WORTMANN FX 79-K-144/17 AIRFOIL (fx79k144-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: WORTMANN FX 79-K-144/17 AIRFOIL (fx79k144-il) Reynolds number: 1,000,000 Max Cl/Cd: 102.73 at α=3.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx79k144-il-1000000-n5.txt Download as CSV file: xf-fx79k144-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 79-K-144/17 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
------ -------- --------- --------- -------- -------- --------
-15.750 -1.0203 0.05612 0.05275 -0.0621 0.7714 0.0046
-15.500 -1.0465 0.04832 0.04474 -0.0674 0.7711 0.0045
-15.250 -1.0621 0.04345 0.03970 -0.0694 0.7707 0.0046
-15.000 -1.0718 0.03988 0.03597 -0.0699 0.7703 0.0046
-14.750 -1.0772 0.03705 0.03300 -0.0695 0.7699 0.0046
-14.500 -1.0793 0.03468 0.03048 -0.0687 0.7695 0.0046
-14.250 -1.0785 0.03265 0.02831 -0.0676 0.7691 0.0047
-14.000 -1.0749 0.03088 0.02641 -0.0664 0.7687 0.0047
-13.750 -1.0690 0.02930 0.02470 -0.0652 0.7683 0.0048
-13.500 -1.0607 0.02789 0.02317 -0.0640 0.7680 0.0049
-13.250 -1.0509 0.02661 0.02176 -0.0628 0.7676 0.0049
-13.000 -1.0415 0.02553 0.02057 -0.0611 0.7672 0.0050
-12.750 -1.0275 0.02449 0.01941 -0.0600 0.7667 0.0050
-12.500 -1.0112 0.02351 0.01832 -0.0592 0.7662 0.0051
-12.250 -0.9934 0.02260 0.01729 -0.0585 0.7657 0.0052
-12.000 -0.9744 0.02176 0.01633 -0.0578 0.7651 0.0052
-11.750 -0.9543 0.02098 0.01545 -0.0573 0.7646 0.0053
-11.500 -0.9333 0.02025 0.01462 -0.0569 0.7641 0.0054
-11.250 -0.9115 0.01954 0.01383 -0.0565 0.7637 0.0055
-11.000 -0.8890 0.01889 0.01309 -0.0562 0.7633 0.0056
-10.750 -0.8659 0.01827 0.01240 -0.0559 0.7629 0.0057
-10.500 -0.8422 0.01770 0.01174 -0.0557 0.7624 0.0058
-10.250 -0.8181 0.01717 0.01114 -0.0556 0.7619 0.0059
-10.000 -0.7935 0.01667 0.01057 -0.0555 0.7614 0.0060
-9.750 -0.7687 0.01617 0.01001 -0.0554 0.7608 0.0061
-9.500 -0.7437 0.01567 0.00946 -0.0553 0.7602 0.0064
-9.250 -0.7183 0.01522 0.00896 -0.0553 0.7597 0.0066
-9.000 -0.6926 0.01479 0.00849 -0.0553 0.7592 0.0070
-8.750 -0.6667 0.01439 0.00804 -0.0554 0.7587 0.0073
-8.500 -0.6406 0.01400 0.00763 -0.0554 0.7582 0.0078
-8.250 -0.6142 0.01365 0.00728 -0.0555 0.7577 0.0087
-8.000 -0.5874 0.01337 0.00703 -0.0557 0.7572 0.0108
-7.750 -0.5600 0.01315 0.00680 -0.0560 0.7566 0.0131
-7.500 -0.5325 0.01294 0.00655 -0.0562 0.7560 0.0140
-7.250 -0.5052 0.01269 0.00629 -0.0564 0.7553 0.0148
-7.000 -0.4776 0.01247 0.00606 -0.0567 0.7548 0.0156
-6.750 -0.4499 0.01226 0.00583 -0.0569 0.7542 0.0164
-6.500 -0.4221 0.01205 0.00560 -0.0572 0.7534 0.0171
-6.250 -0.3941 0.01186 0.00539 -0.0575 0.7526 0.0177
-6.000 -0.3660 0.01169 0.00518 -0.0578 0.7519 0.0181
-5.750 -0.3385 0.01139 0.00485 -0.0580 0.7512 0.0189
-5.500 -0.3107 0.01114 0.00460 -0.0583 0.7505 0.0196
-5.250 -0.2827 0.01094 0.00438 -0.0586 0.7497 0.0204
-5.000 -0.2545 0.01073 0.00417 -0.0590 0.7488 0.0210
-4.750 -0.2261 0.01053 0.00397 -0.0593 0.7478 0.0215
-4.500 -0.1976 0.01034 0.00378 -0.0597 0.7467 0.0220
-4.250 -0.1690 0.01018 0.00361 -0.0601 0.7457 0.0228
-4.000 -0.1404 0.01000 0.00343 -0.0605 0.7446 0.0239
-3.750 -0.1118 0.00981 0.00326 -0.0609 0.7433 0.0256
-3.500 -0.0830 0.00963 0.00308 -0.0613 0.7419 0.0274
-3.250 -0.0542 0.00944 0.00292 -0.0617 0.7406 0.0316
-3.000 -0.0254 0.00922 0.00275 -0.0621 0.7393 0.0429
-2.750 0.0033 0.00899 0.00259 -0.0626 0.7382 0.0607
-2.500 0.0321 0.00877 0.00245 -0.0631 0.7372 0.0836
-2.250 0.0609 0.00855 0.00232 -0.0636 0.7362 0.1116
-2.000 0.0899 0.00835 0.00223 -0.0641 0.7349 0.1401
-1.750 0.1189 0.00811 0.00215 -0.0647 0.7331 0.1818
-1.250 0.1768 0.00732 0.00193 -0.0662 0.7282 0.3432
-1.000 0.2063 0.00649 0.00173 -0.0675 0.7259 0.5325
-0.750 0.2368 0.00603 0.00160 -0.0685 0.7237 0.6362
-0.500 0.2664 0.00565 0.00165 -0.0691 0.7213 0.7544
-0.250 0.2959 0.00572 0.00180 -0.0695 0.7173 0.7913
0.000 0.3258 0.00574 0.00181 -0.0700 0.7128 0.8007
0.250 0.3555 0.00576 0.00182 -0.0705 0.7091 0.8086
0.500 0.3854 0.00580 0.00185 -0.0710 0.7050 0.8140
0.750 0.4149 0.00582 0.00187 -0.0715 0.6995 0.8169
1.000 0.4444 0.00582 0.00185 -0.0719 0.6930 0.8198
1.250 0.4739 0.00586 0.00186 -0.0724 0.6816 0.8238
1.500 0.5033 0.00591 0.00184 -0.0728 0.6649 0.8274
1.750 0.5312 0.00600 0.00185 -0.0730 0.6480 0.8296
2.000 0.5593 0.00613 0.00190 -0.0732 0.6346 0.8308
2.500 0.6162 0.00637 0.00205 -0.0740 0.6118 0.8325
2.750 0.6441 0.00654 0.00216 -0.0742 0.5934 0.8335
3.000 0.6721 0.00669 0.00226 -0.0745 0.5742 0.8346
3.250 0.6999 0.00687 0.00237 -0.0748 0.5533 0.8355
3.500 0.7273 0.00708 0.00250 -0.0750 0.5339 0.8366
3.750 0.7533 0.00740 0.00270 -0.0750 0.5056 0.8381
4.000 0.7765 0.00794 0.00300 -0.0746 0.4510 0.8396
4.250 0.7988 0.00856 0.00334 -0.0741 0.3948 0.8406
4.500 0.8220 0.00908 0.00365 -0.0738 0.3502 0.8415
4.750 0.8392 0.01002 0.00418 -0.0725 0.2686 0.8425
5.000 0.8522 0.01121 0.00489 -0.0707 0.1703 0.8436
5.250 0.8693 0.01206 0.00543 -0.0694 0.1062 0.8445
5.500 0.8891 0.01268 0.00587 -0.0686 0.0705 0.8454
5.750 0.9083 0.01331 0.00634 -0.0676 0.0386 0.8462
6.000 0.9304 0.01373 0.00672 -0.0671 0.0277 0.8469
6.250 0.9530 0.01410 0.00706 -0.0667 0.0234 0.8475
6.500 0.9756 0.01444 0.00740 -0.0662 0.0215 0.8481
6.750 0.9973 0.01480 0.00777 -0.0657 0.0196 0.8487
7.000 1.0169 0.01514 0.00813 -0.0647 0.0186 0.8495
7.250 1.0366 0.01553 0.00853 -0.0638 0.0170 0.8504
7.500 1.0563 0.01603 0.00903 -0.0631 0.0148 0.8512
7.750 1.0765 0.01653 0.00954 -0.0625 0.0111 0.8519
8.000 1.0939 0.01728 0.01026 -0.0618 0.0079 0.8526
8.250 1.1129 0.01801 0.01101 -0.0615 0.0070 0.8533
8.500 1.1318 0.01871 0.01173 -0.0610 0.0065 0.8540
8.750 1.1504 0.01939 0.01244 -0.0605 0.0063 0.8547
9.000 1.1684 0.02010 0.01318 -0.0599 0.0062 0.8553
9.250 1.1857 0.02084 0.01396 -0.0591 0.0060 0.8559
9.500 1.2026 0.02160 0.01475 -0.0584 0.0059 0.8565
10.000 1.2338 0.02323 0.01647 -0.0565 0.0056 0.8579
10.250 1.2487 0.02409 0.01738 -0.0555 0.0055 0.8587
10.500 1.2626 0.02502 0.01836 -0.0544 0.0054 0.8595
10.750 1.2759 0.02598 0.01937 -0.0533 0.0053 0.8603
11.000 1.2888 0.02698 0.02043 -0.0522 0.0052 0.8611
11.250 1.3004 0.02807 0.02157 -0.0509 0.0051 0.8620
11.500 1.3115 0.02921 0.02277 -0.0497 0.0050 0.8628
11.750 1.3218 0.03043 0.02404 -0.0484 0.0049 0.8636
12.000 1.3303 0.03179 0.02547 -0.0470 0.0048 0.8645
12.250 1.3380 0.03322 0.02698 -0.0455 0.0047 0.8653
12.500 1.3438 0.03483 0.02867 -0.0440 0.0047 0.8662
12.750 1.3518 0.03629 0.03020 -0.0427 0.0046 0.8671
13.000 1.3604 0.03772 0.03169 -0.0416 0.0046 0.8679
13.250 1.3689 0.03921 0.03325 -0.0405 0.0046 0.8687
13.500 1.3764 0.04085 0.03495 -0.0395 0.0045 0.8696
13.750 1.3840 0.04253 0.03671 -0.0386 0.0045 0.8704
14.000 1.3906 0.04435 0.03861 -0.0377 0.0044 0.8712
14.250 1.3971 0.04624 0.04058 -0.0368 0.0044 0.8719
14.500 1.4027 0.04827 0.04270 -0.0361 0.0044 0.8730
14.750 1.4075 0.05043 0.04495 -0.0354 0.0043 0.8740
15.000 1.4121 0.05264 0.04726 -0.0348 0.0043 0.8752
15.250 1.4162 0.05495 0.04966 -0.0342 0.0042 0.8764
15.500 1.4197 0.05739 0.05219 -0.0338 0.0041 0.8777
15.750 1.4226 0.05995 0.05486 -0.0335 0.0041 0.8791
16.000 1.4245 0.06268 0.05768 -0.0332 0.0040 0.8805
16.250 1.4254 0.06555 0.06066 -0.0330 0.0040 0.8819
16.500 1.4250 0.06864 0.06386 -0.0330 0.0039 0.8833
16.750 1.4237 0.07193 0.06725 -0.0330 0.0039 0.8847
17.000 1.4218 0.07537 0.07080 -0.0333 0.0039 0.8860
17.500 1.4146 0.08286 0.07852 -0.0341 0.0038 0.8891
17.750 1.4099 0.08686 0.08264 -0.0348 0.0038 0.8910
18.000 1.4039 0.09113 0.08703 -0.0356 0.0038 0.8930
18.250 1.3975 0.09557 0.09159 -0.0366 0.0037 0.8952
18.500 1.3900 0.10024 0.09638 -0.0379 0.0037 0.8974
18.750 1.3822 0.10504 0.10130 -0.0393 0.0037 0.8998
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