WORTMANN FX 76-120 (fx76120-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: WORTMANN FX 76-120 (fx76120-il) Reynolds number: 1,000,000 Max Cl/Cd: 78.92 at α=8.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx76120-il-1000000.txt Download as CSV file: xf-fx76120-il-1000000.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 = 1.000 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-18.250 -1.2222 0.08724 0.08383 -0.0200 1.0000 0.0144
-18.000 -1.2436 0.08021 0.07669 -0.0236 1.0000 0.0144
-17.750 -1.2658 0.07314 0.06949 -0.0272 1.0000 0.0145
-17.500 -1.2813 0.06716 0.06339 -0.0302 1.0000 0.0146
-17.250 -1.2999 0.06081 0.05691 -0.0334 1.0000 0.0146
-17.000 -1.3192 0.05447 0.05043 -0.0367 1.0000 0.0145
-16.750 -1.3237 0.05036 0.04620 -0.0388 1.0000 0.0147
-16.500 -1.3420 0.04462 0.04031 -0.0415 1.0000 0.0148
-16.250 -1.3508 0.04045 0.03603 -0.0431 1.0000 0.0150
-16.000 -1.3622 0.03637 0.03182 -0.0442 1.0000 0.0152
-15.750 -1.3623 0.03382 0.02920 -0.0443 1.0000 0.0156
-15.500 -1.3608 0.03164 0.02693 -0.0440 1.0000 0.0159
-15.250 -1.3551 0.02998 0.02521 -0.0434 1.0000 0.0163
-15.000 -1.3504 0.02837 0.02351 -0.0425 1.0000 0.0166
-14.750 -1.3422 0.02712 0.02219 -0.0414 1.0000 0.0170
-14.500 -1.3318 0.02610 0.02111 -0.0402 1.0000 0.0175
-14.250 -1.3201 0.02522 0.02016 -0.0389 1.0000 0.0178
-14.000 -1.3122 0.02416 0.01901 -0.0372 1.0000 0.0180
-13.750 -1.3119 0.02275 0.01751 -0.0344 1.0000 0.0186
-13.500 -1.3049 0.02179 0.01651 -0.0319 1.0000 0.0191
-13.250 -1.2932 0.02115 0.01584 -0.0298 1.0000 0.0198
-13.000 -1.2816 0.02055 0.01519 -0.0275 1.0000 0.0203
-12.750 -1.2695 0.02003 0.01462 -0.0251 1.0000 0.0209
-12.500 -1.2572 0.01952 0.01405 -0.0227 1.0000 0.0214
-12.250 -1.2410 0.01908 0.01355 -0.0209 1.0000 0.0218
-12.000 -1.2311 0.01820 0.01263 -0.0182 1.0000 0.0228
-11.750 -1.2158 0.01765 0.01206 -0.0162 1.0000 0.0236
-11.500 -1.1985 0.01721 0.01159 -0.0145 1.0000 0.0244
-11.250 -1.1807 0.01681 0.01114 -0.0128 1.0000 0.0252
-11.000 -1.1613 0.01651 0.01081 -0.0114 1.0000 0.0260
-10.750 -1.1464 0.01592 0.01018 -0.0092 1.0000 0.0270
-10.500 -1.1302 0.01543 0.00968 -0.0072 1.0000 0.0283
-10.250 -1.1122 0.01506 0.00929 -0.0054 1.0000 0.0294
-10.000 -1.0940 0.01474 0.00894 -0.0036 1.0000 0.0305
-9.750 -1.0752 0.01447 0.00864 -0.0019 1.0000 0.0313
-9.500 -1.0606 0.01396 0.00811 0.0005 1.0000 0.0332
-9.250 -1.0440 0.01360 0.00775 0.0026 1.0000 0.0348
-9.000 -1.0267 0.01331 0.00744 0.0046 1.0000 0.0361
-8.750 -1.0089 0.01307 0.00716 0.0066 1.0000 0.0372
-8.500 -0.9935 0.01266 0.00675 0.0089 1.0000 0.0397
-8.250 -0.9753 0.01236 0.00645 0.0107 0.9999 0.0419
-8.000 -0.9414 0.01209 0.00615 0.0093 0.9986 0.0441
-7.750 -0.9080 0.01166 0.00576 0.0078 0.9967 0.0489
-7.500 -0.8733 0.01139 0.00549 0.0063 0.9951 0.0527
-7.250 -0.8422 0.01097 0.00512 0.0054 0.9928 0.0599
-7.000 -0.8101 0.01061 0.00481 0.0043 0.9907 0.0685
-6.750 -0.7774 0.01024 0.00451 0.0031 0.9890 0.0804
-6.500 -0.7439 0.00989 0.00423 0.0018 0.9877 0.0946
-6.250 -0.7141 0.00955 0.00398 0.0012 0.9846 0.1102
-6.000 -0.6819 0.00921 0.00374 0.0002 0.9824 0.1285
-5.750 -0.6476 0.00892 0.00353 -0.0013 0.9807 0.1448
-5.500 -0.6111 0.00865 0.00332 -0.0032 0.9793 0.1594
-5.250 -0.5795 0.00840 0.00313 -0.0039 0.9747 0.1727
-5.000 -0.5445 0.00817 0.00294 -0.0054 0.9718 0.1856
-4.750 -0.5079 0.00796 0.00278 -0.0073 0.9698 0.1984
-4.500 -0.4758 0.00775 0.00263 -0.0082 0.9657 0.2108
-4.250 -0.4426 0.00754 0.00247 -0.0093 0.9607 0.2244
-4.000 -0.4052 0.00732 0.00230 -0.0113 0.9563 0.2394
-3.750 -0.3756 0.00713 0.00217 -0.0116 0.9467 0.2559
-3.500 -0.3450 0.00695 0.00205 -0.0121 0.9376 0.2742
-3.250 -0.3142 0.00678 0.00192 -0.0126 0.9282 0.2929
-3.000 -0.2880 0.00663 0.00182 -0.0121 0.9169 0.3118
-2.750 -0.2613 0.00646 0.00172 -0.0117 0.9046 0.3345
-2.500 -0.2350 0.00631 0.00162 -0.0112 0.8904 0.3592
-2.250 -0.2097 0.00617 0.00153 -0.0105 0.8747 0.3847
-2.000 -0.1845 0.00605 0.00146 -0.0097 0.8582 0.4105
-1.750 -0.1601 0.00593 0.00138 -0.0088 0.8395 0.4368
-1.500 -0.1360 0.00583 0.00131 -0.0078 0.8190 0.4647
-1.000 -0.0899 0.00566 0.00120 -0.0054 0.7683 0.5289
-0.750 -0.0673 0.00561 0.00117 -0.0040 0.7411 0.5618
-0.500 -0.0448 0.00559 0.00114 -0.0027 0.7120 0.5921
-0.250 -0.0222 0.00556 0.00112 -0.0014 0.6828 0.6211
0.000 0.0001 0.00556 0.00112 0.0000 0.6525 0.6515
0.250 0.0222 0.00556 0.00112 0.0014 0.6213 0.6828
0.500 0.0448 0.00559 0.00114 0.0027 0.5920 0.7119
0.750 0.0674 0.00562 0.00117 0.0040 0.5615 0.7402
1.000 0.0899 0.00567 0.00120 0.0054 0.5283 0.7682
1.250 0.1128 0.00575 0.00125 0.0066 0.4950 0.7945
1.500 0.1361 0.00582 0.00131 0.0078 0.4655 0.8187
1.750 0.1600 0.00593 0.00138 0.0088 0.4362 0.8398
2.000 0.1845 0.00605 0.00146 0.0097 0.4106 0.8588
2.250 0.2096 0.00617 0.00153 0.0105 0.3844 0.8750
2.500 0.2351 0.00632 0.00162 0.0112 0.3592 0.8895
2.750 0.2613 0.00646 0.00172 0.0117 0.3341 0.9046
3.000 0.2879 0.00663 0.00182 0.0121 0.3111 0.9170
3.250 0.3141 0.00678 0.00192 0.0126 0.2925 0.9281
3.500 0.3449 0.00695 0.00205 0.0121 0.2737 0.9375
3.750 0.3755 0.00713 0.00217 0.0116 0.2558 0.9465
4.000 0.4053 0.00732 0.00230 0.0113 0.2399 0.9562
4.250 0.4427 0.00754 0.00247 0.0092 0.2245 0.9607
4.500 0.4758 0.00775 0.00263 0.0082 0.2109 0.9656
4.750 0.5079 0.00797 0.00278 0.0073 0.1971 0.9698
5.000 0.5444 0.00817 0.00294 0.0055 0.1851 0.9717
5.250 0.5795 0.00839 0.00313 0.0039 0.1732 0.9747
5.500 0.6112 0.00864 0.00332 0.0032 0.1604 0.9794
5.750 0.6479 0.00892 0.00353 0.0012 0.1447 0.9808
6.000 0.6818 0.00922 0.00374 -0.0002 0.1277 0.9824
6.250 0.7142 0.00955 0.00398 -0.0012 0.1100 0.9846
6.500 0.7439 0.00989 0.00423 -0.0017 0.0948 0.9877
6.750 0.7775 0.01024 0.00451 -0.0031 0.0805 0.9890
7.000 0.8102 0.01061 0.00481 -0.0044 0.0687 0.9907
7.250 0.8423 0.01097 0.00512 -0.0054 0.0599 0.9928
7.500 0.8735 0.01138 0.00547 -0.0063 0.0528 0.9951
7.750 0.9081 0.01166 0.00576 -0.0079 0.0487 0.9967
8.000 0.9415 0.01209 0.00615 -0.0093 0.0441 0.9986
8.250 0.9755 0.01236 0.00644 -0.0107 0.0418 0.9999
8.500 0.9933 0.01267 0.00675 -0.0089 0.0395 1.0000
8.750 1.0088 0.01308 0.00717 -0.0065 0.0372 1.0000
9.000 1.0267 0.01331 0.00743 -0.0046 0.0361 1.0000
9.250 1.0440 0.01360 0.00774 -0.0026 0.0346 1.0000
9.500 1.0607 0.01395 0.00810 -0.0005 0.0331 1.0000
9.750 1.0752 0.01447 0.00864 0.0019 0.0313 1.0000
10.000 1.0940 0.01474 0.00894 0.0036 0.0304 1.0000
10.250 1.1122 0.01506 0.00930 0.0054 0.0294 1.0000
10.500 1.1302 0.01543 0.00968 0.0071 0.0282 1.0000
10.750 1.1465 0.01592 0.01018 0.0091 0.0272 1.0000
11.000 1.1610 0.01653 0.01083 0.0114 0.0260 1.0000
11.250 1.1805 0.01682 0.01116 0.0128 0.0253 1.0000
11.500 1.1985 0.01722 0.01160 0.0145 0.0244 1.0000
11.750 1.2156 0.01767 0.01208 0.0162 0.0237 1.0000
12.000 1.2310 0.01822 0.01265 0.0182 0.0228 1.0000
12.250 1.2407 0.01910 0.01358 0.0209 0.0218 1.0000
12.500 1.2572 0.01954 0.01407 0.0227 0.0213 1.0000
12.750 1.2704 0.02001 0.01459 0.0250 0.0209 1.0000
13.000 1.2812 0.02059 0.01523 0.0276 0.0203 1.0000
13.250 1.2936 0.02115 0.01584 0.0298 0.0198 1.0000
13.500 1.3052 0.02180 0.01652 0.0318 0.0191 1.0000
13.750 1.3127 0.02273 0.01749 0.0342 0.0184 1.0000
14.000 1.3149 0.02404 0.01888 0.0368 0.0179 1.0000
14.250 1.3264 0.02487 0.01978 0.0383 0.0177 1.0000
14.500 1.3373 0.02579 0.02078 0.0397 0.0173 1.0000
14.750 1.3452 0.02697 0.02204 0.0411 0.0168 1.0000
15.000 1.3515 0.02835 0.02350 0.0423 0.0166 1.0000
15.250 1.3579 0.02983 0.02505 0.0432 0.0163 1.0000
15.500 1.3623 0.03160 0.02689 0.0439 0.0159 1.0000
15.750 1.3649 0.03367 0.02904 0.0442 0.0157 1.0000
16.000 1.3610 0.03663 0.03209 0.0439 0.0153 1.0000
16.250 1.3553 0.04007 0.03564 0.0430 0.0151 1.0000
16.500 1.3401 0.04505 0.04076 0.0410 0.0148 1.0000
16.750 1.3249 0.05041 0.04625 0.0384 0.0146 1.0000
17.000 1.3203 0.05457 0.05053 0.0364 0.0145 1.0000
17.250 1.3021 0.06077 0.05688 0.0331 0.0145 1.0000
17.500 1.2878 0.06651 0.06274 0.0302 0.0145 1.0000
17.750 1.2711 0.07268 0.06903 0.0270 0.0144 1.0000
18.000 1.2471 0.08000 0.07648 0.0233 0.0144 1.0000
18.250 1.2290 0.08658 0.08318 0.0200 0.0143 1.0000
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