WORTMANN FX 76-120 (fx76120-il) Xfoil prediction polar at RE=100,000 Ncrit=5
| Details | Polar file |
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Airfoil: WORTMANN FX 76-120 (fx76120-il) Reynolds number: 100,000 Max Cl/Cd: 37.79 at α=6.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx76120-il-100000-n5.txt Download as CSV file: xf-fx76120-il-100000-n5.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 76-120
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.100 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-14.750 -0.8386 0.09882 0.09284 -0.0229 1.0000 0.0431
-14.500 -0.8932 0.08426 0.07805 -0.0327 1.0000 0.0425
-14.250 -0.9262 0.07505 0.06861 -0.0387 1.0000 0.0423
-14.000 -0.9516 0.06793 0.06125 -0.0429 1.0000 0.0424
-13.750 -0.9707 0.06234 0.05542 -0.0457 1.0000 0.0426
-13.500 -0.9868 0.05762 0.05046 -0.0473 1.0000 0.0430
-13.250 -1.0006 0.05359 0.04615 -0.0480 1.0000 0.0436
-13.000 -1.0101 0.05026 0.04254 -0.0478 1.0000 0.0441
-12.750 -1.0107 0.04782 0.04003 -0.0470 1.0000 0.0450
-12.500 -1.0087 0.04586 0.03804 -0.0461 1.0000 0.0460
-12.250 -1.0079 0.04399 0.03609 -0.0447 1.0000 0.0472
-12.000 -1.0072 0.04214 0.03408 -0.0430 1.0000 0.0486
-11.750 -1.0053 0.04033 0.03209 -0.0410 1.0000 0.0499
-11.500 -1.0025 0.03859 0.03012 -0.0388 1.0000 0.0514
-11.250 -0.9973 0.03699 0.02835 -0.0364 1.0000 0.0527
-11.000 -0.9912 0.03570 0.02708 -0.0341 1.0000 0.0544
-10.750 -0.9841 0.03451 0.02585 -0.0317 1.0000 0.0563
-10.500 -0.9747 0.03329 0.02450 -0.0295 1.0000 0.0586
-10.250 -0.9634 0.03205 0.02305 -0.0274 1.0000 0.0610
-10.000 -0.9528 0.03081 0.02180 -0.0253 1.0000 0.0633
-9.750 -0.9415 0.02978 0.02074 -0.0232 1.0000 0.0662
-9.500 -0.9286 0.02878 0.01963 -0.0211 1.0000 0.0696
-9.250 -0.9156 0.02773 0.01851 -0.0190 1.0000 0.0732
-9.000 -0.9032 0.02677 0.01754 -0.0168 1.0000 0.0768
-8.750 -0.8890 0.02590 0.01657 -0.0147 1.0000 0.0818
-8.500 -0.8757 0.02499 0.01567 -0.0126 1.0000 0.0869
-8.250 -0.8610 0.02419 0.01483 -0.0105 1.0000 0.0933
-8.000 -0.8466 0.02338 0.01404 -0.0084 1.0000 0.1005
-7.750 -0.8308 0.02267 0.01328 -0.0065 1.0000 0.1099
-7.500 -0.8153 0.02198 0.01261 -0.0045 1.0000 0.1202
-7.250 -0.7993 0.02134 0.01202 -0.0025 1.0000 0.1322
-7.000 -0.7827 0.02078 0.01147 -0.0007 1.0000 0.1456
-6.750 -0.7657 0.02026 0.01096 0.0012 1.0000 0.1597
-6.500 -0.7483 0.01980 0.01051 0.0030 1.0000 0.1743
-6.250 -0.7307 0.01937 0.01008 0.0048 1.0000 0.1889
-6.000 -0.7130 0.01897 0.00968 0.0065 1.0000 0.2036
-5.750 -0.6951 0.01859 0.00930 0.0083 1.0000 0.2183
-5.500 -0.6770 0.01823 0.00896 0.0100 1.0000 0.2331
-5.250 -0.6588 0.01789 0.00863 0.0117 1.0000 0.2481
-5.000 -0.6405 0.01756 0.00831 0.0134 1.0000 0.2633
-4.750 -0.6221 0.01725 0.00802 0.0151 1.0000 0.2789
-4.500 -0.6037 0.01694 0.00775 0.0168 1.0000 0.2950
-4.250 -0.5854 0.01664 0.00751 0.0184 1.0000 0.3119
-4.000 -0.5669 0.01636 0.00729 0.0201 1.0000 0.3297
-3.750 -0.5484 0.01610 0.00711 0.0217 1.0000 0.3485
-3.500 -0.5299 0.01586 0.00695 0.0233 1.0000 0.3687
-3.250 -0.5048 0.01564 0.00680 0.0236 0.9977 0.3937
-3.000 -0.4681 0.01539 0.00670 0.0215 0.9904 0.4253
-2.750 -0.4308 0.01515 0.00661 0.0195 0.9825 0.4603
-2.500 -0.3939 0.01488 0.00653 0.0176 0.9739 0.4986
-2.250 -0.3575 0.01464 0.00647 0.0159 0.9652 0.5410
-2.000 -0.3193 0.01442 0.00644 0.0140 0.9573 0.5855
-1.750 -0.2852 0.01422 0.00641 0.0130 0.9474 0.6287
-1.500 -0.2470 0.01405 0.00643 0.0114 0.9388 0.6725
-1.250 -0.2055 0.01392 0.00644 0.0092 0.9297 0.7151
-1.000 -0.1657 0.01382 0.00648 0.0076 0.9181 0.7533
-0.750 -0.1236 0.01376 0.00650 0.0055 0.9064 0.7866
-0.500 -0.0802 0.01371 0.00650 0.0032 0.8940 0.8147
-0.250 -0.0388 0.01370 0.00653 0.0014 0.8789 0.8390
0.000 -0.0001 0.01369 0.00652 0.0000 0.8608 0.8610
0.250 0.0387 0.01370 0.00653 -0.0014 0.8390 0.8788
0.500 0.0801 0.01371 0.00650 -0.0032 0.8150 0.8939
0.750 0.1236 0.01376 0.00649 -0.0055 0.7862 0.9064
1.000 0.1658 0.01382 0.00648 -0.0076 0.7531 0.9182
1.250 0.2054 0.01391 0.00644 -0.0092 0.7155 0.9297
1.500 0.2470 0.01405 0.00643 -0.0114 0.6733 0.9388
1.750 0.2853 0.01422 0.00641 -0.0130 0.6291 0.9475
2.000 0.3195 0.01442 0.00644 -0.0140 0.5855 0.9573
2.250 0.3575 0.01464 0.00647 -0.0159 0.5408 0.9652
2.500 0.3940 0.01488 0.00653 -0.0176 0.4985 0.9740
2.750 0.4309 0.01515 0.00660 -0.0195 0.4600 0.9826
3.000 0.4682 0.01539 0.00670 -0.0215 0.4251 0.9905
3.250 0.5049 0.01563 0.00681 -0.0236 0.3938 0.9977
3.500 0.5298 0.01586 0.00695 -0.0233 0.3692 1.0000
3.750 0.5484 0.01610 0.00711 -0.0217 0.3485 1.0000
4.000 0.5669 0.01636 0.00729 -0.0201 0.3297 1.0000
4.250 0.5853 0.01664 0.00751 -0.0184 0.3119 1.0000
4.500 0.6037 0.01694 0.00775 -0.0168 0.2952 1.0000
4.750 0.6221 0.01725 0.00802 -0.0151 0.2789 1.0000
5.000 0.6405 0.01756 0.00831 -0.0134 0.2634 1.0000
5.250 0.6588 0.01789 0.00863 -0.0117 0.2483 1.0000
5.500 0.6770 0.01823 0.00895 -0.0100 0.2333 1.0000
5.750 0.6950 0.01859 0.00930 -0.0083 0.2183 1.0000
6.000 0.7129 0.01897 0.00968 -0.0065 0.2036 1.0000
6.250 0.7307 0.01937 0.01008 -0.0048 0.1891 1.0000
6.500 0.7483 0.01980 0.01051 -0.0030 0.1747 1.0000
6.750 0.7656 0.02027 0.01096 -0.0012 0.1600 1.0000
7.000 0.7827 0.02078 0.01147 0.0007 0.1456 1.0000
7.250 0.7993 0.02134 0.01202 0.0025 0.1322 1.0000
7.500 0.8153 0.02198 0.01261 0.0045 0.1204 1.0000
7.750 0.8308 0.02266 0.01327 0.0065 0.1098 1.0000
8.000 0.8467 0.02337 0.01402 0.0084 0.1006 1.0000
8.250 0.8610 0.02419 0.01482 0.0105 0.0934 1.0000
8.500 0.8758 0.02499 0.01568 0.0126 0.0870 1.0000
8.750 0.8890 0.02590 0.01658 0.0148 0.0818 1.0000
9.000 0.9033 0.02677 0.01754 0.0168 0.0768 1.0000
9.250 0.9155 0.02774 0.01850 0.0190 0.0730 1.0000
9.500 0.9287 0.02877 0.01963 0.0211 0.0696 1.0000
9.750 0.9416 0.02978 0.02074 0.0231 0.0661 1.0000
10.000 0.9528 0.03080 0.02178 0.0253 0.0632 1.0000
10.250 0.9636 0.03205 0.02305 0.0274 0.0610 1.0000
10.500 0.9748 0.03328 0.02449 0.0295 0.0585 1.0000
10.750 0.9845 0.03453 0.02587 0.0316 0.0563 1.0000
11.000 0.9915 0.03570 0.02709 0.0341 0.0543 1.0000
11.250 0.9981 0.03700 0.02837 0.0364 0.0528 1.0000
11.500 1.0027 0.03860 0.03014 0.0387 0.0513 1.0000
11.750 1.0060 0.04032 0.03209 0.0409 0.0499 1.0000
12.000 1.0073 0.04211 0.03407 0.0430 0.0484 1.0000
12.250 1.0083 0.04391 0.03600 0.0446 0.0470 1.0000
12.500 1.0094 0.04581 0.03798 0.0460 0.0459 1.0000
12.750 1.0116 0.04777 0.03998 0.0469 0.0450 1.0000
13.000 1.0108 0.05025 0.04253 0.0477 0.0441 1.0000
13.250 1.0006 0.05366 0.04623 0.0479 0.0435 1.0000
13.500 0.9877 0.05763 0.05046 0.0472 0.0430 1.0000
13.750 0.9718 0.06232 0.05540 0.0456 0.0426 1.0000
14.000 0.9525 0.06795 0.06127 0.0428 0.0423 1.0000
14.250 0.9275 0.07502 0.06857 0.0386 0.0422 1.0000
14.500 0.8929 0.08455 0.07835 0.0322 0.0424 1.0000
14.750 0.8369 0.09950 0.09353 0.0223 0.0431 1.0000
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