WORTMANN FX 77-W-258 AIRFOIL (fx77w258-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: WORTMANN FX 77-W-258 AIRFOIL (fx77w258-il) Reynolds number: 1,000,000 Max Cl/Cd: 103.56 at α=8.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx77w258-il-1000000-n5.txt Download as CSV file: xf-fx77w258-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 77-W-258 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
------ -------- --------- --------- -------- -------- --------
-19.750 -0.9862 0.10782 0.10225 -0.0209 0.4659 0.0046
-19.500 -1.0024 0.10136 0.09567 -0.0242 0.4646 0.0046
-19.250 -1.0165 0.09540 0.08958 -0.0271 0.4632 0.0046
-19.000 -1.0280 0.08999 0.08406 -0.0296 0.4617 0.0046
-18.750 -1.0364 0.08510 0.07906 -0.0317 0.4600 0.0046
-18.500 -1.0428 0.08064 0.07450 -0.0335 0.4582 0.0046
-18.250 -1.0476 0.07649 0.07024 -0.0351 0.4563 0.0046
-18.000 -1.0504 0.07269 0.06634 -0.0365 0.4542 0.0046
-17.500 -1.0499 0.06610 0.05959 -0.0385 0.4505 0.0046
-17.250 -1.0487 0.06303 0.05644 -0.0393 0.4497 0.0046
-17.000 -1.0454 0.06027 0.05361 -0.0400 0.4488 0.0046
-16.750 -1.0409 0.05770 0.05097 -0.0405 0.4478 0.0046
-16.500 -1.0362 0.05521 0.04841 -0.0409 0.4467 0.0046
-16.250 -1.0290 0.05306 0.04621 -0.0411 0.4455 0.0046
-16.000 -1.0223 0.05091 0.04399 -0.0413 0.4443 0.0046
-15.750 -1.0139 0.04896 0.04198 -0.0414 0.4430 0.0046
-15.500 -1.0050 0.04711 0.04007 -0.0415 0.4415 0.0046
-15.250 -0.9959 0.04531 0.03821 -0.0415 0.4400 0.0046
-15.000 -0.9853 0.04372 0.03656 -0.0414 0.4385 0.0046
-14.750 -0.9747 0.04213 0.03491 -0.0412 0.4369 0.0046
-14.500 -0.9631 0.04065 0.03339 -0.0411 0.4352 0.0046
-14.250 -0.9505 0.03932 0.03201 -0.0408 0.4336 0.0046
-14.000 -0.9380 0.03802 0.03065 -0.0405 0.4321 0.0046
-13.750 -0.9258 0.03671 0.02929 -0.0402 0.4305 0.0046
-13.500 -0.9122 0.03556 0.02811 -0.0398 0.4301 0.0046
-13.250 -0.8983 0.03445 0.02697 -0.0394 0.4297 0.0046
-13.000 -0.8844 0.03336 0.02585 -0.0390 0.4291 0.0046
-12.750 -0.8704 0.03227 0.02473 -0.0385 0.4285 0.0046
-12.500 -0.8551 0.03130 0.02372 -0.0381 0.4278 0.0047
-12.250 -0.8394 0.03035 0.02275 -0.0377 0.4270 0.0047
-12.000 -0.8238 0.02941 0.02178 -0.0372 0.4262 0.0047
-11.750 -0.8076 0.02850 0.02084 -0.0368 0.4253 0.0047
-11.500 -0.7905 0.02767 0.01998 -0.0364 0.4243 0.0047
-11.250 -0.7732 0.02686 0.01914 -0.0359 0.4231 0.0047
-11.000 -0.7559 0.02604 0.01830 -0.0355 0.4219 0.0047
-10.750 -0.7382 0.02525 0.01748 -0.0351 0.4205 0.0047
-10.500 -0.7199 0.02451 0.01671 -0.0347 0.4192 0.0047
-10.250 -0.7014 0.02378 0.01595 -0.0343 0.4178 0.0047
-10.000 -0.6827 0.02306 0.01520 -0.0339 0.4165 0.0048
-9.750 -0.6635 0.02238 0.01449 -0.0336 0.4151 0.0048
-9.500 -0.6441 0.02171 0.01380 -0.0332 0.4138 0.0048
-9.250 -0.6246 0.02105 0.01311 -0.0329 0.4126 0.0048
-9.000 -0.6052 0.02043 0.01247 -0.0325 0.4113 0.0049
-8.750 -0.5890 0.01981 0.01183 -0.0315 0.4108 0.0049
-8.500 -0.5740 0.01922 0.01123 -0.0305 0.4104 0.0049
-8.250 -0.5521 0.01865 0.01064 -0.0305 0.4100 0.0050
-8.000 -0.5283 0.01810 0.01008 -0.0309 0.4095 0.0050
-7.750 -0.5029 0.01760 0.00956 -0.0315 0.4089 0.0051
-7.500 -0.4767 0.01717 0.00912 -0.0320 0.4083 0.0052
-7.250 -0.4500 0.01681 0.00874 -0.0323 0.4077 0.0053
-7.000 -0.4228 0.01648 0.00841 -0.0327 0.4070 0.0053
-6.750 -0.3950 0.01617 0.00809 -0.0332 0.4063 0.0055
-6.500 -0.3668 0.01588 0.00779 -0.0337 0.4056 0.0056
-6.250 -0.3381 0.01561 0.00751 -0.0342 0.4048 0.0058
-6.000 -0.3091 0.01534 0.00724 -0.0347 0.4039 0.0061
-5.750 -0.2797 0.01510 0.00699 -0.0353 0.4029 0.0064
-5.500 -0.2503 0.01484 0.00676 -0.0360 0.4018 0.0121
-5.250 -0.2202 0.01465 0.00658 -0.0366 0.4010 0.0128
-5.000 -0.1899 0.01448 0.00640 -0.0373 0.4002 0.0137
-4.750 -0.1594 0.01432 0.00624 -0.0380 0.3994 0.0144
-4.500 -0.1288 0.01417 0.00610 -0.0388 0.3986 0.0149
-4.250 -0.0980 0.01404 0.00596 -0.0395 0.3978 0.0153
-4.000 -0.0671 0.01390 0.00582 -0.0403 0.3969 0.0157
-3.750 -0.0361 0.01375 0.00568 -0.0411 0.3961 0.0163
-3.500 -0.0050 0.01363 0.00556 -0.0419 0.3952 0.0169
-3.250 0.0262 0.01352 0.00545 -0.0427 0.3942 0.0174
-3.000 0.0575 0.01344 0.00536 -0.0435 0.3931 0.0179
-2.750 0.0888 0.01336 0.00528 -0.0444 0.3922 0.0183
-2.500 0.1204 0.01325 0.00519 -0.0453 0.3920 0.0190
-2.250 0.1521 0.01314 0.00509 -0.0462 0.3917 0.0204
-2.000 0.1839 0.01300 0.00502 -0.0471 0.3913 0.0334
-1.750 0.2157 0.01291 0.00496 -0.0480 0.3908 0.0373
-1.500 0.2475 0.01283 0.00489 -0.0489 0.3902 0.0390
-1.250 0.2794 0.01275 0.00483 -0.0499 0.3896 0.0403
-1.000 0.3113 0.01268 0.00478 -0.0508 0.3888 0.0420
-0.750 0.3433 0.01258 0.00473 -0.0518 0.3880 0.0487
-0.500 0.3753 0.01251 0.00469 -0.0528 0.3873 0.0650
-0.250 0.4073 0.01245 0.00466 -0.0537 0.3866 0.0697
0.000 0.4396 0.01233 0.00461 -0.0549 0.3857 0.0941
0.250 0.4716 0.01227 0.00459 -0.0558 0.3848 0.1044
0.500 0.5043 0.01210 0.00453 -0.0571 0.3838 0.1439
0.750 0.5373 0.01190 0.00447 -0.0585 0.3827 0.1933
1.000 0.5716 0.01150 0.00435 -0.0605 0.3816 0.2795
1.250 0.6080 0.01082 0.00413 -0.0631 0.3805 0.4295
1.500 0.6434 0.01032 0.00403 -0.0654 0.3795 0.5559
1.750 0.6753 0.01035 0.00413 -0.0663 0.3785 0.5795
2.000 0.7068 0.01044 0.00426 -0.0671 0.3775 0.5910
2.250 0.7380 0.01055 0.00438 -0.0679 0.3761 0.5995
2.500 0.7690 0.01069 0.00451 -0.0686 0.3745 0.6076
2.750 0.8002 0.01079 0.00460 -0.0694 0.3735 0.6131
3.000 0.8317 0.01085 0.00465 -0.0702 0.3726 0.6162
3.250 0.8631 0.01090 0.00473 -0.0710 0.3714 0.6194
3.500 0.8943 0.01098 0.00485 -0.0718 0.3701 0.6239
3.750 0.9254 0.01108 0.00495 -0.0726 0.3684 0.6282
4.000 0.9565 0.01115 0.00502 -0.0734 0.3658 0.6307
4.250 0.9874 0.01123 0.00507 -0.0741 0.3620 0.6323
4.500 1.0179 0.01134 0.00514 -0.0749 0.3576 0.6336
4.750 1.0485 0.01146 0.00524 -0.0756 0.3550 0.6348
5.000 1.0791 0.01156 0.00535 -0.0764 0.3530 0.6359
5.250 1.1096 0.01165 0.00545 -0.0771 0.3502 0.6380
5.500 1.1399 0.01174 0.00555 -0.0779 0.3466 0.6406
5.750 1.1695 0.01189 0.00568 -0.0785 0.3411 0.6431
6.000 1.1988 0.01207 0.00584 -0.0791 0.3358 0.6449
6.250 1.2278 0.01227 0.00602 -0.0797 0.3309 0.6464
6.500 1.2565 0.01248 0.00622 -0.0802 0.3264 0.6474
6.750 1.2848 0.01272 0.00643 -0.0807 0.3221 0.6481
7.000 1.3137 0.01289 0.00661 -0.0813 0.3193 0.6489
7.250 1.3422 0.01308 0.00681 -0.0818 0.3162 0.6497
7.500 1.3698 0.01333 0.00705 -0.0823 0.3123 0.6505
7.750 1.3967 0.01362 0.00733 -0.0826 0.3082 0.6511
8.000 1.4235 0.01390 0.00760 -0.0829 0.3048 0.6517
8.250 1.4515 0.01407 0.00780 -0.0834 0.3028 0.6521
8.500 1.4788 0.01428 0.00802 -0.0838 0.2992 0.6526
8.750 1.5014 0.01479 0.00848 -0.0836 0.2875 0.6530
9.000 1.5186 0.01559 0.00919 -0.0827 0.2707 0.6534
9.250 1.5348 0.01637 0.00991 -0.0816 0.2601 0.6538
9.500 1.5517 0.01702 0.01054 -0.0807 0.2525 0.6542
9.750 1.5594 0.01800 0.01150 -0.0785 0.2406 0.6546
10.000 1.5530 0.01931 0.01281 -0.0743 0.2266 0.6549
10.250 1.5285 0.02280 0.01627 -0.0710 0.2106 0.6552
10.500 1.5188 0.02624 0.01977 -0.0705 0.2033 0.6555
10.750 1.5068 0.03038 0.02399 -0.0707 0.1988 0.6558
11.000 1.4839 0.03589 0.02962 -0.0709 0.1957 0.6560
11.500 1.4211 0.04808 0.04208 -0.0700 0.1926 0.6564
11.750 1.3956 0.05338 0.04749 -0.0695 0.1912 0.6565
12.000 1.3690 0.05880 0.05300 -0.0690 0.1885 0.6567
12.250 1.3420 0.06450 0.05877 -0.0687 0.1826 0.6568
12.500 1.3078 0.07108 0.06535 -0.0684 0.1714 0.6569
12.750 1.2824 0.07690 0.07119 -0.0684 0.1638 0.6570
13.250 1.2654 0.08493 0.07926 -0.0688 0.1560 0.6576
13.500 1.2605 0.08857 0.08291 -0.0691 0.1519 0.6580
13.750 1.2604 0.09166 0.08602 -0.0694 0.1466 0.6585
14.000 1.2488 0.09619 0.09054 -0.0698 0.1388 0.6589
14.250 1.2418 0.10021 0.09457 -0.0703 0.1273 0.6593
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