SG6051 (sg6051-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: SG6051 (sg6051-il) Reynolds number: 1,000,000 Max Cl/Cd: 115.79 at α=3.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-sg6051-il-1000000-n5.txt Download as CSV file: xf-sg6051-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: SG6051
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
------ -------- --------- --------- -------- -------- --------
-13.500 -0.6691 0.10229 0.10049 -0.0290 1.0000 0.0037
-13.250 -0.8288 0.06678 0.06478 -0.0502 1.0000 0.0033
-13.000 -0.8892 0.04371 0.04136 -0.0706 0.9896 0.0031
-12.250 -0.9275 0.03155 0.02833 -0.0711 0.9117 0.0032
-12.000 -0.9230 0.02869 0.02516 -0.0703 0.9019 0.0032
-11.750 -0.9121 0.02642 0.02263 -0.0696 0.8943 0.0033
-11.500 -0.8966 0.02465 0.02063 -0.0691 0.8872 0.0033
-11.250 -0.8784 0.02316 0.01894 -0.0686 0.8813 0.0034
-11.000 -0.8581 0.02189 0.01750 -0.0684 0.8755 0.0035
-10.750 -0.8366 0.02077 0.01620 -0.0681 0.8699 0.0036
-10.500 -0.8138 0.01976 0.01504 -0.0679 0.8650 0.0036
-10.250 -0.7902 0.01884 0.01399 -0.0678 0.8598 0.0037
-10.000 -0.7660 0.01802 0.01302 -0.0677 0.8550 0.0038
-9.750 -0.7411 0.01725 0.01213 -0.0677 0.8508 0.0038
-9.500 -0.7156 0.01653 0.01130 -0.0677 0.8462 0.0039
-9.250 -0.6898 0.01588 0.01053 -0.0678 0.8419 0.0041
-9.000 -0.6636 0.01528 0.00981 -0.0678 0.8381 0.0042
-8.750 -0.6368 0.01472 0.00916 -0.0680 0.8341 0.0043
-8.500 -0.6099 0.01420 0.00855 -0.0681 0.8298 0.0044
-8.250 -0.5827 0.01373 0.00798 -0.0683 0.8257 0.0046
-8.000 -0.5553 0.01330 0.00747 -0.0685 0.8222 0.0047
-7.750 -0.5274 0.01290 0.00699 -0.0687 0.8184 0.0049
-7.500 -0.4998 0.01243 0.00645 -0.0689 0.8142 0.0051
-7.250 -0.4720 0.01204 0.00597 -0.0691 0.8103 0.0055
-7.000 -0.4439 0.01168 0.00556 -0.0694 0.8066 0.0059
-6.750 -0.4155 0.01135 0.00519 -0.0697 0.8025 0.0063
-6.500 -0.3870 0.01106 0.00484 -0.0700 0.7982 0.0069
-6.250 -0.3587 0.01074 0.00447 -0.0703 0.7941 0.0086
-6.000 -0.3302 0.01042 0.00415 -0.0707 0.7901 0.0123
-5.750 -0.3015 0.01015 0.00390 -0.0710 0.7856 0.0176
-5.500 -0.2727 0.00996 0.00369 -0.0714 0.7814 0.0212
-5.250 -0.2437 0.00978 0.00351 -0.0718 0.7776 0.0245
-5.000 -0.2146 0.00963 0.00334 -0.0722 0.7734 0.0263
-4.750 -0.1855 0.00945 0.00316 -0.0726 0.7689 0.0295
-4.500 -0.1564 0.00932 0.00300 -0.0730 0.7648 0.0318
-4.250 -0.1271 0.00920 0.00286 -0.0734 0.7608 0.0336
-4.000 -0.0979 0.00902 0.00268 -0.0738 0.7562 0.0378
-3.750 -0.0687 0.00890 0.00254 -0.0742 0.7519 0.0408
-3.500 -0.0393 0.00880 0.00241 -0.0746 0.7479 0.0427
-3.250 -0.0099 0.00865 0.00227 -0.0751 0.7434 0.0480
-3.000 0.0194 0.00854 0.00215 -0.0755 0.7388 0.0528
-2.750 0.0487 0.00843 0.00204 -0.0759 0.7346 0.0603
-2.500 0.0782 0.00831 0.00194 -0.0764 0.7302 0.0706
-2.250 0.1075 0.00816 0.00184 -0.0769 0.7252 0.0906
-2.000 0.1367 0.00801 0.00176 -0.0774 0.7203 0.1173
-1.500 0.1954 0.00761 0.00160 -0.0784 0.7097 0.2036
-1.250 0.2243 0.00724 0.00152 -0.0790 0.7050 0.3017
-1.000 0.2537 0.00706 0.00151 -0.0796 0.7001 0.3616
-0.750 0.2832 0.00700 0.00150 -0.0801 0.6949 0.3874
-0.500 0.3125 0.00695 0.00149 -0.0805 0.6900 0.4125
-0.250 0.3420 0.00684 0.00148 -0.0810 0.6846 0.4490
0.000 0.3712 0.00671 0.00148 -0.0815 0.6788 0.4926
0.250 0.4002 0.00645 0.00151 -0.0821 0.6728 0.5871
0.500 0.4292 0.00625 0.00153 -0.0825 0.6653 0.6662
0.750 0.4581 0.00616 0.00156 -0.0829 0.6580 0.7150
1.000 0.4867 0.00605 0.00160 -0.0831 0.6501 0.7708
1.250 0.5143 0.00594 0.00165 -0.0831 0.6420 0.8323
1.750 0.5669 0.00587 0.00174 -0.0824 0.6221 0.9134
2.000 0.5918 0.00586 0.00176 -0.0816 0.6123 0.9468
2.250 0.6207 0.00590 0.00177 -0.0819 0.6009 0.9791
2.500 0.6524 0.00598 0.00180 -0.0829 0.5867 0.9957
2.750 0.6822 0.00608 0.00185 -0.0835 0.5714 1.0000
3.000 0.7106 0.00622 0.00194 -0.0838 0.5555 1.0000
3.250 0.7387 0.00640 0.00204 -0.0841 0.5347 1.0000
3.500 0.7665 0.00662 0.00216 -0.0843 0.5109 1.0000
4.000 0.8209 0.00719 0.00248 -0.0846 0.4503 1.0000
4.250 0.8467 0.00763 0.00272 -0.0845 0.4051 1.0000
4.500 0.8717 0.00815 0.00300 -0.0844 0.3544 1.0000
4.750 0.8959 0.00875 0.00333 -0.0841 0.2994 1.0000
5.000 0.9202 0.00930 0.00365 -0.0839 0.2532 1.0000
5.250 0.9445 0.00981 0.00398 -0.0836 0.2130 1.0000
5.500 0.9692 0.01026 0.00429 -0.0834 0.1829 1.0000
5.750 0.9932 0.01076 0.00462 -0.0830 0.1523 1.0000
6.000 1.0175 0.01119 0.00495 -0.0827 0.1278 1.0000
6.250 1.0417 0.01162 0.00529 -0.0824 0.1077 1.0000
6.500 1.0657 0.01204 0.00563 -0.0820 0.0900 1.0000
6.750 1.0886 0.01254 0.00602 -0.0815 0.0715 1.0000
7.000 1.1117 0.01299 0.00640 -0.0809 0.0569 1.0000
7.250 1.1346 0.01344 0.00679 -0.0803 0.0459 1.0000
7.500 1.1573 0.01388 0.00719 -0.0797 0.0376 1.0000
7.750 1.1796 0.01432 0.00760 -0.0791 0.0312 1.0000
8.000 1.2021 0.01471 0.00799 -0.0784 0.0276 1.0000
8.250 1.2236 0.01516 0.00843 -0.0776 0.0240 1.0000
8.500 1.2454 0.01555 0.00884 -0.0768 0.0223 1.0000
8.750 1.2662 0.01598 0.00928 -0.0759 0.0204 1.0000
9.000 1.2856 0.01647 0.00977 -0.0747 0.0183 1.0000
9.250 1.3054 0.01690 0.01024 -0.0736 0.0171 1.0000
9.500 1.3231 0.01738 0.01075 -0.0722 0.0154 1.0000
9.750 1.3372 0.01797 0.01135 -0.0701 0.0136 1.0000
10.000 1.3527 0.01853 0.01194 -0.0683 0.0122 1.0000
10.250 1.3670 0.01921 0.01263 -0.0665 0.0105 1.0000
10.500 1.3819 0.01989 0.01334 -0.0649 0.0094 1.0000
10.750 1.3964 0.02063 0.01412 -0.0633 0.0085 1.0000
11.000 1.4100 0.02146 0.01499 -0.0616 0.0077 1.0000
11.250 1.4242 0.02228 0.01586 -0.0601 0.0073 1.0000
11.500 1.4380 0.02314 0.01678 -0.0587 0.0069 1.0000
11.750 1.4512 0.02407 0.01777 -0.0572 0.0066 1.0000
12.000 1.4636 0.02508 0.01882 -0.0557 0.0062 1.0000
12.250 1.4751 0.02617 0.01997 -0.0542 0.0059 1.0000
12.500 1.4852 0.02742 0.02127 -0.0527 0.0055 1.0000
12.750 1.4960 0.02860 0.02254 -0.0512 0.0053 1.0000
13.000 1.5070 0.02980 0.02381 -0.0499 0.0052 1.0000
13.250 1.5170 0.03110 0.02518 -0.0486 0.0051 1.0000
13.500 1.5263 0.03249 0.02665 -0.0473 0.0049 1.0000
13.750 1.5347 0.03396 0.02819 -0.0460 0.0048 1.0000
14.000 1.5425 0.03551 0.02982 -0.0447 0.0047 1.0000
14.250 1.5496 0.03717 0.03156 -0.0435 0.0045 1.0000
14.500 1.5557 0.03894 0.03341 -0.0424 0.0044 1.0000
14.750 1.5608 0.04082 0.03537 -0.0412 0.0043 1.0000
15.000 1.5648 0.04286 0.03750 -0.0401 0.0041 1.0000
15.250 1.5673 0.04512 0.03984 -0.0391 0.0040 1.0000
15.500 1.5678 0.04766 0.04248 -0.0382 0.0039 1.0000
15.750 1.5663 0.05049 0.04542 -0.0373 0.0037 1.0000
16.000 1.5688 0.05298 0.04801 -0.0368 0.0037 1.0000
16.250 1.5711 0.05558 0.05070 -0.0364 0.0036 1.0000
16.500 1.5717 0.05844 0.05366 -0.0361 0.0036 1.0000
16.750 1.5708 0.06154 0.05687 -0.0360 0.0035 1.0000
17.000 1.5685 0.06490 0.06034 -0.0360 0.0034 1.0000
17.250 1.5656 0.06847 0.06402 -0.0362 0.0034 1.0000
17.500 1.5616 0.07226 0.06792 -0.0366 0.0033 1.0000
17.750 1.5560 0.07638 0.07216 -0.0372 0.0033 1.0000
18.000 1.5489 0.08079 0.07669 -0.0380 0.0032 1.0000
18.250 1.5411 0.08542 0.08145 -0.0391 0.0032 1.0000
18.500 1.5312 0.09050 0.08666 -0.0404 0.0031 1.0000
18.750 1.5207 0.09583 0.09211 -0.0420 0.0031 1.0000
19.000 1.5077 0.10165 0.09806 -0.0440 0.0031 1.0000
19.250 1.4941 0.10770 0.10424 -0.0463 0.0030 1.0000
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