FX 79-W-151 A (fx79w151a-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: FX 79-W-151 A (fx79w151a-il) Reynolds number: 1,000,000 Max Cl/Cd: 126.12 at α=6.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx79w151a-il-1000000-n5.txt Download as CSV file: xf-fx79w151a-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: FX 79-W-151 A
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
------ -------- --------- --------- -------- -------- --------
-16.250 -0.8167 0.08778 0.08527 -0.0471 1.0000 0.0061
-16.000 -0.9026 0.07038 0.06765 -0.0576 1.0000 0.0058
-15.500 -1.0364 0.03786 0.03444 -0.0825 0.9788 0.0055
-15.250 -1.0194 0.03298 0.02933 -0.0915 0.9603 0.0056
-15.000 -1.0012 0.02896 0.02505 -0.0988 0.9427 0.0057
-14.750 -0.9806 0.02692 0.02284 -0.1021 0.9234 0.0059
-14.500 -0.9692 0.02545 0.02122 -0.1023 0.9037 0.0063
-14.250 -0.9644 0.02422 0.01981 -0.1006 0.8864 0.0063
-14.000 -0.9584 0.02328 0.01875 -0.0983 0.8726 0.0064
-13.750 -0.9549 0.02232 0.01764 -0.0953 0.8603 0.0065
-13.500 -0.9455 0.02170 0.01693 -0.0929 0.8497 0.0067
-13.000 -0.9312 0.02033 0.01533 -0.0868 0.8300 0.0068
-12.750 -0.9195 0.01973 0.01462 -0.0844 0.8219 0.0068
-12.500 -0.9046 0.01917 0.01397 -0.0826 0.8141 0.0072
-12.250 -0.8892 0.01862 0.01332 -0.0807 0.8061 0.0074
-12.000 -0.8723 0.01811 0.01272 -0.0791 0.7982 0.0074
-11.750 -0.8555 0.01756 0.01207 -0.0775 0.7911 0.0076
-11.500 -0.8371 0.01706 0.01149 -0.0760 0.7834 0.0078
-11.250 -0.8190 0.01654 0.01086 -0.0745 0.7762 0.0082
-11.000 -0.7999 0.01602 0.01027 -0.0732 0.7689 0.0085
-10.750 -0.7801 0.01557 0.00975 -0.0719 0.7622 0.0089
-10.500 -0.7589 0.01517 0.00928 -0.0709 0.7553 0.0092
-10.250 -0.7378 0.01477 0.00881 -0.0698 0.7485 0.0098
-10.000 -0.7156 0.01442 0.00838 -0.0689 0.7421 0.0103
-9.750 -0.6936 0.01404 0.00794 -0.0679 0.7353 0.0109
-9.500 -0.6716 0.01365 0.00750 -0.0670 0.7288 0.0121
-9.250 -0.6486 0.01332 0.00712 -0.0661 0.7217 0.0131
-9.000 -0.6257 0.01300 0.00675 -0.0653 0.7154 0.0145
-8.750 -0.6024 0.01267 0.00639 -0.0645 0.7087 0.0164
-8.500 -0.5785 0.01242 0.00608 -0.0638 0.7021 0.0177
-8.250 -0.5547 0.01210 0.00574 -0.0631 0.6961 0.0199
-8.000 -0.5305 0.01185 0.00545 -0.0625 0.6897 0.0218
-7.750 -0.5060 0.01162 0.00517 -0.0619 0.6834 0.0236
-7.500 -0.4816 0.01136 0.00489 -0.0613 0.6764 0.0260
-7.250 -0.4569 0.01116 0.00464 -0.0607 0.6701 0.0283
-7.000 -0.4318 0.01094 0.00440 -0.0602 0.6634 0.0308
-6.750 -0.4072 0.01072 0.00415 -0.0596 0.6566 0.0343
-6.500 -0.3816 0.01054 0.00394 -0.0592 0.6506 0.0369
-6.250 -0.3569 0.01032 0.00371 -0.0586 0.6439 0.0424
-6.000 -0.3317 0.01013 0.00351 -0.0581 0.6381 0.0478
-5.750 -0.3063 0.00994 0.00333 -0.0577 0.6316 0.0549
-5.250 -0.2552 0.00963 0.00301 -0.0568 0.6192 0.0688
-5.000 -0.2295 0.00949 0.00287 -0.0564 0.6128 0.0751
-4.750 -0.2031 0.00940 0.00274 -0.0561 0.6074 0.0791
-4.500 -0.1770 0.00928 0.00262 -0.0558 0.6014 0.0847
-4.000 -0.1241 0.00912 0.00241 -0.0552 0.5905 0.0934
-3.750 -0.0980 0.00902 0.00231 -0.0549 0.5845 0.0998
-3.500 -0.0716 0.00896 0.00222 -0.0546 0.5790 0.1049
-3.250 -0.0448 0.00889 0.00213 -0.0543 0.5738 0.1091
-3.000 -0.0186 0.00881 0.00205 -0.0540 0.5680 0.1159
-2.500 0.0345 0.00867 0.00191 -0.0535 0.5577 0.1293
-2.250 0.0611 0.00863 0.00185 -0.0533 0.5525 0.1351
-2.000 0.0875 0.00857 0.00179 -0.0530 0.5480 0.1430
-1.500 0.1403 0.00845 0.00170 -0.0525 0.5372 0.1658
-1.250 0.1665 0.00839 0.00166 -0.0522 0.5326 0.1797
-1.000 0.1928 0.00832 0.00163 -0.0519 0.5273 0.1968
-0.750 0.2183 0.00823 0.00160 -0.0515 0.5220 0.2218
-0.500 0.2441 0.00816 0.00158 -0.0511 0.5173 0.2456
-0.250 0.2700 0.00807 0.00157 -0.0508 0.5126 0.2730
0.000 0.2953 0.00798 0.00156 -0.0503 0.5077 0.3044
0.250 0.3204 0.00789 0.00156 -0.0499 0.5032 0.3405
0.500 0.3448 0.00774 0.00156 -0.0493 0.4983 0.3941
0.750 0.3685 0.00760 0.00157 -0.0485 0.4928 0.4522
1.000 0.3922 0.00748 0.00159 -0.0478 0.4881 0.5061
1.250 0.4161 0.00736 0.00162 -0.0470 0.4834 0.5584
1.500 0.4390 0.00724 0.00165 -0.0461 0.4786 0.6128
1.750 0.4598 0.00711 0.00170 -0.0446 0.4741 0.6790
2.000 0.4814 0.00698 0.00174 -0.0433 0.4698 0.7360
2.250 0.5025 0.00687 0.00180 -0.0419 0.4646 0.7929
2.500 0.5397 0.00669 0.00194 -0.0440 0.4592 0.8956
2.750 0.6238 0.00679 0.00211 -0.0566 0.4524 0.9399
3.000 0.6674 0.00695 0.00224 -0.0602 0.4469 0.9537
3.250 0.6979 0.00710 0.00237 -0.0608 0.4422 0.9667
3.500 0.7256 0.00723 0.00250 -0.0608 0.4373 0.9765
3.750 0.7605 0.00737 0.00261 -0.0625 0.4318 0.9781
4.000 0.7948 0.00750 0.00272 -0.0641 0.4268 0.9802
4.250 0.8277 0.00761 0.00283 -0.0654 0.4220 0.9827
4.500 0.8576 0.00775 0.00296 -0.0660 0.4172 0.9861
4.750 0.8914 0.00788 0.00308 -0.0676 0.4128 0.9878
5.000 0.9276 0.00800 0.00320 -0.0696 0.4077 0.9894
5.250 0.9621 0.00814 0.00333 -0.0713 0.4028 0.9913
5.500 0.9946 0.00829 0.00347 -0.0726 0.3979 0.9932
5.750 1.0259 0.00841 0.00362 -0.0736 0.3934 0.9949
6.000 1.0567 0.00856 0.00376 -0.0745 0.3881 0.9966
6.250 1.0882 0.00872 0.00392 -0.0756 0.3829 0.9981
6.500 1.1199 0.00888 0.00408 -0.0768 0.3748 0.9993
6.750 1.1480 0.00911 0.00427 -0.0773 0.3632 1.0000
7.000 1.1666 0.00936 0.00447 -0.0757 0.3497 1.0000
7.250 1.1847 0.00964 0.00470 -0.0741 0.3363 1.0000
7.500 1.1983 0.01009 0.00503 -0.0717 0.3115 1.0000
7.750 1.2089 0.01064 0.00542 -0.0687 0.2821 1.0000
8.000 1.2135 0.01137 0.00594 -0.0648 0.2435 1.0000
8.250 1.2022 0.01255 0.00680 -0.0580 0.1900 1.0000
8.500 1.1936 0.01332 0.00743 -0.0516 0.1616 1.0000
8.750 1.1881 0.01439 0.00832 -0.0466 0.1289 1.0000
9.000 1.1888 0.01550 0.00929 -0.0430 0.1011 1.0000
9.250 1.1870 0.01694 0.01056 -0.0395 0.0686 1.0000
9.500 1.1992 0.01774 0.01136 -0.0379 0.0610 1.0000
9.750 1.2001 0.01930 0.01279 -0.0354 0.0379 1.0000
10.000 1.2063 0.02063 0.01407 -0.0336 0.0259 1.0000
10.250 1.2154 0.02184 0.01526 -0.0322 0.0193 1.0000
10.500 1.2249 0.02308 0.01651 -0.0309 0.0148 1.0000
10.750 1.2342 0.02436 0.01780 -0.0298 0.0118 1.0000
11.000 1.2451 0.02557 0.01905 -0.0288 0.0105 1.0000
11.250 1.2564 0.02678 0.02030 -0.0280 0.0101 1.0000
11.500 1.2651 0.02823 0.02177 -0.0271 0.0089 1.0000
11.750 1.2748 0.02963 0.02322 -0.0263 0.0082 1.0000
12.000 1.2836 0.03114 0.02477 -0.0255 0.0078 1.0000
12.250 1.2909 0.03280 0.02647 -0.0248 0.0071 1.0000
12.500 1.2986 0.03445 0.02816 -0.0241 0.0070 1.0000
12.750 1.3046 0.03632 0.03008 -0.0234 0.0064 1.0000
13.000 1.3116 0.03814 0.03196 -0.0229 0.0064 1.0000
13.250 1.3186 0.04000 0.03388 -0.0224 0.0060 1.0000
13.500 1.3245 0.04201 0.03595 -0.0220 0.0060 1.0000
13.750 1.3294 0.04415 0.03815 -0.0216 0.0057 1.0000
14.000 1.3322 0.04656 0.04060 -0.0212 0.0052 1.0000
14.250 1.3378 0.04871 0.04281 -0.0210 0.0053 1.0000
14.500 1.3394 0.05130 0.04546 -0.0207 0.0050 1.0000
14.750 1.3408 0.05399 0.04820 -0.0206 0.0046 1.0000
15.000 1.3415 0.05680 0.05109 -0.0205 0.0046 1.0000
15.250 1.3471 0.05909 0.05344 -0.0205 0.0045 1.0000
15.500 1.3496 0.06171 0.05613 -0.0205 0.0044 1.0000
15.750 1.3521 0.06440 0.05888 -0.0206 0.0043 1.0000
16.000 1.3504 0.06766 0.06222 -0.0207 0.0043 1.0000
16.250 1.3536 0.07033 0.06495 -0.0209 0.0042 1.0000
16.500 1.3562 0.07310 0.06777 -0.0212 0.0040 1.0000
16.750 1.3534 0.07657 0.07132 -0.0215 0.0039 1.0000
17.000 1.3533 0.07975 0.07458 -0.0219 0.0038 1.0000
17.250 1.3528 0.08301 0.07790 -0.0224 0.0037 1.0000
17.500 1.3535 0.08616 0.08112 -0.0229 0.0038 1.0000
17.750 1.3524 0.08953 0.08455 -0.0235 0.0036 1.0000
18.000 1.3519 0.09287 0.08795 -0.0241 0.0035 1.0000
18.250 1.3513 0.09624 0.09138 -0.0248 0.0033 1.0000
18.500 1.3505 0.09968 0.09490 -0.0256 0.0034 1.0000
18.750 1.3464 0.10366 0.09896 -0.0265 0.0034 1.0000
19.000 1.3420 0.10769 0.10305 -0.0275 0.0033 1.0000
19.250 1.3381 0.11164 0.10707 -0.0286 0.0030 1.0000
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