SG6040 (sg6040-il) Xfoil prediction polar at RE=50,000 Ncrit=5
| Details | Polar file |
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Airfoil: SG6040 (sg6040-il) Reynolds number: 50,000 Max Cl/Cd: 26.38 at α=8.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-sg6040-il-50000-n5.txt Download as CSV file: xf-sg6040-il-50000-n5.csv |
XFOIL Version 6.96
Calculated polar for: SG6040
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.050 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-12.250 -0.4551 0.10131 0.09364 -0.0627 1.0000 0.0541
-12.000 -0.4769 0.09325 0.08563 -0.0664 1.0000 0.0539
-11.750 -0.5056 0.08515 0.07753 -0.0704 1.0000 0.0536
-11.500 -0.5328 0.07865 0.07100 -0.0730 1.0000 0.0531
-11.250 -0.5620 0.07301 0.06532 -0.0746 1.0000 0.0526
-11.000 -0.5921 0.06834 0.06057 -0.0749 1.0000 0.0524
-10.750 -0.6198 0.06476 0.05691 -0.0738 1.0000 0.0522
-10.500 -0.6470 0.06202 0.05409 -0.0712 1.0000 0.0521
-10.250 -0.6759 0.05993 0.05194 -0.0673 1.0000 0.0521
-10.000 -0.7013 0.05796 0.04987 -0.0629 1.0000 0.0522
-9.750 -0.7209 0.05576 0.04749 -0.0591 1.0000 0.0526
-9.500 -0.7364 0.05345 0.04493 -0.0554 1.0000 0.0532
-9.250 -0.7473 0.05107 0.04222 -0.0521 1.0000 0.0540
-9.000 -0.7470 0.04950 0.04063 -0.0495 1.0000 0.0551
-8.750 -0.7451 0.04799 0.03904 -0.0470 1.0000 0.0564
-8.500 -0.7419 0.04629 0.03719 -0.0447 1.0000 0.0579
-8.250 -0.7342 0.04440 0.03504 -0.0428 0.9994 0.0598
-8.000 -0.7065 0.04219 0.03248 -0.0443 0.9938 0.0637
-7.750 -0.6795 0.04077 0.03099 -0.0457 0.9875 0.0686
-7.500 -0.6505 0.03922 0.02928 -0.0470 0.9821 0.0753
-7.250 -0.6236 0.03788 0.02772 -0.0477 0.9755 0.0844
-7.000 -0.5948 0.03670 0.02645 -0.0491 0.9697 0.0964
-6.750 -0.5710 0.03560 0.02537 -0.0496 0.9623 0.1111
-6.500 -0.5430 0.03453 0.02436 -0.0510 0.9563 0.1294
-6.250 -0.5209 0.03357 0.02340 -0.0511 0.9485 0.1486
-6.000 -0.4903 0.03263 0.02241 -0.0527 0.9428 0.1724
-5.750 -0.4708 0.03175 0.02163 -0.0522 0.9343 0.1931
-5.500 -0.4412 0.03082 0.02074 -0.0536 0.9285 0.2213
-5.250 -0.4222 0.02992 0.02001 -0.0530 0.9201 0.2489
-5.000 -0.3948 0.02891 0.01926 -0.0540 0.9138 0.2929
-4.750 -0.3757 0.02810 0.01887 -0.0533 0.9058 0.3531
-4.500 -0.3513 0.02793 0.01923 -0.0522 0.8989 0.4376
-4.250 -0.3271 0.02831 0.01974 -0.0507 0.8915 0.5049
-4.000 -0.3021 0.02866 0.01993 -0.0499 0.8836 0.5526
-3.750 -0.2702 0.02906 0.02013 -0.0500 0.8779 0.5899
-3.500 -0.2526 0.02951 0.02049 -0.0475 0.8684 0.6136
-3.250 -0.2208 0.02984 0.02063 -0.0476 0.8629 0.6413
-3.000 -0.2046 0.03025 0.02095 -0.0448 0.8535 0.6604
-2.750 -0.1766 0.03064 0.02125 -0.0436 0.8475 0.6809
-2.500 -0.1576 0.03097 0.02148 -0.0413 0.8393 0.6993
-2.250 -0.1337 0.03119 0.02160 -0.0398 0.8322 0.7172
-2.000 -0.1001 0.03125 0.02152 -0.0399 0.8279 0.7337
-1.750 -0.0893 0.03136 0.02155 -0.0371 0.8170 0.7474
-1.500 -0.0561 0.03129 0.02135 -0.0375 0.8122 0.7591
-1.250 -0.0416 0.03138 0.02136 -0.0354 0.8023 0.7690
-1.000 -0.0103 0.03118 0.02101 -0.0362 0.7965 0.7798
-0.750 0.0098 0.03122 0.02099 -0.0349 0.7882 0.7874
-0.500 0.0363 0.03108 0.02073 -0.0351 0.7810 0.7967
-0.250 0.0744 0.03085 0.02040 -0.0366 0.7770 0.8033
0.000 0.0836 0.03102 0.02053 -0.0342 0.7656 0.8121
0.250 0.1201 0.03079 0.02021 -0.0356 0.7610 0.8187
0.500 0.1321 0.03099 0.02037 -0.0336 0.7504 0.8268
0.750 0.1660 0.03080 0.02012 -0.0347 0.7452 0.8338
1.000 0.1818 0.03099 0.02028 -0.0332 0.7356 0.8415
1.250 0.2123 0.03088 0.02013 -0.0339 0.7294 0.8491
1.500 0.2351 0.03097 0.02020 -0.0334 0.7216 0.8566
1.750 0.2591 0.03102 0.02024 -0.0332 0.7137 0.8650
2.000 0.2991 0.03075 0.01994 -0.0349 0.7097 0.8719
2.250 0.3072 0.03123 0.02045 -0.0327 0.6981 0.8821
2.500 0.3469 0.03096 0.02018 -0.0344 0.6937 0.8897
2.750 0.3588 0.03150 0.02077 -0.0328 0.6827 0.9009
3.000 0.3981 0.03127 0.02055 -0.0347 0.6778 0.9102
3.250 0.4178 0.03181 0.02116 -0.0344 0.6676 0.9223
3.500 0.4592 0.03168 0.02107 -0.0368 0.6619 0.9326
3.750 0.4888 0.03211 0.02157 -0.0382 0.6528 0.9466
4.000 0.5314 0.03214 0.02167 -0.0412 0.6461 0.9600
4.500 0.5936 0.03262 0.02227 -0.0444 0.6296 1.0000
5.000 0.6356 0.03335 0.02302 -0.0440 0.6129 1.0000
5.250 0.6814 0.03289 0.02259 -0.0465 0.6089 1.0000
5.500 0.6831 0.03421 0.02394 -0.0442 0.5962 1.0000
6.000 0.7314 0.03509 0.02490 -0.0443 0.5793 1.0000
6.500 0.7808 0.03585 0.02578 -0.0441 0.5619 1.0000
6.750 0.7925 0.03688 0.02688 -0.0427 0.5507 1.0000
7.000 0.8342 0.03622 0.02631 -0.0438 0.5440 1.0000
7.250 0.8406 0.03745 0.02761 -0.0419 0.5314 1.0000
7.500 0.8763 0.03699 0.02723 -0.0423 0.5229 1.0000
7.750 0.8981 0.03724 0.02758 -0.0414 0.5116 1.0000
8.000 0.9083 0.03815 0.02857 -0.0397 0.4987 1.0000
8.250 0.9327 0.03816 0.02866 -0.0389 0.4871 1.0000
8.500 0.9754 0.03697 0.02756 -0.0394 0.4762 1.0000
8.750 0.9824 0.03790 0.02858 -0.0372 0.4616 1.0000
9.000 0.9934 0.03859 0.02936 -0.0353 0.4468 1.0000
9.250 1.0063 0.03916 0.03002 -0.0336 0.4316 1.0000
9.500 1.0195 0.03968 0.03061 -0.0320 0.4156 1.0000
9.750 1.0318 0.04027 0.03126 -0.0303 0.3989 1.0000
10.000 1.0438 0.04090 0.03194 -0.0286 0.3813 1.0000
10.250 1.0559 0.04152 0.03260 -0.0270 0.3629 1.0000
10.500 1.0613 0.04274 0.03386 -0.0253 0.3433 1.0000
10.750 1.0636 0.04434 0.03549 -0.0236 0.3228 1.0000
11.000 1.0692 0.04567 0.03680 -0.0221 0.3015 1.0000
11.250 1.0742 0.04715 0.03820 -0.0207 0.2802 1.0000
11.500 1.0747 0.04924 0.04027 -0.0195 0.2591 1.0000
11.750 1.0762 0.05130 0.04226 -0.0184 0.2392 1.0000
12.000 1.0772 0.05349 0.04434 -0.0174 0.2212 1.0000
12.250 1.0780 0.05586 0.04661 -0.0167 0.2050 1.0000
12.500 1.0782 0.05844 0.04912 -0.0161 0.1902 1.0000
12.750 1.0788 0.06112 0.05179 -0.0156 0.1768 1.0000
13.000 1.0800 0.06385 0.05451 -0.0153 0.1648 1.0000
13.250 1.0822 0.06652 0.05718 -0.0151 0.1544 1.0000
13.500 1.0864 0.06894 0.05951 -0.0148 0.1453 1.0000
13.750 1.0879 0.07197 0.06268 -0.0148 0.1363 1.0000
14.000 1.0932 0.07443 0.06510 -0.0147 0.1290 1.0000
14.250 1.0958 0.07747 0.06830 -0.0149 0.1220 1.0000
14.500 1.1035 0.07969 0.07045 -0.0148 0.1161 1.0000
14.750 1.1032 0.08334 0.07435 -0.0153 0.1107 1.0000
15.000 1.1102 0.08576 0.07680 -0.0154 0.1057 1.0000
15.250 1.1131 0.08902 0.08019 -0.0159 0.1015 1.0000
15.500 1.1091 0.09338 0.08481 -0.0171 0.0978 1.0000
15.750 1.1108 0.09676 0.08829 -0.0179 0.0943 1.0000
16.000 1.1220 0.09875 0.09025 -0.0178 0.0909 1.0000
16.250 1.1051 0.10546 0.09731 -0.0206 0.0890 1.0000
16.500 1.0849 0.11305 0.10520 -0.0241 0.0873 1.0000
16.750 1.0576 0.12243 0.11486 -0.0291 0.0861 1.0000
17.000 1.0066 0.13805 0.13075 -0.0381 0.0856 1.0000
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