WORTMANN FX 62-K-131 AIRFOIL (fx62k131-il) Xfoil prediction polar at RE=100,000 Ncrit=0
| Details | Polar file |
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Airfoil: WORTMANN FX 62-K-131 AIRFOIL (fx62k131-il) Reynolds number: 100,000 Max Cl/Cd: 56.41 at α=8.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx62k131-il-100000.txt Download as CSV file: xf-fx62k131-il-100000.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 62-K-131 AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.100 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-11.500 -0.3349 0.13907 0.13433 -0.0461 1.0001 0.0612
-11.250 -0.3490 0.13848 0.13383 -0.0439 1.0001 0.0623
-11.000 -0.3649 0.13800 0.13344 -0.0423 1.0001 0.0630
-10.750 -0.3806 0.13735 0.13288 -0.0413 1.0001 0.0635
-10.500 -0.3960 0.13643 0.13204 -0.0408 1.0001 0.0638
-10.250 -0.4104 0.13520 0.13089 -0.0405 1.0001 0.0640
-10.000 -0.4034 0.13004 0.12577 -0.0379 1.0001 0.0652
-9.750 -0.3920 0.12692 0.12263 -0.0344 1.0001 0.0678
-9.500 -0.3954 0.12484 0.12059 -0.0329 1.0001 0.0698
-9.250 -0.4014 0.12275 0.11855 -0.0319 1.0001 0.0718
-9.000 -0.4097 0.12066 0.11651 -0.0313 1.0001 0.0739
-8.750 -0.4224 0.11868 0.11460 -0.0313 1.0001 0.0757
-8.500 -0.4403 0.11692 0.11292 -0.0319 1.0001 0.0767
-8.250 -0.4601 0.11510 0.11119 -0.0325 1.0001 0.0772
-8.000 -0.4805 0.11315 0.10932 -0.0326 1.0001 0.0774
-7.750 -0.4667 0.10801 0.10420 -0.0308 0.9992 0.0796
-7.500 -0.4470 0.10473 0.10088 -0.0305 0.9968 0.0842
-7.250 -0.4488 0.10131 0.09750 -0.0334 0.9932 0.0875
-7.000 -0.4634 0.09811 0.09435 -0.0367 0.9887 0.0896
-6.750 -0.4791 0.09207 0.08826 -0.0495 0.9833 0.0910
-6.500 -0.4849 0.08637 0.08243 -0.0559 0.9788 0.0926
-6.250 -0.4600 0.08440 0.08066 -0.0495 0.9766 0.0981
-6.000 -0.4646 0.07879 0.07440 -0.0657 0.9706 0.1059
-5.750 -0.4497 0.07460 0.07065 -0.0600 0.9681 0.1097
-5.500 -0.4332 0.06949 0.06525 -0.0676 0.9638 0.1217
-5.250 -0.4106 0.06544 0.06105 -0.0720 0.9600 0.1359
-5.000 -0.3943 0.06207 0.05761 -0.0738 0.9556 0.1504
-4.750 -0.3712 0.05894 0.05449 -0.0755 0.9518 0.1680
-4.500 -0.3368 0.05556 0.05096 -0.0808 0.9483 0.2082
-4.000 -0.1942 0.04109 0.03381 -0.0992 0.9419 0.0743
-3.750 -0.1435 0.03802 0.02996 -0.1026 0.9387 0.0621
-3.500 -0.0944 0.03528 0.02682 -0.1062 0.9361 0.0578
-3.250 -0.0585 0.03374 0.02500 -0.1073 0.9323 0.0571
-3.000 -0.0292 0.03273 0.02387 -0.1075 0.9276 0.0595
-2.750 0.0100 0.03165 0.02276 -0.1097 0.9241 0.0676
-2.500 0.0620 0.03058 0.02175 -0.1143 0.9215 0.0815
-2.250 0.0998 0.02884 0.02288 -0.1153 0.9185 0.7049
-2.000 0.0900 0.03028 0.02430 -0.1055 0.9111 0.7539
-1.750 0.0843 0.03142 0.02538 -0.0964 0.9048 0.7909
-1.500 0.0679 0.03208 0.02607 -0.0855 0.8973 0.8243
-1.250 0.0512 0.03238 0.02637 -0.0743 0.8907 0.8617
-1.000 0.0361 0.03222 0.02620 -0.0645 0.8834 0.8959
-0.750 0.0326 0.03183 0.02572 -0.0573 0.8771 0.9261
-0.500 0.0446 0.03161 0.02532 -0.0549 0.8698 0.9405
-0.250 0.0812 0.03165 0.02511 -0.0568 0.8654 0.9514
0.000 0.0928 0.03160 0.02495 -0.0552 0.8566 0.9623
0.250 0.1341 0.03168 0.02482 -0.0582 0.8520 0.9716
0.500 0.1564 0.03185 0.02487 -0.0588 0.8433 0.9817
0.750 0.2056 0.03208 0.02493 -0.0635 0.8385 0.9895
1.000 0.2276 0.03233 0.02512 -0.0642 0.8289 0.9998
1.250 0.2708 0.03264 0.02528 -0.0677 0.8242 0.9999
1.500 0.2887 0.03318 0.02577 -0.0679 0.8145 0.9999
1.750 0.3347 0.03346 0.02596 -0.0717 0.8101 0.9999
2.000 0.3551 0.03408 0.02655 -0.0722 0.8001 0.9999
2.250 0.4029 0.03428 0.02668 -0.0761 0.7960 0.9999
2.500 0.4240 0.03496 0.02736 -0.0768 0.7856 0.9999
2.750 0.4728 0.03503 0.02740 -0.0806 0.7818 0.9999
3.000 0.4941 0.03574 0.02813 -0.0812 0.7710 0.9999
3.250 0.5434 0.03566 0.02805 -0.0848 0.7675 0.9999
3.500 0.5645 0.03642 0.02884 -0.0854 0.7564 0.9999
3.750 0.5916 0.03706 0.02952 -0.0867 0.7470 0.9999
4.000 0.6345 0.03699 0.02953 -0.0893 0.7419 0.9999
4.250 0.6595 0.03771 0.03030 -0.0903 0.7316 0.9999
4.500 0.7058 0.03736 0.03004 -0.0931 0.7275 0.9999
4.750 0.7298 0.03808 0.03087 -0.0938 0.7165 0.9999
5.000 0.7783 0.03740 0.03030 -0.0966 0.7131 0.9999
5.250 0.8015 0.03808 0.03110 -0.0971 0.7016 0.9999
5.500 0.8526 0.03703 0.03023 -0.0998 0.6989 0.9999
5.750 0.8762 0.03762 0.03096 -0.1002 0.6870 0.9999
6.000 0.9281 0.03616 0.02968 -0.1025 0.6845 0.9999
6.500 1.0109 0.03388 0.02784 -0.1048 0.6706 0.9999
6.750 1.0486 0.03242 0.02660 -0.1050 0.6592 0.9999
7.000 1.0944 0.03007 0.02448 -0.1056 0.6481 0.9999
7.250 1.1461 0.02751 0.02222 -0.1069 0.6370 0.9999
7.500 1.1937 0.02538 0.02034 -0.1080 0.6214 0.9999
7.750 1.2333 0.02362 0.01876 -0.1079 0.5959 0.9999
8.000 1.2633 0.02256 0.01774 -0.1068 0.5576 0.9999
8.250 1.2799 0.02269 0.01784 -0.1046 0.5116 0.9999
8.500 1.2897 0.02341 0.01845 -0.1019 0.4587 0.9999
8.750 1.2913 0.02478 0.01964 -0.0984 0.3926 0.9999
9.000 1.2810 0.02716 0.02149 -0.0941 0.3085 0.9999
9.250 1.2635 0.03051 0.02416 -0.0899 0.2157 0.9999
9.500 1.2453 0.03438 0.02732 -0.0862 0.1453 0.9999
9.750 1.2328 0.03806 0.03052 -0.0832 0.1029 0.9999
10.000 1.2273 0.04132 0.03353 -0.0811 0.0703 0.9999
10.250 1.2208 0.04472 0.03682 -0.0786 0.0540 0.9999
10.500 1.2208 0.04772 0.03982 -0.0763 0.0441 0.9999
10.750 1.2304 0.05027 0.04237 -0.0741 0.0379 0.9999
11.000 1.2433 0.05245 0.04459 -0.0731 0.0328 0.9999
11.250 1.2734 0.05485 0.04703 -0.0719 0.0292 0.9999
11.500 1.3047 0.05758 0.05009 -0.0711 0.0279 0.9999
11.750 1.3263 0.06118 0.05409 -0.0702 0.0274 0.9999
12.000 1.3349 0.06522 0.05855 -0.0688 0.0273 0.9999
12.250 1.3348 0.06946 0.06319 -0.0673 0.0275 0.9999
12.500 1.3282 0.07396 0.06806 -0.0658 0.0277 0.9999
12.750 1.3177 0.07862 0.07306 -0.0645 0.0280 0.9999
13.000 1.3045 0.08346 0.07821 -0.0636 0.0283 0.9999
13.250 1.2890 0.08853 0.08357 -0.0631 0.0286 0.9999
13.500 1.2723 0.09382 0.08913 -0.0633 0.0289 0.9999
13.750 1.2540 0.09954 0.09510 -0.0640 0.0292 0.9999
14.000 1.2358 0.10546 0.10123 -0.0654 0.0295 0.9999
14.250 1.2176 0.11191 0.10788 -0.0675 0.0298 0.9999
14.750 0.9663 0.10201 0.09834 -0.0419 0.0298 0.9999
15.000 0.9436 0.10774 0.10425 -0.0447 0.0300 0.9999
15.250 0.9231 0.11357 0.11021 -0.0476 0.0304 0.9999
15.500 0.9022 0.11946 0.11632 -0.0516 0.0307 0.9999
15.750 0.8682 0.12847 0.12558 -0.0584 0.0317 0.9999
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