SG6043 (sg6043-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: SG6043 (sg6043-il) Reynolds number: 1,000,000 Max Cl/Cd: 145.24 at α=2.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-sg6043-il-1000000-n5.txt Download as CSV file: xf-sg6043-il-1000000-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 = 1.000 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-9.500 -0.1085 0.08890 0.08701 -0.0968 0.9673 0.0064
-9.250 -0.1027 0.08375 0.08187 -0.1004 0.9640 0.0067
-8.250 -0.1252 0.02065 0.01760 -0.1748 0.9002 0.0081
-8.000 -0.1022 0.01794 0.01445 -0.1766 0.8918 0.0084
-7.750 -0.0779 0.01649 0.01273 -0.1772 0.8841 0.0086
-7.500 -0.0518 0.01541 0.01140 -0.1778 0.8774 0.0088
-7.250 -0.0271 0.01419 0.00993 -0.1781 0.8704 0.0090
-7.000 -0.0012 0.01315 0.00868 -0.1784 0.8640 0.0092
-6.750 0.0251 0.01250 0.00790 -0.1785 0.8580 0.0093
-6.500 0.0518 0.01202 0.00732 -0.1786 0.8516 0.0095
-6.250 0.0789 0.01154 0.00673 -0.1786 0.8460 0.0097
-6.000 0.1058 0.01108 0.00617 -0.1787 0.8403 0.0098
-5.750 0.1329 0.01067 0.00565 -0.1787 0.8346 0.0101
-5.500 0.1602 0.01027 0.00515 -0.1787 0.8297 0.0103
-5.250 0.1875 0.00988 0.00469 -0.1787 0.8245 0.0105
-5.000 0.2149 0.00956 0.00428 -0.1787 0.8193 0.0107
-4.750 0.2425 0.00929 0.00393 -0.1787 0.8145 0.0110
-4.500 0.2702 0.00906 0.00365 -0.1786 0.8096 0.0113
-4.250 0.2978 0.00885 0.00338 -0.1786 0.8043 0.0115
-4.000 0.3254 0.00847 0.00293 -0.1786 0.7993 0.0119
-3.750 0.3532 0.00822 0.00265 -0.1787 0.7939 0.0122
-3.500 0.3808 0.00804 0.00243 -0.1786 0.7883 0.0127
-3.250 0.4085 0.00790 0.00224 -0.1786 0.7832 0.0131
-3.000 0.4364 0.00775 0.00207 -0.1786 0.7782 0.0135
-2.750 0.4642 0.00764 0.00192 -0.1785 0.7728 0.0139
-2.500 0.4918 0.00755 0.00179 -0.1784 0.7677 0.0144
-2.250 0.5198 0.00742 0.00165 -0.1784 0.7622 0.0152
-2.000 0.5472 0.00735 0.00155 -0.1783 0.7559 0.0167
-1.750 0.5748 0.00728 0.00146 -0.1781 0.7498 0.0191
-1.500 0.6024 0.00716 0.00139 -0.1781 0.7427 0.0328
-1.250 0.6295 0.00711 0.00135 -0.1779 0.7357 0.0476
-1.000 0.6570 0.00705 0.00132 -0.1778 0.7281 0.0613
-0.750 0.6838 0.00702 0.00130 -0.1776 0.7197 0.0783
-0.500 0.7108 0.00697 0.00129 -0.1774 0.7100 0.1034
-0.250 0.7376 0.00690 0.00130 -0.1772 0.7001 0.1437
0.000 0.7639 0.00685 0.00132 -0.1769 0.6890 0.1942
0.250 0.7908 0.00671 0.00136 -0.1768 0.6773 0.2882
0.500 0.8172 0.00659 0.00142 -0.1767 0.6643 0.3898
0.750 0.8431 0.00650 0.00152 -0.1764 0.6492 0.4983
1.000 0.8685 0.00653 0.00161 -0.1759 0.6335 0.5593
1.250 0.8936 0.00660 0.00170 -0.1753 0.6172 0.6004
1.500 0.9183 0.00669 0.00181 -0.1747 0.5995 0.6426
1.750 0.9423 0.00678 0.00194 -0.1739 0.5802 0.7010
2.000 0.9659 0.00686 0.00209 -0.1730 0.5587 0.7646
2.250 0.9875 0.00695 0.00226 -0.1716 0.5358 0.8396
2.500 1.0036 0.00691 0.00235 -0.1689 0.5151 1.0000
2.750 1.0270 0.00718 0.00250 -0.1680 0.4904 1.0000
3.000 1.0493 0.00750 0.00267 -0.1669 0.4616 1.0000
3.250 1.0711 0.00786 0.00286 -0.1658 0.4306 1.0000
3.500 1.0931 0.00821 0.00306 -0.1647 0.4025 1.0000
3.750 1.1153 0.00854 0.00327 -0.1636 0.3766 1.0000
4.000 1.1376 0.00886 0.00347 -0.1626 0.3543 1.0000
4.250 1.1591 0.00922 0.00370 -0.1614 0.3290 1.0000
4.500 1.1804 0.00958 0.00394 -0.1602 0.3048 1.0000
4.750 1.2018 0.00991 0.00417 -0.1590 0.2853 1.0000
5.000 1.2217 0.01028 0.00443 -0.1575 0.2643 1.0000
5.250 1.2415 0.01065 0.00469 -0.1561 0.2429 1.0000
5.500 1.2606 0.01104 0.00498 -0.1544 0.2220 1.0000
5.750 1.2785 0.01150 0.00531 -0.1526 0.1981 1.0000
6.000 1.2970 0.01193 0.00564 -0.1510 0.1784 1.0000
6.250 1.3165 0.01231 0.00594 -0.1495 0.1643 1.0000
6.500 1.3359 0.01268 0.00626 -0.1480 0.1523 1.0000
6.750 1.3549 0.01307 0.00660 -0.1465 0.1403 1.0000
7.000 1.3735 0.01349 0.00696 -0.1449 0.1285 1.0000
7.500 1.4112 0.01429 0.00769 -0.1418 0.1102 1.0000
7.750 1.4294 0.01473 0.00809 -0.1402 0.1022 1.0000
8.000 1.4473 0.01518 0.00851 -0.1386 0.0942 1.0000
8.250 1.4657 0.01560 0.00892 -0.1371 0.0882 1.0000
8.500 1.4829 0.01609 0.00939 -0.1354 0.0821 1.0000
8.750 1.5009 0.01653 0.00983 -0.1339 0.0772 1.0000
9.000 1.5175 0.01707 0.01035 -0.1322 0.0713 1.0000
9.250 1.5344 0.01758 0.01086 -0.1305 0.0666 1.0000
9.500 1.5506 0.01815 0.01142 -0.1288 0.0617 1.0000
9.750 1.5663 0.01873 0.01201 -0.1271 0.0572 1.0000
10.000 1.5814 0.01938 0.01265 -0.1253 0.0523 1.0000
10.250 1.5963 0.02004 0.01331 -0.1235 0.0483 1.0000
10.500 1.6111 0.02072 0.01400 -0.1217 0.0449 1.0000
10.750 1.6249 0.02148 0.01476 -0.1199 0.0417 1.0000
11.000 1.6398 0.02216 0.01548 -0.1182 0.0395 1.0000
11.250 1.6531 0.02297 0.01631 -0.1165 0.0369 1.0000
11.500 1.6661 0.02383 0.01718 -0.1147 0.0348 1.0000
11.750 1.6800 0.02462 0.01802 -0.1131 0.0334 1.0000
12.000 1.6931 0.02549 0.01893 -0.1114 0.0318 1.0000
12.250 1.7047 0.02649 0.01996 -0.1096 0.0301 1.0000
12.500 1.7164 0.02751 0.02102 -0.1079 0.0286 1.0000
12.750 1.7286 0.02850 0.02206 -0.1064 0.0274 1.0000
13.000 1.7397 0.02959 0.02320 -0.1048 0.0259 1.0000
13.250 1.7493 0.03083 0.02448 -0.1031 0.0244 1.0000
13.500 1.7592 0.03208 0.02577 -0.1015 0.0230 1.0000
13.750 1.7689 0.03338 0.02712 -0.1000 0.0216 1.0000
14.000 1.7767 0.03487 0.02864 -0.0984 0.0199 1.0000
14.250 1.7849 0.03635 0.03018 -0.0969 0.0188 1.0000
14.500 1.7929 0.03790 0.03179 -0.0955 0.0176 1.0000
14.750 1.7992 0.03964 0.03358 -0.0941 0.0165 1.0000
15.000 1.8055 0.04144 0.03544 -0.0928 0.0156 1.0000
15.250 1.8122 0.04324 0.03731 -0.0916 0.0150 1.0000
15.500 1.8178 0.04519 0.03933 -0.0905 0.0143 1.0000
15.750 1.8219 0.04735 0.04156 -0.0894 0.0135 1.0000
16.000 1.8250 0.04970 0.04397 -0.0884 0.0128 1.0000
16.250 1.8291 0.05198 0.04635 -0.0875 0.0124 1.0000
16.500 1.8326 0.05441 0.04886 -0.0868 0.0118 1.0000
16.750 1.8346 0.05706 0.05159 -0.0862 0.0113 1.0000
17.000 1.8351 0.05998 0.05458 -0.0857 0.0107 1.0000
17.250 1.8346 0.06311 0.05780 -0.0854 0.0102 1.0000
17.500 1.8348 0.06626 0.06104 -0.0852 0.0099 1.0000
17.750 1.8346 0.06952 0.06441 -0.0852 0.0097 1.0000
18.000 1.8334 0.07301 0.06800 -0.0853 0.0094 1.0000
18.250 1.8310 0.07674 0.07184 -0.0857 0.0092 1.0000
18.500 1.8275 0.08074 0.07595 -0.0863 0.0089 1.0000
18.750 1.8227 0.08505 0.08036 -0.0871 0.0087 1.0000
19.000 1.8167 0.08964 0.08506 -0.0881 0.0084 1.0000
19.250 1.8093 0.09454 0.09007 -0.0894 0.0082 1.0000
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