WORTMANN FX M2 AIRFOIL (fxm2-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: WORTMANN FX M2 AIRFOIL (fxm2-il) Reynolds number: 1,000,000 Max Cl/Cd: 100.47 at α=6.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fxm2-il-1000000-n5.txt Download as CSV file: xf-fxm2-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX M2 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
------ -------- --------- --------- -------- -------- --------
-9.250 -0.1965 0.09699 0.09275 -0.0475 0.3351 0.0059
-9.000 -0.1959 0.09245 0.08822 -0.0491 0.3280 0.0066
-8.750 -0.1892 0.08983 0.08555 -0.0500 0.3023 0.0065
-8.500 -0.1829 0.08731 0.08299 -0.0509 0.2912 0.0067
-8.250 -0.1757 0.08448 0.08029 -0.0520 0.3269 0.0067
-8.000 -0.1681 0.08262 0.07829 -0.0525 0.2861 0.0068
-7.750 -0.1669 0.07907 0.07477 -0.0536 0.2861 0.0067
-7.500 -0.1578 0.07740 0.07311 -0.0540 0.2847 0.0069
-7.250 -0.1538 0.07516 0.07089 -0.0543 0.2831 0.0069
-7.000 -0.1529 0.07242 0.06816 -0.0553 0.2798 0.0069
-6.750 -0.1436 0.06979 0.06554 -0.0574 0.2791 0.0070
-6.500 -0.1315 0.06732 0.06308 -0.0598 0.2778 0.0072
-6.250 -0.1185 0.06430 0.06006 -0.0629 0.2765 0.0073
-6.000 -0.1036 0.06093 0.05668 -0.0667 0.2751 0.0075
-5.750 -0.0862 0.05742 0.05315 -0.0707 0.2718 0.0077
-5.500 -0.0663 0.05310 0.04878 -0.0756 0.2695 0.0077
-5.000 -0.0129 0.03876 0.03411 -0.0900 0.2654 0.0092
-4.750 0.0130 0.03676 0.03198 -0.0916 0.2439 0.0094
-4.500 0.0402 0.03424 0.02929 -0.0934 0.2392 0.0097
-3.500 0.1655 0.01407 0.00717 -0.1015 0.2299 0.0152
-3.250 0.1933 0.01410 0.00715 -0.1013 0.2272 0.0154
-3.000 0.2210 0.01416 0.00717 -0.1010 0.2245 0.0156
-2.750 0.2490 0.01391 0.00684 -0.1009 0.2220 0.0160
-2.500 0.2775 0.01321 0.00601 -0.1008 0.2207 0.0166
-2.250 0.3062 0.01196 0.00453 -0.1009 0.2191 0.0179
-2.000 0.3345 0.01148 0.00394 -0.1007 0.2163 0.0184
-1.750 0.3626 0.01128 0.00368 -0.1006 0.2116 0.0190
-1.500 0.3907 0.01127 0.00366 -0.1003 0.2075 0.0194
-1.250 0.4184 0.01129 0.00357 -0.1001 0.1852 0.0200
-1.000 0.4464 0.01116 0.00336 -0.0999 0.1789 0.0208
-0.750 0.4744 0.01099 0.00311 -0.0997 0.1730 0.0215
-0.500 0.5025 0.01086 0.00292 -0.0995 0.1695 0.0221
-0.250 0.5308 0.01071 0.00273 -0.0994 0.1665 0.0227
0.000 0.5587 0.01070 0.00270 -0.0992 0.1622 0.0234
0.250 0.5865 0.01074 0.00271 -0.0989 0.1574 0.0242
0.500 0.6145 0.01072 0.00266 -0.0987 0.1541 0.0251
0.750 0.6426 0.01068 0.00260 -0.0986 0.1507 0.0260
1.000 0.6704 0.01071 0.00257 -0.0983 0.1440 0.0266
1.250 0.6969 0.01094 0.00260 -0.0980 0.1130 0.0274
1.500 0.7240 0.01109 0.00268 -0.0977 0.0987 0.0284
1.750 0.7510 0.01127 0.00280 -0.0974 0.0836 0.0297
2.000 0.7783 0.01140 0.00287 -0.0971 0.0769 0.0307
2.250 0.8059 0.01147 0.00293 -0.0969 0.0760 0.0316
2.500 0.8334 0.01156 0.00299 -0.0967 0.0746 0.0326
2.750 0.8609 0.01164 0.00307 -0.0964 0.0734 0.0342
3.000 0.8883 0.01175 0.00317 -0.0962 0.0724 0.0362
3.250 0.9156 0.01187 0.00327 -0.0959 0.0716 0.0377
3.500 0.9429 0.01199 0.00338 -0.0957 0.0707 0.0399
3.750 0.9701 0.01212 0.00351 -0.0954 0.0698 0.0436
4.000 0.9974 0.01222 0.00367 -0.0952 0.0690 0.0854
4.250 1.0253 0.01221 0.00388 -0.0952 0.0683 0.2483
4.500 1.0526 0.01230 0.00405 -0.0951 0.0676 0.3049
4.750 1.0800 0.01237 0.00423 -0.0950 0.0672 0.3716
5.000 1.1080 0.01231 0.00445 -0.0951 0.0669 0.5137
5.250 1.1363 0.01215 0.00471 -0.0954 0.0666 0.7062
5.500 1.1547 0.01175 0.00488 -0.0932 0.0662 1.0000
5.750 1.1814 0.01195 0.00506 -0.0929 0.0656 1.0000
6.000 1.2080 0.01215 0.00526 -0.0926 0.0650 1.0000
6.250 1.2345 0.01236 0.00547 -0.0923 0.0642 1.0000
6.500 1.2608 0.01258 0.00568 -0.0920 0.0632 1.0000
6.750 1.2870 0.01281 0.00590 -0.0916 0.0617 1.0000
7.000 1.3128 0.01309 0.00615 -0.0913 0.0596 1.0000
7.250 1.3387 0.01334 0.00640 -0.0909 0.0579 1.0000
7.500 1.3639 0.01366 0.00670 -0.0905 0.0499 1.0000
7.750 1.3886 0.01406 0.00704 -0.0900 0.0461 1.0000
8.000 1.4138 0.01436 0.00733 -0.0896 0.0457 1.0000
8.250 1.4389 0.01466 0.00764 -0.0892 0.0454 1.0000
8.500 1.4638 0.01497 0.00796 -0.0887 0.0450 1.0000
8.750 1.4884 0.01531 0.00830 -0.0882 0.0444 1.0000
9.000 1.5125 0.01570 0.00870 -0.0877 0.0433 1.0000
9.250 1.5366 0.01607 0.00909 -0.0872 0.0424 1.0000
9.500 1.5606 0.01642 0.00946 -0.0866 0.0419 1.0000
9.750 1.5845 0.01677 0.00984 -0.0861 0.0417 1.0000
10.000 1.6082 0.01714 0.01023 -0.0855 0.0415 1.0000
10.250 1.6316 0.01751 0.01064 -0.0849 0.0413 1.0000
10.500 1.6546 0.01790 0.01106 -0.0843 0.0411 1.0000
10.750 1.6774 0.01830 0.01150 -0.0836 0.0409 1.0000
11.000 1.6998 0.01872 0.01196 -0.0829 0.0408 1.0000
11.250 1.7219 0.01914 0.01243 -0.0821 0.0407 1.0000
11.500 1.7436 0.01958 0.01291 -0.0814 0.0406 1.0000
11.750 1.7648 0.02004 0.01343 -0.0805 0.0405 1.0000
12.000 1.7855 0.02052 0.01396 -0.0796 0.0404 1.0000
12.250 1.8056 0.02101 0.01451 -0.0786 0.0403 1.0000
12.500 1.8251 0.02153 0.01508 -0.0776 0.0402 1.0000
12.750 1.8439 0.02207 0.01569 -0.0765 0.0401 1.0000
13.000 1.8618 0.02263 0.01632 -0.0752 0.0400 1.0000
13.250 1.8786 0.02323 0.01699 -0.0738 0.0397 1.0000
13.500 1.8928 0.02388 0.01772 -0.0720 0.0392 1.0000
13.750 1.9033 0.02460 0.01852 -0.0697 0.0387 1.0000
14.000 1.9120 0.02540 0.01940 -0.0671 0.0382 1.0000
14.250 1.9202 0.02628 0.02035 -0.0647 0.0379 1.0000
14.500 1.9268 0.02730 0.02145 -0.0623 0.0375 1.0000
14.750 1.9310 0.02852 0.02277 -0.0598 0.0369 1.0000
15.000 1.9332 0.02998 0.02431 -0.0574 0.0363 1.0000
15.250 1.9339 0.03164 0.02608 -0.0553 0.0358 1.0000
15.500 1.9325 0.03362 0.02816 -0.0534 0.0352 1.0000
15.750 1.9395 0.03502 0.02964 -0.0522 0.0349 1.0000
16.000 1.9446 0.03668 0.03140 -0.0513 0.0345 1.0000
16.250 1.9468 0.03875 0.03357 -0.0505 0.0341 1.0000
16.500 1.9471 0.04121 0.03615 -0.0502 0.0337 1.0000
16.750 1.9454 0.04410 0.03915 -0.0502 0.0332 1.0000
17.000 1.9411 0.04757 0.04274 -0.0508 0.0324 1.0000
17.250 1.9340 0.05172 0.04702 -0.0519 0.0314 1.0000
17.500 1.9224 0.05679 0.05222 -0.0538 0.0298 1.0000
17.750 1.9043 0.06317 0.05876 -0.0564 0.0287 1.0000
18.000 1.8795 0.07095 0.06671 -0.0600 0.0284 1.0000
18.250 1.8466 0.08044 0.07639 -0.0646 0.0285 1.0000
18.500 1.8058 0.09162 0.08779 -0.0703 0.0295 1.0000
18.750 1.7606 0.10401 0.10039 -0.0768 0.0305 1.0000
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