SD6080 (9.2%) (sd6080-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: SD6080 (9.2%) (sd6080-il) Reynolds number: 1,000,000 Max Cl/Cd: 137.42 at α=4.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-sd6080-il-1000000.txt Download as CSV file: xf-sd6080-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: SD6080 (9.2%)
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
------ -------- --------- --------- -------- -------- --------
-10.250 -0.3630 0.11013 0.10847 -0.0235 1.0000 0.0082
-10.000 -0.3578 0.10682 0.10517 -0.0248 1.0000 0.0082
-8.000 -0.3216 0.07677 0.07527 -0.0418 0.9789 0.0102
-7.750 -0.3104 0.06752 0.06598 -0.0545 0.9463 0.0105
-7.500 -0.3072 0.06307 0.06144 -0.0590 0.9165 0.0105
-7.250 -0.3023 0.05931 0.05759 -0.0625 0.8963 0.0107
-7.000 -0.2944 0.05520 0.05338 -0.0663 0.8798 0.0108
-6.750 -0.2820 0.05206 0.05015 -0.0690 0.8665 0.0112
-6.500 -0.2691 0.04733 0.04529 -0.0728 0.8541 0.0115
-6.250 -0.2544 0.04198 0.03975 -0.0762 0.8426 0.0119
-6.000 -0.2376 0.03511 0.03259 -0.0790 0.8322 0.0130
-4.750 -0.1305 0.01376 0.00876 -0.0799 0.7892 0.0104
-4.500 -0.1041 0.01248 0.00731 -0.0796 0.7814 0.0100
-4.250 -0.0773 0.01129 0.00592 -0.0794 0.7730 0.0100
-4.000 -0.0502 0.01056 0.00505 -0.0791 0.7652 0.0101
-3.750 -0.0231 0.00976 0.00412 -0.0789 0.7571 0.0104
-3.500 0.0039 0.00904 0.00330 -0.0787 0.7494 0.0113
-3.250 0.0316 0.00871 0.00290 -0.0787 0.7414 0.0119
-3.000 0.0596 0.00843 0.00256 -0.0786 0.7338 0.0126
-2.750 0.0875 0.00819 0.00225 -0.0785 0.7260 0.0132
-2.500 0.1157 0.00795 0.00195 -0.0785 0.7186 0.0143
-2.250 0.1437 0.00773 0.00166 -0.0784 0.7111 0.0169
-2.000 0.1718 0.00743 0.00142 -0.0784 0.7037 0.0355
-1.750 0.1996 0.00719 0.00129 -0.0784 0.6964 0.0778
-1.500 0.2276 0.00700 0.00120 -0.0785 0.6891 0.1176
-1.250 0.2553 0.00676 0.00113 -0.0785 0.6818 0.1838
-1.000 0.2831 0.00650 0.00109 -0.0787 0.6747 0.2637
-0.750 0.3103 0.00617 0.00106 -0.0787 0.6673 0.3807
-0.500 0.3378 0.00589 0.00105 -0.0788 0.6600 0.4858
-0.250 0.3647 0.00562 0.00106 -0.0787 0.6523 0.6017
0.000 0.3905 0.00526 0.00109 -0.0782 0.6446 0.7408
0.250 0.4105 0.00486 0.00114 -0.0762 0.6370 0.9118
0.500 0.4528 0.00478 0.00109 -0.0791 0.6287 1.0000
0.750 0.4804 0.00486 0.00109 -0.0790 0.6209 1.0000
1.000 0.5082 0.00491 0.00110 -0.0790 0.6125 1.0000
1.250 0.5360 0.00499 0.00112 -0.0789 0.6042 1.0000
1.500 0.5638 0.00506 0.00114 -0.0789 0.5953 1.0000
1.750 0.5916 0.00513 0.00117 -0.0788 0.5862 1.0000
2.000 0.6193 0.00523 0.00120 -0.0788 0.5768 1.0000
2.250 0.6471 0.00530 0.00124 -0.0788 0.5668 1.0000
2.500 0.6749 0.00539 0.00130 -0.0787 0.5568 1.0000
2.750 0.7025 0.00549 0.00136 -0.0787 0.5464 1.0000
3.000 0.7300 0.00561 0.00142 -0.0786 0.5347 1.0000
3.250 0.7575 0.00572 0.00149 -0.0786 0.5221 1.0000
3.500 0.7850 0.00584 0.00158 -0.0785 0.5089 1.0000
3.750 0.8123 0.00598 0.00168 -0.0785 0.4947 1.0000
4.000 0.8393 0.00614 0.00178 -0.0784 0.4785 1.0000
4.250 0.8663 0.00632 0.00190 -0.0783 0.4615 1.0000
4.500 0.8932 0.00650 0.00204 -0.0781 0.4431 1.0000
4.750 0.9196 0.00673 0.00219 -0.0780 0.4216 1.0000
5.000 0.9459 0.00697 0.00236 -0.0778 0.3990 1.0000
5.250 0.9711 0.00733 0.00258 -0.0775 0.3655 1.0000
5.500 0.9953 0.00780 0.00285 -0.0771 0.3221 1.0000
5.750 1.0196 0.00826 0.00314 -0.0767 0.2847 1.0000
6.000 1.0438 0.00872 0.00344 -0.0763 0.2511 1.0000
6.500 1.0915 0.00967 0.00410 -0.0754 0.1906 1.0000
6.750 1.1149 0.01018 0.00447 -0.0749 0.1617 1.0000
7.000 1.1383 0.01066 0.00483 -0.0743 0.1378 1.0000
7.250 1.1614 0.01116 0.00523 -0.0738 0.1148 1.0000
7.500 1.1836 0.01174 0.00567 -0.0731 0.0906 1.0000
7.750 1.2046 0.01241 0.00619 -0.0723 0.0652 1.0000
8.000 1.2228 0.01334 0.00690 -0.0711 0.0340 1.0000
8.250 1.2402 0.01432 0.00772 -0.0697 0.0137 1.0000
8.500 1.2620 0.01482 0.00826 -0.0689 0.0119 1.0000
8.750 1.2829 0.01539 0.00886 -0.0680 0.0108 1.0000
9.000 1.3020 0.01609 0.00964 -0.0667 0.0098 1.0000
9.250 1.3216 0.01670 0.01031 -0.0656 0.0094 1.0000
9.500 1.3407 0.01730 0.01099 -0.0645 0.0092 1.0000
9.750 1.3585 0.01796 0.01172 -0.0631 0.0089 1.0000
10.000 1.3747 0.01869 0.01252 -0.0616 0.0086 1.0000
10.250 1.3889 0.01944 0.01334 -0.0597 0.0083 1.0000
10.500 1.3995 0.02021 0.01417 -0.0573 0.0081 1.0000
10.750 1.4081 0.02108 0.01510 -0.0547 0.0078 1.0000
11.000 1.4152 0.02210 0.01620 -0.0521 0.0075 1.0000
11.250 1.4191 0.02340 0.01760 -0.0495 0.0073 1.0000
11.500 1.4179 0.02516 0.01947 -0.0466 0.0071 1.0000
11.750 1.4128 0.02739 0.02183 -0.0438 0.0069 1.0000
12.000 1.4132 0.02936 0.02391 -0.0417 0.0068 1.0000
12.250 1.4202 0.03087 0.02551 -0.0405 0.0067 1.0000
12.500 1.4250 0.03264 0.02737 -0.0392 0.0067 1.0000
12.750 1.4288 0.03461 0.02944 -0.0381 0.0066 1.0000
13.000 1.4303 0.03687 0.03180 -0.0370 0.0065 1.0000
13.250 1.4336 0.03904 0.03407 -0.0362 0.0064 1.0000
13.500 1.4353 0.04146 0.03659 -0.0356 0.0064 1.0000
13.750 1.4347 0.04422 0.03947 -0.0350 0.0063 1.0000
14.000 1.4359 0.04687 0.04223 -0.0347 0.0062 1.0000
14.250 1.4335 0.05002 0.04550 -0.0345 0.0062 1.0000
14.500 1.4318 0.05322 0.04881 -0.0346 0.0061 1.0000
14.750 1.4307 0.05646 0.05217 -0.0349 0.0060 1.0000
15.000 1.4271 0.06014 0.05597 -0.0354 0.0059 1.0000
15.250 1.4235 0.06398 0.05992 -0.0362 0.0058 1.0000
15.500 1.4199 0.06799 0.06405 -0.0372 0.0058 1.0000
15.750 1.4170 0.07202 0.06818 -0.0386 0.0056 1.0000
16.000 1.4131 0.07635 0.07261 -0.0402 0.0055 1.0000
16.250 1.4062 0.08132 0.07771 -0.0420 0.0054 1.0000
16.500 1.3985 0.08659 0.08310 -0.0442 0.0054 1.0000
16.750 1.3907 0.09204 0.08866 -0.0466 0.0053 1.0000
17.000 1.3829 0.09767 0.09440 -0.0492 0.0052 1.0000
17.250 1.3716 0.10408 0.10096 -0.0523 0.0052 1.0000
17.500 1.3631 0.11013 0.10712 -0.0554 0.0052 1.0000
17.750 1.3525 0.11674 0.11384 -0.0589 0.0051 1.0000
18.000 1.3421 0.12348 0.12071 -0.0626 0.0051 1.0000
18.250 1.3307 0.13059 0.12793 -0.0666 0.0051 1.0000
18.500 1.3185 0.13802 0.13550 -0.0710 0.0051 1.0000
18.750 1.3074 0.14539 0.14299 -0.0754 0.0050 1.0000
19.000 1.2957 0.15305 0.15076 -0.0802 0.0050 1.0000
19.250 1.2843 0.16087 0.15870 -0.0851 0.0050 1.0000
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Polar data table (+)
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