S4310 (s4310-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: S4310 (s4310-il) Reynolds number: 1,000,000 Max Cl/Cd: 117.91 at α=4.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-s4310-il-1000000-n5.txt Download as CSV file: xf-s4310-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: S4310
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
------ -------- --------- --------- -------- -------- --------
-12.750 -0.3643 0.13633 0.13461 -0.0218 1.0000 0.0042
-12.500 -0.3549 0.13428 0.13258 -0.0229 1.0000 0.0045
-10.500 -0.6630 0.02789 0.02504 -0.0846 0.8536 0.0047
-10.250 -0.6539 0.02468 0.02146 -0.0845 0.8434 0.0048
-10.000 -0.6363 0.02294 0.01949 -0.0842 0.8349 0.0049
-9.750 -0.6180 0.02119 0.01748 -0.0838 0.8263 0.0050
-9.500 -0.5961 0.02007 0.01619 -0.0835 0.8186 0.0052
-9.000 -0.5517 0.01769 0.01336 -0.0829 0.8033 0.0055
-8.500 -0.5038 0.01584 0.01115 -0.0824 0.7888 0.0057
-8.250 -0.4788 0.01512 0.01026 -0.0821 0.7815 0.0059
-8.000 -0.4533 0.01445 0.00944 -0.0819 0.7746 0.0060
-7.750 -0.4273 0.01391 0.00876 -0.0817 0.7674 0.0060
-7.500 -0.4020 0.01308 0.00778 -0.0815 0.7606 0.0064
-7.250 -0.3755 0.01262 0.00723 -0.0813 0.7536 0.0067
-7.000 -0.3486 0.01221 0.00675 -0.0812 0.7472 0.0069
-6.750 -0.3215 0.01188 0.00634 -0.0811 0.7401 0.0072
-6.500 -0.2943 0.01156 0.00594 -0.0810 0.7338 0.0076
-6.250 -0.2670 0.01123 0.00552 -0.0809 0.7269 0.0079
-6.000 -0.2396 0.01093 0.00514 -0.0808 0.7207 0.0084
-5.750 -0.2120 0.01066 0.00480 -0.0807 0.7141 0.0087
-5.250 -0.1565 0.01020 0.00427 -0.0806 0.7015 0.0101
-5.000 -0.1287 0.01000 0.00402 -0.0806 0.6950 0.0107
-4.750 -0.1008 0.00979 0.00375 -0.0805 0.6891 0.0114
-4.500 -0.0728 0.00961 0.00351 -0.0805 0.6825 0.0118
-4.250 -0.0451 0.00933 0.00318 -0.0804 0.6766 0.0127
-4.000 -0.0169 0.00916 0.00299 -0.0805 0.6702 0.0135
-3.500 0.0394 0.00890 0.00265 -0.0805 0.6579 0.0154
-3.250 0.0676 0.00880 0.00250 -0.0805 0.6514 0.0160
-3.000 0.0956 0.00856 0.00221 -0.0804 0.6454 0.0171
-2.750 0.1237 0.00841 0.00203 -0.0804 0.6388 0.0185
-2.500 0.1519 0.00830 0.00188 -0.0804 0.6326 0.0196
-2.250 0.1803 0.00819 0.00173 -0.0805 0.6260 0.0206
-2.000 0.2084 0.00812 0.00161 -0.0804 0.6195 0.0214
-1.750 0.2368 0.00801 0.00148 -0.0805 0.6127 0.0242
-1.250 0.2932 0.00780 0.00130 -0.0805 0.5982 0.0456
-1.000 0.3211 0.00768 0.00123 -0.0805 0.5902 0.0743
-0.750 0.3491 0.00753 0.00119 -0.0806 0.5819 0.1147
-0.500 0.3770 0.00739 0.00115 -0.0807 0.5736 0.1621
-0.250 0.4049 0.00727 0.00113 -0.0807 0.5647 0.2084
0.000 0.4327 0.00713 0.00113 -0.0808 0.5562 0.2684
0.250 0.4603 0.00701 0.00114 -0.0808 0.5473 0.3340
0.500 0.4879 0.00684 0.00116 -0.0809 0.5385 0.4123
0.750 0.5143 0.00648 0.00121 -0.0809 0.5297 0.5721
1.000 0.5407 0.00624 0.00126 -0.0806 0.5199 0.6903
1.250 0.5663 0.00606 0.00133 -0.0802 0.5103 0.7878
1.500 0.5896 0.00593 0.00141 -0.0790 0.5000 0.8793
1.750 0.6132 0.00593 0.00147 -0.0778 0.4888 0.9391
2.000 0.6473 0.00600 0.00151 -0.0791 0.4754 0.9768
2.250 0.6841 0.00613 0.00156 -0.0811 0.4608 0.9996
2.500 0.7110 0.00627 0.00163 -0.0810 0.4473 1.0000
2.750 0.7378 0.00642 0.00171 -0.0808 0.4336 1.0000
3.000 0.7644 0.00659 0.00180 -0.0806 0.4186 1.0000
3.250 0.7909 0.00677 0.00191 -0.0804 0.4032 1.0000
3.500 0.8174 0.00696 0.00202 -0.0803 0.3880 1.0000
3.750 0.8437 0.00717 0.00215 -0.0801 0.3721 1.0000
4.000 0.8700 0.00738 0.00228 -0.0799 0.3558 1.0000
4.250 0.8961 0.00760 0.00244 -0.0797 0.3396 1.0000
4.500 0.9221 0.00783 0.00260 -0.0794 0.3232 1.0000
4.750 0.9479 0.00808 0.00276 -0.0792 0.3073 1.0000
5.000 0.9735 0.00834 0.00295 -0.0789 0.2910 1.0000
5.250 0.9991 0.00859 0.00314 -0.0787 0.2764 1.0000
5.500 1.0244 0.00887 0.00335 -0.0784 0.2615 1.0000
5.750 1.0498 0.00913 0.00355 -0.0781 0.2484 1.0000
6.000 1.0748 0.00941 0.00378 -0.0777 0.2344 1.0000
6.250 1.0997 0.00969 0.00401 -0.0774 0.2218 1.0000
6.500 1.1242 0.00999 0.00426 -0.0770 0.2085 1.0000
6.750 1.1487 0.01029 0.00451 -0.0766 0.1972 1.0000
7.000 1.1729 0.01060 0.00478 -0.0762 0.1860 1.0000
7.500 1.2195 0.01132 0.00538 -0.0751 0.1602 1.0000
7.750 1.2420 0.01172 0.00572 -0.0744 0.1467 1.0000
8.000 1.2640 0.01213 0.00608 -0.0737 0.1338 1.0000
8.250 1.2861 0.01252 0.00643 -0.0729 0.1231 1.0000
8.500 1.3072 0.01295 0.00682 -0.0721 0.1113 1.0000
8.750 1.3266 0.01348 0.00726 -0.0710 0.0977 1.0000
9.000 1.3461 0.01396 0.00770 -0.0699 0.0868 1.0000
9.250 1.3644 0.01449 0.00819 -0.0686 0.0761 1.0000
9.500 1.3817 0.01503 0.00868 -0.0672 0.0666 1.0000
9.750 1.3968 0.01560 0.00921 -0.0654 0.0580 1.0000
10.000 1.4082 0.01622 0.00979 -0.0630 0.0494 1.0000
10.250 1.4207 0.01680 0.01036 -0.0608 0.0429 1.0000
10.500 1.4303 0.01756 0.01108 -0.0584 0.0350 1.0000
10.750 1.4394 0.01840 0.01191 -0.0560 0.0277 1.0000
11.000 1.4476 0.01934 0.01282 -0.0537 0.0209 1.0000
11.250 1.4518 0.02059 0.01403 -0.0512 0.0126 1.0000
11.500 1.4539 0.02206 0.01548 -0.0486 0.0052 1.0000
11.750 1.4618 0.02322 0.01669 -0.0468 0.0037 1.0000
12.000 1.4723 0.02426 0.01778 -0.0454 0.0034 1.0000
12.250 1.4822 0.02537 0.01895 -0.0440 0.0031 1.0000
12.500 1.4918 0.02655 0.02020 -0.0428 0.0030 1.0000
12.750 1.4998 0.02790 0.02162 -0.0415 0.0027 1.0000
13.000 1.5075 0.02932 0.02310 -0.0403 0.0026 1.0000
13.250 1.5146 0.03084 0.02470 -0.0392 0.0025 1.0000
13.500 1.5198 0.03258 0.02651 -0.0382 0.0023 1.0000
13.750 1.5244 0.03445 0.02846 -0.0372 0.0021 1.0000
14.000 1.5298 0.03628 0.03037 -0.0364 0.0021 1.0000
14.250 1.5348 0.03821 0.03238 -0.0358 0.0020 1.0000
14.500 1.5379 0.04040 0.03465 -0.0352 0.0020 1.0000
14.750 1.5408 0.04267 0.03701 -0.0347 0.0020 1.0000
15.000 1.5433 0.04508 0.03952 -0.0344 0.0019 1.0000
15.250 1.5442 0.04775 0.04228 -0.0342 0.0019 1.0000
15.500 1.5453 0.05049 0.04511 -0.0342 0.0018 1.0000
15.750 1.5437 0.05366 0.04838 -0.0344 0.0018 1.0000
16.000 1.5421 0.05694 0.05176 -0.0348 0.0018 1.0000
16.250 1.5396 0.06045 0.05537 -0.0353 0.0017 1.0000
16.500 1.5378 0.06397 0.05899 -0.0360 0.0017 1.0000
16.750 1.5326 0.06809 0.06322 -0.0370 0.0017 1.0000
17.000 1.5266 0.07247 0.06771 -0.0382 0.0016 1.0000
17.250 1.5201 0.07705 0.07240 -0.0396 0.0016 1.0000
17.500 1.5122 0.08196 0.07743 -0.0413 0.0016 1.0000
17.750 1.5040 0.08709 0.08268 -0.0432 0.0016 1.0000
18.000 1.4950 0.09248 0.08818 -0.0453 0.0015 1.0000
18.250 1.4825 0.09862 0.09445 -0.0479 0.0015 1.0000
18.500 1.4709 0.10473 0.10069 -0.0507 0.0015 1.0000
18.750 1.4585 0.11114 0.10722 -0.0537 0.0015 1.0000
19.000 1.4463 0.11760 0.11380 -0.0568 0.0015 1.0000
19.250 1.4336 0.12429 0.12061 -0.0602 0.0015 1.0000
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