FX 79-W-151 A (fx79w151a-il) Xfoil prediction polar at RE=100,000 Ncrit=9
| Details | Polar file |
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Airfoil: FX 79-W-151 A (fx79w151a-il) Reynolds number: 100,000 Max Cl/Cd: 35.64 at α=12° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx79w151a-il-100000.txt Download as CSV file: xf-fx79w151a-il-100000.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 = 0.100 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-10.000 -0.3741 0.10933 0.10528 -0.0404 1.0000 0.1354
-9.750 -0.4023 0.10570 0.10175 -0.0472 0.9946 0.1362
-9.500 -0.4804 0.07478 0.07071 -0.0700 0.9843 0.0793
-9.250 -0.4846 0.06848 0.06429 -0.0740 0.9747 0.0786
-9.000 -0.4945 0.06165 0.05722 -0.0778 0.9634 0.0781
-8.750 -0.5064 0.05536 0.05055 -0.0794 0.9523 0.0779
-8.500 -0.5127 0.04932 0.04392 -0.0800 0.9430 0.0784
-8.250 -0.4903 0.04792 0.04258 -0.0807 0.9343 0.0835
-8.000 -0.4768 0.04507 0.03937 -0.0808 0.9261 0.0880
-7.750 -0.4730 0.04109 0.03460 -0.0793 0.9172 0.0917
-7.500 -0.4594 0.03927 0.03265 -0.0781 0.9078 0.0962
-7.250 -0.4305 0.03752 0.03057 -0.0790 0.9020 0.1035
-7.000 -0.4244 0.03572 0.02830 -0.0759 0.8916 0.1084
-6.750 -0.3894 0.03447 0.02698 -0.0775 0.8866 0.1172
-6.500 -0.3802 0.03317 0.02527 -0.0746 0.8764 0.1232
-6.250 -0.3471 0.03213 0.02409 -0.0756 0.8714 0.1337
-6.000 -0.3337 0.03117 0.02297 -0.0734 0.8617 0.1402
-5.750 -0.3038 0.03024 0.02170 -0.0736 0.8564 0.1522
-5.500 -0.2865 0.02967 0.02120 -0.0720 0.8473 0.1604
-5.250 -0.2566 0.02876 0.02014 -0.0723 0.8417 0.1725
-5.000 -0.2391 0.02839 0.01951 -0.0704 0.8331 0.1824
-4.750 -0.2099 0.02762 0.01874 -0.0706 0.8271 0.1945
-4.500 -0.1833 0.02700 0.01810 -0.0704 0.8210 0.2060
-4.250 -0.1621 0.02659 0.01763 -0.0693 0.8129 0.2174
-4.000 -0.1270 0.02578 0.01676 -0.0701 0.8091 0.2324
-3.750 -0.1138 0.02579 0.01670 -0.0678 0.7989 0.2433
-3.500 -0.0805 0.02502 0.01598 -0.0684 0.7947 0.2614
-3.250 -0.0651 0.02496 0.01598 -0.0665 0.7856 0.2767
-3.000 -0.0357 0.02428 0.01543 -0.0665 0.7805 0.3017
-2.750 -0.0172 0.02400 0.01533 -0.0649 0.7730 0.3317
-2.500 0.0041 0.02340 0.01505 -0.0635 0.7665 0.3848
-2.250 0.0289 0.02215 0.01459 -0.0621 0.7631 0.5259
-2.000 0.0509 0.02188 0.01525 -0.0605 0.7538 0.7382
-1.750 0.1551 0.02171 0.01515 -0.0719 0.7517 0.8908
-1.500 0.2370 0.02172 0.01486 -0.0800 0.7487 0.9304
-1.250 0.3064 0.02207 0.01500 -0.0876 0.7415 0.9589
-1.000 0.3864 0.02182 0.01452 -0.0971 0.7363 0.9840
-0.750 0.4562 0.02115 0.01360 -0.1051 0.7322 1.0000
-0.500 0.4661 0.02157 0.01398 -0.1033 0.7225 1.0000
-0.250 0.4858 0.02137 0.01364 -0.1019 0.7175 1.0000
0.000 0.4961 0.02190 0.01414 -0.0999 0.7084 1.0000
0.250 0.5169 0.02176 0.01388 -0.0986 0.7032 1.0000
0.500 0.5281 0.02232 0.01441 -0.0966 0.6948 1.0000
0.750 0.5485 0.02230 0.01429 -0.0953 0.6891 1.0000
1.000 0.5630 0.02272 0.01466 -0.0934 0.6820 1.0000
1.250 0.5806 0.02296 0.01485 -0.0918 0.6753 1.0000
1.500 0.6068 0.02277 0.01454 -0.0911 0.6714 1.0000
1.750 0.6128 0.02374 0.01554 -0.0883 0.6618 1.0000
2.000 0.6391 0.02358 0.01529 -0.0877 0.6576 1.0000
2.250 0.6464 0.02454 0.01626 -0.0850 0.6489 1.0000
2.500 0.6702 0.02459 0.01627 -0.0841 0.6440 1.0000
2.750 0.6923 0.02480 0.01642 -0.0830 0.6391 1.0000
3.000 0.7000 0.02574 0.01739 -0.0803 0.6307 1.0000
3.250 0.7304 0.02550 0.01708 -0.0802 0.6270 1.0000
3.500 0.7301 0.02695 0.01860 -0.0766 0.6178 1.0000
3.750 0.7567 0.02699 0.01860 -0.0761 0.6136 1.0000
4.000 0.7906 0.02668 0.01824 -0.0765 0.6107 1.0000
4.250 0.7802 0.02866 0.02031 -0.0718 0.6001 1.0000
4.500 0.8145 0.02832 0.01995 -0.0722 0.5970 1.0000
4.750 0.7990 0.03071 0.02243 -0.0670 0.5870 1.0000
5.000 0.8286 0.03067 0.02238 -0.0669 0.5833 1.0000
5.250 0.8678 0.03014 0.02184 -0.0679 0.5809 1.0000
5.500 0.8358 0.03347 0.02525 -0.0610 0.5692 1.0000
5.750 0.8757 0.03289 0.02471 -0.0621 0.5669 1.0000
6.000 0.7199 0.04472 0.03649 -0.0458 0.5420 1.0000
6.250 0.7468 0.04484 0.03665 -0.0453 0.5385 1.0000
6.500 0.7863 0.04396 0.03583 -0.0455 0.5369 1.0000
6.750 0.8323 0.04265 0.03459 -0.0462 0.5360 1.0000
7.000 0.8895 0.04092 0.03296 -0.0484 0.5353 1.0000
7.250 0.7143 0.05763 0.04952 -0.0382 0.5086 1.0000
7.500 0.7508 0.05711 0.04906 -0.0381 0.5061 1.0000
7.750 0.7108 0.06331 0.05526 -0.0362 0.4954 1.0000
8.000 0.7409 0.06339 0.05540 -0.0359 0.4919 1.0000
8.250 0.7215 0.06789 0.05993 -0.0347 0.4835 1.0000
8.500 0.7373 0.06924 0.06134 -0.0342 0.4783 1.0000
8.750 0.7775 0.06836 0.06057 -0.0339 0.4756 1.0000
9.000 0.7404 0.07461 0.06683 -0.0330 0.4652 1.0000
9.250 0.7794 0.07372 0.06603 -0.0325 0.4613 1.0000
9.500 0.7564 0.07875 0.07109 -0.0319 0.4516 1.0000
9.750 0.7910 0.07816 0.07061 -0.0313 0.4468 1.0000
10.000 0.8425 0.07590 0.06851 -0.0307 0.4445 1.0000
10.250 0.8094 0.08188 0.07451 -0.0302 0.4320 1.0000
10.500 0.7986 0.08586 0.07853 -0.0299 0.4224 1.0000
10.750 0.8348 0.08477 0.07757 -0.0290 0.4169 1.0000
11.000 0.8902 0.08155 0.07453 -0.0278 0.4145 1.0000
11.250 0.8658 0.08688 0.07989 -0.0276 0.4015 1.0000
11.500 0.8550 0.09078 0.08387 -0.0273 0.3897 1.0000
11.750 0.9103 0.08683 0.08012 -0.0256 0.3860 1.0000
12.000 1.2922 0.03626 0.03009 -0.0193 0.3630 1.0000
12.250 1.2824 0.03807 0.03198 -0.0166 0.3463 1.0000
12.500 1.2731 0.03999 0.03390 -0.0143 0.3245 1.0000
12.750 1.2499 0.04383 0.03784 -0.0124 0.3028 1.0000
13.000 1.2285 0.04784 0.04182 -0.0110 0.2730 1.0000
13.250 1.2075 0.05206 0.04581 -0.0099 0.2299 1.0000
13.500 1.1792 0.05738 0.05070 -0.0090 0.1841 1.0000
13.750 1.1485 0.06352 0.05651 -0.0088 0.1483 1.0000
14.000 1.1204 0.06977 0.06249 -0.0090 0.1212 1.0000
14.250 1.0985 0.07547 0.06799 -0.0094 0.1034 1.0000
14.500 1.0774 0.08118 0.07345 -0.0097 0.0882 1.0000
14.750 1.0652 0.08565 0.07774 -0.0096 0.0761 1.0000
15.000 1.0637 0.08866 0.08070 -0.0092 0.0663 1.0000
15.250 1.0701 0.09042 0.08242 -0.0082 0.0589 1.0000
15.500 1.0888 0.08974 0.08147 -0.0056 0.0529 1.0000
15.750 1.1060 0.09021 0.08209 -0.0039 0.0495 1.0000
16.000 1.1208 0.09103 0.08288 -0.0026 0.0460 1.0000
16.250 1.1543 0.08928 0.08097 0.0010 0.0427 1.0000
16.500 1.1615 0.09172 0.08364 0.0014 0.0412 1.0000
16.750 1.1741 0.09363 0.08576 0.0024 0.0401 1.0000
17.000 1.1823 0.09623 0.08856 0.0029 0.0393 1.0000
17.250 1.1857 0.09950 0.09206 0.0031 0.0387 1.0000
17.500 1.1842 0.10340 0.09620 0.0026 0.0388 1.0000
17.750 1.1764 0.10817 0.10125 0.0016 0.0387 1.0000
18.000 1.1641 0.11369 0.10704 -0.0001 0.0386 1.0000
18.250 1.1480 0.11988 0.11350 -0.0024 0.0387 1.0000
18.500 1.1300 0.12663 0.12051 -0.0054 0.0393 1.0000
18.750 1.1084 0.13431 0.12840 -0.0093 0.0398 1.0000
19.000 1.0827 0.14320 0.13753 -0.0141 0.0403 1.0000
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