SG6043 (sg6043-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: SG6043 (sg6043-il) Reynolds number: 500,000 Max Cl/Cd: 129.77 at α=2.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-sg6043-il-500000-n5.txt Download as CSV file: xf-sg6043-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: SG6043
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
------ -------- --------- --------- -------- -------- --------
-9.750 -0.0393 0.08498 0.08256 -0.0928 0.9540 0.0143
-9.500 -0.0317 0.08113 0.07870 -0.0949 0.9517 0.0143
-9.250 -0.1161 0.09556 0.09302 -0.0874 0.9662 0.0130
-8.750 -0.1041 0.08646 0.08393 -0.0935 0.9564 0.0114
-8.500 -0.0918 0.08341 0.08088 -0.0956 0.9527 0.0112
-8.250 -0.0801 0.08060 0.07807 -0.0977 0.9484 0.0107
-8.000 -0.0730 0.07698 0.07445 -0.1000 0.9412 0.0107
-7.750 -0.0588 0.07268 0.07015 -0.1047 0.9376 0.0107
-7.500 -0.0495 0.06866 0.06612 -0.1084 0.9299 0.0107
-7.250 -0.0324 0.06365 0.06110 -0.1153 0.9245 0.0107
-6.750 0.0045 0.02296 0.01917 -0.1683 0.8955 0.0113
-6.500 0.0295 0.01845 0.01387 -0.1714 0.8886 0.0116
-6.250 0.0576 0.01671 0.01184 -0.1727 0.8830 0.0118
-5.750 0.1149 0.01469 0.00939 -0.1743 0.8725 0.0124
-5.500 0.1436 0.01385 0.00836 -0.1749 0.8670 0.0127
-5.250 0.1736 0.01312 0.00744 -0.1756 0.8623 0.0130
-5.000 0.2003 0.01258 0.00676 -0.1755 0.8566 0.0136
-4.750 0.2288 0.01206 0.00610 -0.1758 0.8514 0.0141
-4.500 0.2583 0.01157 0.00546 -0.1762 0.8469 0.0143
-4.250 0.2851 0.01103 0.00486 -0.1761 0.8414 0.0146
-4.000 0.3132 0.01057 0.00434 -0.1763 0.8362 0.0151
-3.500 0.3696 0.00996 0.00364 -0.1765 0.8263 0.0161
-3.250 0.3976 0.00972 0.00334 -0.1766 0.8209 0.0167
-2.750 0.4538 0.00931 0.00283 -0.1766 0.8103 0.0184
-2.500 0.4818 0.00915 0.00264 -0.1766 0.8046 0.0201
-2.250 0.5105 0.00902 0.00246 -0.1768 0.7997 0.0222
-2.000 0.5378 0.00887 0.00232 -0.1766 0.7941 0.0267
-1.750 0.5657 0.00873 0.00222 -0.1766 0.7885 0.0413
-1.500 0.5940 0.00864 0.00214 -0.1767 0.7834 0.0574
-1.250 0.6211 0.00854 0.00210 -0.1766 0.7771 0.0761
-1.000 0.6488 0.00844 0.00205 -0.1766 0.7708 0.1027
-0.500 0.7038 0.00815 0.00202 -0.1766 0.7573 0.2115
-0.250 0.7316 0.00793 0.00203 -0.1767 0.7505 0.3178
0.000 0.7588 0.00768 0.00209 -0.1768 0.7425 0.4433
0.250 0.7858 0.00755 0.00217 -0.1767 0.7345 0.5475
0.500 0.8120 0.00749 0.00223 -0.1763 0.7251 0.6094
0.750 0.8381 0.00747 0.00228 -0.1758 0.7156 0.6587
1.250 0.8871 0.00738 0.00244 -0.1741 0.6939 0.7831
1.500 0.9050 0.00725 0.00250 -0.1717 0.6816 0.8789
1.750 0.9275 0.00722 0.00248 -0.1702 0.6678 1.0000
2.000 0.9525 0.00737 0.00254 -0.1696 0.6534 1.0000
2.250 0.9772 0.00753 0.00262 -0.1689 0.6379 1.0000
2.500 1.0012 0.00772 0.00271 -0.1681 0.6202 1.0000
2.750 1.0244 0.00794 0.00283 -0.1671 0.6004 1.0000
3.250 1.0691 0.00845 0.00311 -0.1648 0.5576 1.0000
3.500 1.0904 0.00874 0.00329 -0.1635 0.5341 1.0000
3.750 1.1107 0.00909 0.00350 -0.1620 0.5060 1.0000
4.000 1.1303 0.00947 0.00373 -0.1604 0.4779 1.0000
4.250 1.1498 0.00986 0.00397 -0.1588 0.4508 1.0000
4.500 1.1696 0.01024 0.00424 -0.1572 0.4245 1.0000
4.750 1.1882 0.01064 0.00451 -0.1555 0.3986 1.0000
5.000 1.2060 0.01107 0.00481 -0.1536 0.3725 1.0000
5.250 1.2237 0.01152 0.00513 -0.1517 0.3458 1.0000
5.500 1.2417 0.01197 0.00547 -0.1500 0.3225 1.0000
5.750 1.2595 0.01244 0.00583 -0.1482 0.2984 1.0000
6.000 1.2769 0.01294 0.00621 -0.1463 0.2749 1.0000
6.250 1.2935 0.01348 0.00662 -0.1444 0.2507 1.0000
6.500 1.3101 0.01403 0.00707 -0.1425 0.2263 1.0000
6.750 1.3263 0.01462 0.00753 -0.1405 0.2045 1.0000
7.000 1.3432 0.01515 0.00799 -0.1387 0.1871 1.0000
7.250 1.3602 0.01569 0.00846 -0.1370 0.1714 1.0000
7.500 1.3773 0.01623 0.00895 -0.1353 0.1580 1.0000
7.750 1.3937 0.01679 0.00946 -0.1335 0.1452 1.0000
8.000 1.4101 0.01737 0.01000 -0.1317 0.1329 1.0000
8.250 1.4268 0.01794 0.01055 -0.1300 0.1229 1.0000
8.500 1.4429 0.01853 0.01113 -0.1283 0.1145 1.0000
8.750 1.4583 0.01919 0.01175 -0.1265 0.1056 1.0000
9.000 1.4743 0.01980 0.01237 -0.1248 0.0983 1.0000
9.250 1.4890 0.02051 0.01307 -0.1230 0.0914 1.0000
9.500 1.5045 0.02117 0.01375 -0.1213 0.0856 1.0000
9.750 1.5184 0.02195 0.01453 -0.1194 0.0797 1.0000
10.000 1.5334 0.02266 0.01527 -0.1178 0.0746 1.0000
10.250 1.5463 0.02354 0.01615 -0.1159 0.0692 1.0000
10.500 1.5606 0.02432 0.01697 -0.1143 0.0651 1.0000
10.750 1.5732 0.02525 0.01791 -0.1125 0.0604 1.0000
11.000 1.5860 0.02617 0.01887 -0.1107 0.0566 1.0000
11.250 1.5982 0.02716 0.01989 -0.1090 0.0526 1.0000
11.500 1.6093 0.02825 0.02100 -0.1073 0.0491 1.0000
11.750 1.6213 0.02929 0.02210 -0.1057 0.0462 1.0000
12.000 1.6319 0.03047 0.02331 -0.1040 0.0435 1.0000
12.250 1.6418 0.03172 0.02461 -0.1023 0.0413 1.0000
12.500 1.6526 0.03292 0.02589 -0.1008 0.0393 1.0000
12.750 1.6621 0.03427 0.02729 -0.0992 0.0372 1.0000
13.000 1.6699 0.03580 0.02886 -0.0976 0.0352 1.0000
13.250 1.6790 0.03723 0.03038 -0.0962 0.0337 1.0000
13.500 1.6876 0.03874 0.03197 -0.0948 0.0321 1.0000
13.750 1.6948 0.04043 0.03374 -0.0934 0.0306 1.0000
14.000 1.7004 0.04232 0.03569 -0.0921 0.0292 1.0000
14.250 1.7074 0.04412 0.03758 -0.0909 0.0280 1.0000
14.500 1.7138 0.04601 0.03957 -0.0898 0.0268 1.0000
14.750 1.7189 0.04810 0.04174 -0.0887 0.0256 1.0000
15.000 1.7225 0.05041 0.04412 -0.0877 0.0244 1.0000
15.250 1.7256 0.05285 0.04665 -0.0868 0.0235 1.0000
15.500 1.7298 0.05522 0.04914 -0.0861 0.0225 1.0000
15.750 1.7326 0.05782 0.05184 -0.0855 0.0215 1.0000
16.000 1.7339 0.06067 0.05478 -0.0850 0.0206 1.0000
16.250 1.7334 0.06384 0.05804 -0.0847 0.0197 1.0000
16.500 1.7336 0.06702 0.06133 -0.0845 0.0190 1.0000
16.750 1.7337 0.07028 0.06471 -0.0845 0.0183 1.0000
17.000 1.7325 0.07381 0.06835 -0.0846 0.0176 1.0000
17.250 1.7299 0.07762 0.07229 -0.0850 0.0170 1.0000
17.500 1.7257 0.08179 0.07656 -0.0856 0.0165 1.0000
17.750 1.7195 0.08639 0.08128 -0.0865 0.0160 1.0000
18.000 1.7142 0.09094 0.08595 -0.0876 0.0156 1.0000
18.250 1.7091 0.09553 0.09069 -0.0888 0.0152 1.0000
18.500 1.7025 0.10047 0.09577 -0.0904 0.0148 1.0000
18.750 1.6955 0.10558 0.10102 -0.0921 0.0144 1.0000
19.000 1.6873 0.11100 0.10658 -0.0942 0.0141 1.0000
19.250 1.6781 0.11668 0.11238 -0.0966 0.0139 1.0000
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