.02989 -0.0825 0.8111 0.6603
-2.750 -0.1689 0.03494 0.03091 -0.0799 0.8090 0.6690
-2.500 -0.1056 0.03889 0.03483 -0.0835 0.8191 0.6800
-2.000 -0.1269 0.03716 0.03317 -0.0687 0.7962 0.6835
-1.750 -0.0835 0.03758 0.03347 -0.0727 0.7948 0.6926
-1.500 -0.0612 0.03794 0.03385 -0.0700 0.7936 0.6940
-1.250 -0.0526 0.03774 0.03366 -0.0653 0.7839 0.6957
-1.000 -0.0323 0.03810 0.03402 -0.0625 0.7821 0.6983
-0.750 0.0071 0.03842 0.03427 -0.0654 0.7812 0.7078
-0.500 0.0265 0.03866 0.03453 -0.0622 0.7804 0.7095
-0.250 0.0438 0.03916 0.03506 -0.0579 0.7797 0.7132
0.000 0.0523 0.03911 0.03499 -0.0553 0.7701 0.7236
0.250 0.0680 0.03919 0.03510 -0.0513 0.7690 0.7263
0.500 0.0968 0.03915 0.03504 -0.0512 0.7683 0.7288
0.750 0.1334 0.03906 0.03492 -0.0535 0.7678 0.7318
1.000 0.1410 0.03962 0.03553 -0.0461 0.7672 0.7473
1.250 0.1542 0.04067 0.03658 -0.0447 0.7577 0.7686
1.500 0.1762 0.03973 0.03564 -0.0432 0.7569 0.7696
1.750 0.1920 0.03919 0.03510 -0.0408 0.7535 0.7708
2.000 0.2260 0.03868 0.03459 -0.0416 0.7549 0.7720
2.250 0.2321 0.03838 0.03431 -0.0382 0.7467 0.7742
2.500 0.2858 0.03902 0.03492 -0.0452 0.7461 0.7853
2.750 0.3102 0.03812 0.03404 -0.0444 0.7453 0.7862
3.000 0.3370 0.03743 0.03336 -0.0441 0.7446 0.7873
3.250 0.3652 0.03684 0.03278 -0.0440 0.7441 0.7886
3.500 0.3697 0.03670 0.03267 -0.0404 0.7349 0.7909
3.750 0.4015 0.03626 0.03225 -0.0415 0.7339 0.7933
4.000 0.4483 0.03633 0.03234 -0.0466 0.7333 0.8025
4.250 0.4554 0.03599 0.03203 -0.0433 0.7256 0.8038
4.500 0.4810 0.03541 0.03148 -0.0430 0.7234 0.8051
4.750 0.5096 0.03484 0.03094 -0.0433 0.7221 0.8069
5.000 0.5413 0.03429 0.03044 -0.0442 0.7211 0.8094
5.250 0.5883 0.03421 0.03038 -0.0491 0.7203 0.8184
5.500 0.6171 0.03325 0.02947 -0.0491 0.7195 0.8194
5.750 0.6247 0.03316 0.02943 -0.0461 0.7093 0.8210
6.000 0.6572 0.03229 0.02861 -0.0469 0.7077 0.8226
7.000 0.9027 0.03004 0.02644 -0.0845 0.6712 0.7649
7.250 0.9564 0.02811 0.02448 -0.0888 0.6546 0.7637
7.500 1.0177 0.02567 0.02183 -0.0940 0.6193 0.7624
7.750 1.0465 0.02557 0.02140 -0.0955 0.5670 0.7584
8.000 1.0676 0.02713 0.02251 -0.0981 0.5009 0.7509
8.250 1.0671 0.02847 0.02360 -0.0945 0.4514 0.7502
8.500 1.0683 0.02985 0.02469 -0.0914 0.3984 0.7495
8.750 1.0703 0.03129 0.02580 -0.0886 0.3385 0.7487
9.000 1.0730 0.03278 0.02692 -0.0860 0.2749 0.7480
9.250 1.0770 0.03425 0.02802 -0.0837 0.2126 0.7473
9.500 1.0848 0.03557 0.02903 -0.0819 0.1627 0.7465
10.000 1.1125 0.03761 0.03078 -0.0802 0.1090 0.7457
10.250 1.1278 0.03855 0.03164 -0.0795 0.0919 0.7454
10.500 1.1439 0.03950 0.03251 -0.0790 0.0767 0.7447
10.750 1.1585 0.04059 0.03351 -0.0784 0.0592 0.7439
11.000 1.1688 0.04201 0.03474 -0.0772 0.0372 0.7432
11.250 1.1817 0.04330 0.03597 -0.0764 0.0292 0.7425
11.500 1.1961 0.04449 0.03719 -0.0757 0.0257 0.7418
11.750 1.2107 0.04568 0.03842 -0.0752 0.0237 0.7412
12.000 1.2213 0.04721 0.03996 -0.0741 0.0218 0.7406
12.250 1.2302 0.04889 0.04171 -0.0729 0.0205 0.7401
12.500 1.2442 0.05018 0.04307 -0.0723 0.0196 0.7397
12.750 1.2561 0.05162 0.04457 -0.0716 0.0187 0.7392
13.000 1.2664 0.05317 0.04619 -0.0706 0.0179 0.7389
13.250 1.2748 0.05489 0.04795 -0.0695 0.0171 0.7385
13.500 1.2779 0.05709 0.05021 -0.0679 0.0164 0.7382
13.750 1.2780 0.05956 0.05277 -0.0660 0.0158 0.7379
14.000 1.2882 0.06120 0.05449 -0.0652 0.0155 0.7376
14.250 1.2969 0.06297 0.05634 -0.0642 0.0151 0.7373
14.500 1.3043 0.06484 0.05830 -0.0632 0.0147 0.7371
14.750 1.3110 0.06680 0.06034 -0.0622 0.0143 0.7369
15.000 1.3180 0.06876 0.06239 -0.0614 0.0139 0.7367
15.250 1.3243 0.07086 0.06456 -0.0606 0.0135 0.7366
15.500 1.3302 0.07300 0.06676 -0.0599 0.0131 0.7366
15.750 1.3344 0.07533 0.06914 -0.0592 0.0128 0.7366
16.000 1.3357 0.07778 0.07166 -0.0580 0.0124 0.7365
16.250 1.3391 0.08011 0.07410 -0.0570 0.0121 0.7364
16.500 1.3444 0.08250 0.07662 -0.0566 0.0119 0.7363
16.750 1.3489 0.08500 0.07924 -0.0563 0.0117 0.7362
17.000 1.3526 0.08759 0.08197 -0.0561 0.0116 0.7360
17.250 1.3553 0.09033 0.08484 -0.0558 0.0114 0.7359
17.500 1.3572 0.09318 0.08781 -0.0557 0.0112 0.7358
17.750 1.3581 0.09620 0.09097 -0.0558 0.0110 0.7356
18.000 1.3582 0.09935 0.09424 -0.0559 0.0108 0.7355
18.250 1.3579 0.10262 0.09763 -0.0563 0.0107 0.7354
18.500 1.3567 0.10605 0.10119 -0.0568 0.0105 0.7352
18.750 1.3546 0.10970 0.10497 -0.0576 0.0104 0.7351
19.000 1.3515 0.11356 0.10896 -0.0587 0.0103 0.7350
19.250 1.3483 0.11752 0.11305 -0.0600 0.0101 0.7349
19.500 1.3438 0.12172 0.11738 -0.0615 0.0100 0.7347
19.750 1.3407 0.12576 0.12151 -0.0633 0.0099 0.7346
20.000 1.3352 0.13025 0.12613 -0.0652 0.0098 0.7345
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