SG6042 (sg6042-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: SG6042 (sg6042-il) Reynolds number: 1,000,000 Max Cl/Cd: 145.51 at α=2.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-sg6042-il-1000000.txt Download as CSV file: xf-sg6042-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: SG6042
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 1.000 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-9.250 -0.2941 0.09340 0.09174 -0.0550 0.9926 0.0101
-9.000 -0.2829 0.08931 0.08765 -0.0588 0.9906 0.0103
-7.750 -0.2847 0.02202 0.01884 -0.1250 0.9570 0.0090
-7.500 -0.2639 0.01936 0.01576 -0.1253 0.9509 0.0091
-7.250 -0.2400 0.01618 0.01214 -0.1265 0.9470 0.0097
-7.000 -0.2157 0.01542 0.01128 -0.1263 0.9409 0.0100
-6.750 -0.1876 0.01480 0.01057 -0.1267 0.9362 0.0105
-6.500 -0.1582 0.01380 0.00937 -0.1273 0.9321 0.0111
-6.250 -0.1337 0.01305 0.00846 -0.1268 0.9253 0.0116
-6.000 -0.1048 0.01257 0.00783 -0.1270 0.9203 0.0119
-5.750 -0.0804 0.01116 0.00624 -0.1267 0.9145 0.0126
-5.500 -0.0544 0.01058 0.00560 -0.1265 0.9085 0.0131
-5.250 -0.0261 0.01018 0.00513 -0.1266 0.9037 0.0138
-5.000 0.0000 0.00979 0.00469 -0.1263 0.8981 0.0145
-4.750 0.0274 0.00959 0.00442 -0.1261 0.8927 0.0152
-4.500 0.0542 0.00892 0.00365 -0.1260 0.8876 0.0160
-4.250 0.0801 0.00855 0.00326 -0.1256 0.8820 0.0168
-4.000 0.1074 0.00829 0.00295 -0.1255 0.8765 0.0177
-3.750 0.1352 0.00806 0.00267 -0.1254 0.8715 0.0187
-3.500 0.1620 0.00782 0.00239 -0.1252 0.8661 0.0199
-3.250 0.1895 0.00759 0.00213 -0.1251 0.8611 0.0216
-3.000 0.2174 0.00745 0.00195 -0.1250 0.8560 0.0235
-2.750 0.2444 0.00725 0.00177 -0.1247 0.8502 0.0293
-2.500 0.2719 0.00703 0.00162 -0.1246 0.8444 0.0549
-2.250 0.2992 0.00689 0.00154 -0.1245 0.8388 0.0734
-2.000 0.3265 0.00675 0.00145 -0.1244 0.8330 0.0949
-1.750 0.3542 0.00659 0.00137 -0.1244 0.8274 0.1355
-1.500 0.3808 0.00633 0.00131 -0.1242 0.8207 0.2022
-1.250 0.4073 0.00597 0.00125 -0.1241 0.8136 0.3213
-1.000 0.4331 0.00548 0.00123 -0.1240 0.8065 0.4894
-0.750 0.4593 0.00520 0.00125 -0.1237 0.7995 0.6114
-0.500 0.4861 0.00510 0.00128 -0.1234 0.7925 0.6691
-0.250 0.5130 0.00507 0.00128 -0.1231 0.7842 0.7008
0.000 0.5396 0.00503 0.00130 -0.1227 0.7752 0.7345
0.250 0.5662 0.00503 0.00131 -0.1223 0.7661 0.7610
0.500 0.5925 0.00501 0.00133 -0.1218 0.7553 0.7845
0.750 0.6181 0.00500 0.00136 -0.1212 0.7432 0.8143
1.000 0.6430 0.00499 0.00139 -0.1203 0.7300 0.8446
1.250 0.6671 0.00500 0.00143 -0.1193 0.7166 0.8756
1.500 0.6894 0.00500 0.00146 -0.1179 0.7018 0.9107
1.750 0.7120 0.00500 0.00149 -0.1165 0.6840 0.9597
2.000 0.7465 0.00514 0.00151 -0.1179 0.6598 1.0000
2.250 0.7712 0.00530 0.00157 -0.1173 0.6357 1.0000
2.500 0.7957 0.00549 0.00165 -0.1166 0.6133 1.0000
2.750 0.8200 0.00569 0.00175 -0.1159 0.5884 1.0000
3.000 0.8436 0.00594 0.00186 -0.1150 0.5590 1.0000
3.250 0.8673 0.00619 0.00198 -0.1142 0.5306 1.0000
3.500 0.8902 0.00648 0.00213 -0.1132 0.4980 1.0000
3.750 0.9125 0.00683 0.00231 -0.1122 0.4613 1.0000
4.000 0.9348 0.00719 0.00249 -0.1112 0.4237 1.0000
4.250 0.9568 0.00757 0.00270 -0.1101 0.3874 1.0000
4.500 0.9789 0.00795 0.00292 -0.1091 0.3512 1.0000
4.750 1.0012 0.00833 0.00314 -0.1081 0.3190 1.0000
5.000 1.0233 0.00871 0.00337 -0.1071 0.2884 1.0000
5.250 1.0454 0.00910 0.00363 -0.1061 0.2592 1.0000
5.500 1.0675 0.00948 0.00388 -0.1051 0.2341 1.0000
5.750 1.0899 0.00984 0.00413 -0.1042 0.2113 1.0000
6.000 1.1117 0.01023 0.00441 -0.1032 0.1899 1.0000
6.250 1.1337 0.01059 0.00469 -0.1022 0.1702 1.0000
6.500 1.1557 0.01096 0.00497 -0.1012 0.1542 1.0000
6.750 1.1775 0.01132 0.00527 -0.1002 0.1398 1.0000
7.000 1.1990 0.01168 0.00558 -0.0992 0.1263 1.0000
7.250 1.2203 0.01205 0.00589 -0.0981 0.1145 1.0000
7.500 1.2412 0.01243 0.00622 -0.0969 0.1034 1.0000
7.750 1.2612 0.01283 0.00657 -0.0956 0.0937 1.0000
8.000 1.2813 0.01316 0.00689 -0.0943 0.0870 1.0000
8.250 1.3004 0.01354 0.00724 -0.0928 0.0796 1.0000
8.500 1.3189 0.01394 0.00761 -0.0912 0.0729 1.0000
8.750 1.3380 0.01431 0.00799 -0.0897 0.0675 1.0000
9.000 1.3561 0.01474 0.00839 -0.0882 0.0624 1.0000
9.250 1.3742 0.01517 0.00883 -0.0866 0.0578 1.0000
9.500 1.3928 0.01556 0.00924 -0.0851 0.0544 1.0000
9.750 1.4092 0.01609 0.00975 -0.0833 0.0498 1.0000
10.000 1.4273 0.01650 0.01020 -0.0818 0.0473 1.0000
10.250 1.4449 0.01696 0.01068 -0.0803 0.0447 1.0000
10.500 1.4600 0.01756 0.01127 -0.0784 0.0411 1.0000
10.750 1.4766 0.01807 0.01182 -0.0768 0.0389 1.0000
11.000 1.4932 0.01858 0.01237 -0.0752 0.0365 1.0000
11.250 1.5068 0.01929 0.01307 -0.0733 0.0334 1.0000
11.500 1.5217 0.01991 0.01374 -0.0715 0.0313 1.0000
11.750 1.5367 0.02053 0.01440 -0.0699 0.0292 1.0000
12.000 1.5480 0.02141 0.01527 -0.0678 0.0262 1.0000
12.250 1.5619 0.02213 0.01605 -0.0661 0.0249 1.0000
12.500 1.5752 0.02289 0.01685 -0.0644 0.0233 1.0000
12.750 1.5859 0.02386 0.01783 -0.0625 0.0217 1.0000
13.000 1.5946 0.02499 0.01903 -0.0604 0.0203 1.0000
13.250 1.6070 0.02586 0.01996 -0.0588 0.0197 1.0000
13.500 1.6177 0.02687 0.02104 -0.0571 0.0189 1.0000
13.750 1.6273 0.02799 0.02221 -0.0555 0.0179 1.0000
14.000 1.6340 0.02937 0.02364 -0.0536 0.0169 1.0000
14.250 1.6377 0.03104 0.02539 -0.0516 0.0161 1.0000
14.500 1.6472 0.03226 0.02670 -0.0502 0.0158 1.0000
14.750 1.6559 0.03358 0.02810 -0.0489 0.0153 1.0000
15.000 1.6630 0.03508 0.02968 -0.0475 0.0148 1.0000
15.250 1.6689 0.03673 0.03140 -0.0462 0.0143 1.0000
15.500 1.6733 0.03857 0.03331 -0.0450 0.0138 1.0000
15.750 1.6754 0.04069 0.03550 -0.0438 0.0133 1.0000
16.000 1.6733 0.04335 0.03826 -0.0427 0.0129 1.0000
16.250 1.6708 0.04617 0.04120 -0.0418 0.0126 1.0000
16.500 1.6751 0.04836 0.04348 -0.0413 0.0124 1.0000
16.750 1.6782 0.05073 0.04596 -0.0409 0.0121 1.0000
17.000 1.6786 0.05354 0.04887 -0.0407 0.0119 1.0000
17.250 1.6786 0.05650 0.05193 -0.0406 0.0116 1.0000
17.500 1.6781 0.05964 0.05517 -0.0409 0.0113 1.0000
17.750 1.6751 0.06322 0.05887 -0.0413 0.0111 1.0000
18.000 1.6704 0.06719 0.06294 -0.0421 0.0108 1.0000
18.250 1.6639 0.07159 0.06745 -0.0432 0.0107 1.0000
18.500 1.6552 0.07651 0.07249 -0.0448 0.0104 1.0000
18.750 1.6431 0.08218 0.07827 -0.0468 0.0102 1.0000
19.000 1.6285 0.08847 0.08470 -0.0494 0.0101 1.0000
19.250 1.6109 0.09557 0.09195 -0.0526 0.0099 1.0000
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