SG6040 (sg6040-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: SG6040 (sg6040-il) Reynolds number: 500,000 Max Cl/Cd: 88.47 at α=5.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-sg6040-il-500000-n5.txt Download as CSV file: xf-sg6040-il-500000-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 = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-17.750 -0.6806 0.12192 0.11874 -0.0504 1.0000 0.0105
-17.500 -0.7116 0.11150 0.10816 -0.0558 1.0000 0.0105
-17.250 -0.7387 0.10229 0.09880 -0.0605 1.0000 0.0104
-17.000 -0.7605 0.09441 0.09078 -0.0646 1.0000 0.0104
-16.750 -0.7787 0.08737 0.08361 -0.0683 1.0000 0.0104
-16.500 -0.7952 0.08088 0.07699 -0.0717 1.0000 0.0104
-16.250 -0.8093 0.07498 0.07096 -0.0747 1.0000 0.0104
-16.000 -0.8223 0.06951 0.06537 -0.0775 1.0000 0.0105
-15.750 -0.8328 0.06469 0.06043 -0.0797 1.0000 0.0105
-15.500 -0.8424 0.06027 0.05590 -0.0816 1.0000 0.0105
-15.250 -0.8494 0.05646 0.05198 -0.0830 1.0000 0.0106
-15.000 -0.8569 0.05287 0.04828 -0.0840 1.0000 0.0106
-14.750 -0.8625 0.04976 0.04507 -0.0846 1.0000 0.0107
-14.500 -0.8686 0.04681 0.04203 -0.0848 1.0000 0.0107
-14.250 -0.8725 0.04425 0.03937 -0.0847 1.0000 0.0108
-14.000 -0.8760 0.04190 0.03692 -0.0842 1.0000 0.0109
-13.750 -0.8800 0.03965 0.03459 -0.0835 1.0000 0.0109
-13.500 -0.8831 0.03765 0.03252 -0.0824 1.0000 0.0110
-13.250 -0.8859 0.03584 0.03063 -0.0810 1.0000 0.0111
-13.000 -0.8895 0.03416 0.02887 -0.0793 1.0000 0.0111
-12.750 -0.8710 0.03221 0.02681 -0.0817 0.9978 0.0112
-12.500 -0.8516 0.03041 0.02492 -0.0840 0.9948 0.0114
-12.250 -0.8332 0.02875 0.02317 -0.0858 0.9913 0.0114
-12.000 -0.8130 0.02728 0.02159 -0.0875 0.9873 0.0116
-11.750 -0.7919 0.02569 0.01992 -0.0897 0.9838 0.0118
-11.500 -0.7759 0.02427 0.01844 -0.0905 0.9772 0.0120
-11.250 -0.7544 0.02294 0.01705 -0.0921 0.9721 0.0122
-11.000 -0.7377 0.02191 0.01597 -0.0922 0.9634 0.0125
-10.750 -0.7139 0.02085 0.01485 -0.0935 0.9576 0.0128
-10.500 -0.6945 0.02000 0.01394 -0.0935 0.9478 0.0130
-10.250 -0.6657 0.01910 0.01296 -0.0951 0.9423 0.0133
-10.000 -0.6403 0.01833 0.01212 -0.0959 0.9335 0.0137
-9.750 -0.6100 0.01757 0.01128 -0.0975 0.9269 0.0140
-9.500 -0.5832 0.01693 0.01057 -0.0982 0.9176 0.0142
-9.250 -0.5563 0.01629 0.00985 -0.0989 0.9086 0.0146
-9.000 -0.5322 0.01569 0.00917 -0.0990 0.8983 0.0151
-8.750 -0.5090 0.01521 0.00863 -0.0987 0.8882 0.0155
-8.250 -0.4629 0.01441 0.00767 -0.0978 0.8691 0.0169
-8.000 -0.4394 0.01406 0.00724 -0.0974 0.8606 0.0176
-7.750 -0.4173 0.01367 0.00682 -0.0966 0.8514 0.0188
-7.500 -0.3938 0.01334 0.00643 -0.0961 0.8435 0.0208
-7.250 -0.3713 0.01298 0.00605 -0.0955 0.8349 0.0242
-7.000 -0.3481 0.01262 0.00567 -0.0949 0.8274 0.0304
-6.750 -0.3257 0.01221 0.00531 -0.0942 0.8194 0.0415
-6.500 -0.3021 0.01188 0.00500 -0.0938 0.8120 0.0556
-6.250 -0.2777 0.01160 0.00475 -0.0934 0.8046 0.0675
-6.000 -0.2527 0.01137 0.00452 -0.0930 0.7972 0.0763
-5.750 -0.2271 0.01118 0.00430 -0.0928 0.7904 0.0848
-5.500 -0.2018 0.01095 0.00408 -0.0925 0.7831 0.0954
-5.250 -0.1764 0.01073 0.00387 -0.0922 0.7764 0.1083
-5.000 -0.1510 0.01049 0.00367 -0.0919 0.7692 0.1239
-4.750 -0.1258 0.01023 0.00347 -0.0917 0.7621 0.1449
-4.500 -0.1005 0.00993 0.00326 -0.0914 0.7552 0.1739
-4.250 -0.0754 0.00962 0.00306 -0.0912 0.7476 0.2088
-4.000 -0.0500 0.00932 0.00286 -0.0910 0.7407 0.2467
-3.750 -0.0246 0.00900 0.00267 -0.0908 0.7328 0.2913
-3.500 0.0005 0.00866 0.00248 -0.0906 0.7255 0.3451
-3.250 0.0262 0.00834 0.00233 -0.0905 0.7178 0.3999
-3.000 0.0521 0.00811 0.00223 -0.0902 0.7101 0.4504
-2.750 0.0790 0.00798 0.00219 -0.0901 0.7025 0.4909
-2.500 0.1062 0.00795 0.00218 -0.0900 0.6948 0.5170
-2.250 0.1339 0.00795 0.00216 -0.0900 0.6874 0.5328
-2.000 0.1615 0.00796 0.00215 -0.0899 0.6795 0.5463
-1.750 0.1893 0.00799 0.00213 -0.0898 0.6722 0.5575
-1.500 0.2170 0.00803 0.00214 -0.0898 0.6642 0.5703
-1.250 0.2444 0.00807 0.00217 -0.0896 0.6568 0.5824
-1.000 0.2720 0.00810 0.00218 -0.0896 0.6487 0.5925
-0.750 0.2994 0.00817 0.00221 -0.0894 0.6413 0.6011
-0.500 0.3271 0.00821 0.00222 -0.0894 0.6332 0.6085
-0.250 0.3541 0.00827 0.00225 -0.0892 0.6254 0.6145
0.000 0.3820 0.00831 0.00227 -0.0892 0.6175 0.6198
0.500 0.4365 0.00842 0.00231 -0.0890 0.6010 0.6266
0.750 0.4633 0.00849 0.00235 -0.0888 0.5928 0.6300
1.000 0.4908 0.00854 0.00239 -0.0887 0.5849 0.6334
1.250 0.5176 0.00862 0.00243 -0.0885 0.5769 0.6369
1.500 0.5451 0.00869 0.00247 -0.0884 0.5694 0.6401
1.750 0.5717 0.00877 0.00253 -0.0882 0.5612 0.6430
2.000 0.5986 0.00883 0.00260 -0.0881 0.5537 0.6461
2.250 0.6252 0.00891 0.00267 -0.0879 0.5457 0.6492
2.500 0.6519 0.00900 0.00275 -0.0877 0.5382 0.6526
2.750 0.6784 0.00910 0.00283 -0.0874 0.5298 0.6562
3.000 0.7048 0.00920 0.00292 -0.0872 0.5222 0.6593
3.250 0.7309 0.00929 0.00302 -0.0869 0.5138 0.6623
3.500 0.7566 0.00940 0.00313 -0.0865 0.5055 0.6658
3.750 0.7818 0.00952 0.00324 -0.0861 0.4949 0.6697
4.000 0.8068 0.00966 0.00337 -0.0856 0.4829 0.6736
4.250 0.8312 0.00982 0.00349 -0.0850 0.4704 0.6770
4.500 0.8548 0.00999 0.00364 -0.0842 0.4579 0.6806
4.750 0.8786 0.01015 0.00380 -0.0835 0.4450 0.6849
5.000 0.9018 0.01035 0.00397 -0.0827 0.4301 0.6895
5.500 0.9475 0.01074 0.00433 -0.0810 0.4035 0.6982
5.750 0.9696 0.01096 0.00454 -0.0800 0.3906 0.7030
6.000 0.9907 0.01121 0.00476 -0.0789 0.3752 0.7081
6.250 1.0106 0.01149 0.00500 -0.0775 0.3570 0.7133
6.500 1.0277 0.01180 0.00527 -0.0756 0.3358 0.7194
6.750 1.0437 0.01216 0.00555 -0.0735 0.3153 0.7259
7.000 1.0591 0.01256 0.00589 -0.0714 0.2937 0.7320
7.250 1.0743 0.01299 0.00627 -0.0693 0.2715 0.7390
7.750 1.1001 0.01410 0.00720 -0.0645 0.2214 0.7542
8.000 1.1118 0.01473 0.00773 -0.0621 0.1966 0.7630
8.250 1.1235 0.01534 0.00830 -0.0596 0.1764 0.7725
8.500 1.1354 0.01596 0.00888 -0.0573 0.1590 0.7834
8.750 1.1469 0.01660 0.00949 -0.0550 0.1422 0.7963
9.000 1.1583 0.01723 0.01012 -0.0526 0.1285 0.8111
9.250 1.1690 0.01789 0.01079 -0.0503 0.1159 0.8287
9.500 1.1793 0.01853 0.01148 -0.0479 0.1051 0.8514
9.750 1.1882 0.01910 0.01215 -0.0452 0.0964 0.8901
10.500 1.2276 0.02150 0.01459 -0.0410 0.0733 1.0000
10.750 1.2386 0.02246 0.01553 -0.0394 0.0673 1.0000
11.000 1.2498 0.02343 0.01650 -0.0380 0.0620 1.0000
11.250 1.2605 0.02446 0.01754 -0.0365 0.0577 1.0000
11.500 1.2711 0.02553 0.01863 -0.0352 0.0537 1.0000
11.750 1.2807 0.02671 0.01982 -0.0338 0.0505 1.0000
12.000 1.2913 0.02784 0.02099 -0.0326 0.0476 1.0000
12.250 1.3001 0.02915 0.02231 -0.0314 0.0450 1.0000
12.500 1.3087 0.03050 0.02370 -0.0302 0.0426 1.0000
12.750 1.3181 0.03184 0.02509 -0.0292 0.0408 1.0000
13.000 1.3259 0.03333 0.02662 -0.0282 0.0388 1.0000
13.250 1.3322 0.03500 0.02832 -0.0272 0.0371 1.0000
13.500 1.3405 0.03656 0.02994 -0.0264 0.0359 1.0000
13.750 1.3480 0.03823 0.03167 -0.0257 0.0347 1.0000
14.000 1.3543 0.04005 0.03355 -0.0250 0.0334 1.0000
14.250 1.3593 0.04205 0.03560 -0.0244 0.0322 1.0000
14.500 1.3632 0.04422 0.03781 -0.0238 0.0312 1.0000
14.750 1.3696 0.04620 0.03988 -0.0235 0.0303 1.0000
15.000 1.3750 0.04833 0.04208 -0.0232 0.0293 1.0000
15.250 1.3794 0.05063 0.04445 -0.0230 0.0285 1.0000
15.500 1.3825 0.05312 0.04700 -0.0229 0.0276 1.0000
15.750 1.3845 0.05581 0.04975 -0.0229 0.0269 1.0000
16.000 1.3855 0.05868 0.05269 -0.0231 0.0262 1.0000
16.250 1.3885 0.06137 0.05547 -0.0233 0.0257 1.0000
16.500 1.3910 0.06419 0.05838 -0.0237 0.0252 1.0000
16.750 1.3926 0.06717 0.06145 -0.0241 0.0246 1.0000
17.000 1.3936 0.07030 0.06466 -0.0247 0.0241 1.0000
17.250 1.3936 0.07361 0.06805 -0.0254 0.0235 1.0000
17.500 1.3927 0.07711 0.07164 -0.0263 0.0231 1.0000
17.750 1.3908 0.08083 0.07543 -0.0273 0.0226 1.0000
18.000 1.3868 0.08492 0.07960 -0.0285 0.0222 1.0000
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