WORTMANN FX 76-120 (fx76120-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: WORTMANN FX 76-120 (fx76120-il) Reynolds number: 1,000,000 Max Cl/Cd: 76.83 at α=9.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx76120-il-1000000-n5.txt Download as CSV file: xf-fx76120-il-1000000-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 = 1.000 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.000 -1.2330 0.09690 0.09355 -0.0153 1.0000 0.0107
-18.750 -1.2676 0.08756 0.08406 -0.0202 1.0000 0.0108
-18.500 -1.3012 0.07857 0.07491 -0.0248 1.0000 0.0106
-18.250 -1.3294 0.07058 0.06678 -0.0289 1.0000 0.0108
-18.000 -1.3528 0.06344 0.05949 -0.0327 1.0000 0.0107
-17.750 -1.3734 0.05684 0.05274 -0.0361 1.0000 0.0108
-17.500 -1.3871 0.05145 0.04722 -0.0389 1.0000 0.0109
-17.250 -1.3963 0.04690 0.04254 -0.0410 1.0000 0.0110
-17.000 -1.4042 0.04276 0.03828 -0.0427 1.0000 0.0110
-16.750 -1.4053 0.03969 0.03510 -0.0437 1.0000 0.0113
-16.500 -1.4092 0.03652 0.03182 -0.0444 1.0000 0.0114
-16.250 -1.4070 0.03422 0.02942 -0.0446 1.0000 0.0115
-16.000 -1.4054 0.03203 0.02713 -0.0443 1.0000 0.0116
-15.750 -1.4006 0.03029 0.02531 -0.0437 1.0000 0.0119
-15.500 -1.3975 0.02852 0.02346 -0.0428 1.0000 0.0121
-15.250 -1.3919 0.02708 0.02196 -0.0416 1.0000 0.0125
-15.000 -1.3854 0.02581 0.02062 -0.0402 1.0000 0.0128
-14.750 -1.3768 0.02474 0.01950 -0.0387 1.0000 0.0132
-14.500 -1.3672 0.02380 0.01849 -0.0370 1.0000 0.0137
-14.250 -1.3565 0.02297 0.01761 -0.0353 1.0000 0.0140
-14.000 -1.3461 0.02218 0.01675 -0.0334 1.0000 0.0143
-13.750 -1.3345 0.02149 0.01599 -0.0314 1.0000 0.0145
-13.500 -1.3237 0.02080 0.01525 -0.0292 1.0000 0.0149
-13.250 -1.3132 0.02015 0.01457 -0.0267 1.0000 0.0155
-13.000 -1.3018 0.01960 0.01398 -0.0242 1.0000 0.0159
-12.750 -1.2892 0.01907 0.01341 -0.0218 1.0000 0.0165
-12.500 -1.2735 0.01855 0.01285 -0.0200 1.0000 0.0169
-12.250 -1.2570 0.01808 0.01233 -0.0183 1.0000 0.0175
-12.000 -1.2398 0.01764 0.01185 -0.0166 1.0000 0.0179
-11.750 -1.2233 0.01715 0.01132 -0.0148 1.0000 0.0185
-11.500 -1.2062 0.01669 0.01084 -0.0130 1.0000 0.0193
-11.250 -1.1884 0.01627 0.01040 -0.0113 1.0000 0.0200
-11.000 -1.1702 0.01589 0.00999 -0.0097 1.0000 0.0210
-10.750 -1.1518 0.01553 0.00960 -0.0080 1.0000 0.0216
-10.500 -1.1339 0.01515 0.00919 -0.0063 1.0000 0.0224
-10.250 -1.1161 0.01477 0.00880 -0.0045 1.0000 0.0234
-10.000 -1.0982 0.01443 0.00845 -0.0027 1.0000 0.0244
-9.750 -1.0800 0.01412 0.00811 -0.0009 1.0000 0.0254
-9.500 -1.0617 0.01383 0.00780 0.0009 1.0000 0.0264
-9.250 -1.0317 0.01342 0.00739 0.0002 0.9988 0.0281
-9.000 -1.0015 0.01307 0.00703 -0.0006 0.9970 0.0296
-8.750 -0.9715 0.01276 0.00671 -0.0012 0.9948 0.0310
-8.500 -0.9428 0.01241 0.00635 -0.0016 0.9924 0.0330
-8.250 -0.9132 0.01208 0.00603 -0.0021 0.9901 0.0351
-8.000 -0.8822 0.01179 0.00573 -0.0030 0.9881 0.0369
-7.750 -0.8525 0.01145 0.00541 -0.0035 0.9850 0.0401
-7.500 -0.8212 0.01115 0.00512 -0.0043 0.9821 0.0433
-7.250 -0.7891 0.01083 0.00482 -0.0054 0.9800 0.0473
-7.000 -0.7589 0.01055 0.00455 -0.0060 0.9770 0.0520
-6.750 -0.7300 0.01024 0.00428 -0.0063 0.9727 0.0582
-6.500 -0.6980 0.00995 0.00403 -0.0073 0.9700 0.0649
-6.250 -0.6664 0.00966 0.00378 -0.0082 0.9666 0.0740
-6.000 -0.6346 0.00936 0.00354 -0.0091 0.9628 0.0847
-5.750 -0.6004 0.00907 0.00330 -0.0106 0.9589 0.0969
-5.500 -0.5667 0.00875 0.00306 -0.0119 0.9521 0.1127
-5.250 -0.5310 0.00847 0.00284 -0.0137 0.9434 0.1285
-5.000 -0.5009 0.00825 0.00267 -0.0142 0.9331 0.1419
-4.750 -0.4708 0.00808 0.00252 -0.0146 0.9240 0.1530
-4.500 -0.4425 0.00792 0.00237 -0.0147 0.9136 0.1641
-4.250 -0.4152 0.00777 0.00224 -0.0144 0.9000 0.1749
-4.000 -0.3884 0.00766 0.00211 -0.0141 0.8832 0.1852
-3.750 -0.3628 0.00755 0.00199 -0.0134 0.8635 0.1985
-3.500 -0.3380 0.00745 0.00188 -0.0127 0.8426 0.2112
-3.250 -0.3134 0.00736 0.00177 -0.0118 0.8206 0.2239
-3.000 -0.2890 0.00730 0.00168 -0.0109 0.7983 0.2359
-2.750 -0.2651 0.00726 0.00159 -0.0099 0.7712 0.2494
-2.500 -0.2418 0.00724 0.00151 -0.0088 0.7393 0.2634
-2.250 -0.2183 0.00724 0.00145 -0.0077 0.7066 0.2771
-2.000 -0.1946 0.00723 0.00139 -0.0067 0.6762 0.2920
-1.750 -0.1706 0.00723 0.00133 -0.0058 0.6466 0.3068
-1.500 -0.1462 0.00721 0.00129 -0.0049 0.6205 0.3237
-1.250 -0.1220 0.00720 0.00125 -0.0041 0.5923 0.3425
-1.000 -0.0980 0.00720 0.00122 -0.0032 0.5608 0.3629
-0.750 -0.0736 0.00719 0.00119 -0.0024 0.5315 0.3848
-0.500 -0.0491 0.00721 0.00118 -0.0015 0.5015 0.4053
-0.250 -0.0244 0.00723 0.00117 -0.0008 0.4756 0.4255
0.000 0.0001 0.00722 0.00116 0.0000 0.4507 0.4491
0.250 0.0244 0.00723 0.00117 0.0008 0.4259 0.4756
0.500 0.0491 0.00721 0.00118 0.0015 0.4053 0.5013
0.750 0.0737 0.00720 0.00119 0.0023 0.3844 0.5297
1.000 0.0979 0.00721 0.00122 0.0032 0.3621 0.5605
1.250 0.1221 0.00721 0.00125 0.0040 0.3423 0.5900
1.500 0.1463 0.00721 0.00129 0.0049 0.3248 0.6197
1.750 0.1705 0.00723 0.00133 0.0058 0.3064 0.6473
2.000 0.1945 0.00722 0.00139 0.0067 0.2922 0.6783
2.250 0.2183 0.00724 0.00145 0.0077 0.2769 0.7071
2.500 0.2421 0.00725 0.00151 0.0087 0.2634 0.7359
2.750 0.2651 0.00726 0.00159 0.0099 0.2486 0.7713
3.000 0.2889 0.00731 0.00168 0.0109 0.2349 0.7985
3.250 0.3134 0.00737 0.00177 0.0118 0.2230 0.8200
3.500 0.3379 0.00746 0.00188 0.0127 0.2107 0.8426
4.000 0.3885 0.00766 0.00211 0.0140 0.1859 0.8830
4.250 0.4153 0.00777 0.00224 0.0144 0.1756 0.9004
4.500 0.4425 0.00792 0.00237 0.0147 0.1645 0.9135
4.750 0.4707 0.00810 0.00252 0.0146 0.1518 0.9243
5.000 0.5007 0.00827 0.00268 0.0142 0.1400 0.9330
5.250 0.5309 0.00848 0.00284 0.0137 0.1277 0.9433
5.500 0.5669 0.00874 0.00306 0.0119 0.1140 0.9522
5.750 0.6009 0.00905 0.00329 0.0105 0.0985 0.9590
6.000 0.6346 0.00937 0.00354 0.0091 0.0845 0.9628
6.250 0.6664 0.00967 0.00378 0.0082 0.0737 0.9667
6.500 0.6979 0.00995 0.00402 0.0073 0.0650 0.9699
6.750 0.7300 0.01024 0.00428 0.0063 0.0582 0.9727
7.000 0.7590 0.01054 0.00455 0.0059 0.0521 0.9770
7.250 0.7893 0.01082 0.00481 0.0053 0.0478 0.9800
7.500 0.8213 0.01115 0.00511 0.0043 0.0434 0.9821
7.750 0.8525 0.01145 0.00541 0.0035 0.0400 0.9850
8.000 0.8823 0.01179 0.00573 0.0029 0.0371 0.9881
8.250 0.9133 0.01207 0.00603 0.0021 0.0351 0.9901
8.500 0.9429 0.01241 0.00635 0.0016 0.0329 0.9924
8.750 0.9717 0.01276 0.00671 0.0012 0.0310 0.9948
9.000 1.0017 0.01307 0.00703 0.0005 0.0295 0.9971
9.250 1.0318 0.01343 0.00739 -0.0002 0.0279 0.9988
9.500 1.0617 0.01384 0.00781 -0.0009 0.0262 1.0000
9.750 1.0800 0.01412 0.00812 0.0009 0.0255 1.0000
10.000 1.0981 0.01443 0.00845 0.0027 0.0244 1.0000
10.250 1.1161 0.01477 0.00880 0.0045 0.0235 1.0000
10.500 1.1339 0.01515 0.00919 0.0063 0.0224 1.0000
10.750 1.1516 0.01555 0.00962 0.0081 0.0217 1.0000
11.000 1.1702 0.01589 0.01000 0.0097 0.0210 1.0000
11.250 1.1885 0.01627 0.01040 0.0113 0.0201 1.0000
11.500 1.2063 0.01669 0.01084 0.0130 0.0194 1.0000
11.750 1.2236 0.01714 0.01132 0.0147 0.0187 1.0000
12.000 1.2400 0.01764 0.01185 0.0165 0.0179 1.0000
12.250 1.2573 0.01808 0.01233 0.0182 0.0175 1.0000
12.500 1.2737 0.01856 0.01285 0.0200 0.0170 1.0000
12.750 1.2896 0.01907 0.01340 0.0218 0.0164 1.0000
13.000 1.3022 0.01960 0.01398 0.0242 0.0160 1.0000
13.250 1.3133 0.02017 0.01458 0.0267 0.0155 1.0000
13.500 1.3239 0.02082 0.01527 0.0291 0.0149 1.0000
13.750 1.3355 0.02147 0.01597 0.0313 0.0144 1.0000
14.000 1.3475 0.02213 0.01669 0.0332 0.0141 1.0000
14.250 1.3585 0.02290 0.01752 0.0351 0.0138 1.0000
14.500 1.3687 0.02375 0.01843 0.0368 0.0134 1.0000
14.750 1.3779 0.02472 0.01948 0.0385 0.0130 1.0000
15.000 1.3862 0.02581 0.02063 0.0400 0.0128 1.0000
15.250 1.3937 0.02702 0.02190 0.0414 0.0125 1.0000
15.500 1.3984 0.02854 0.02348 0.0426 0.0121 1.0000
15.750 1.4030 0.03018 0.02520 0.0435 0.0119 1.0000
16.000 1.4058 0.03210 0.02721 0.0441 0.0117 1.0000
16.250 1.4087 0.03417 0.02938 0.0443 0.0115 1.0000
16.500 1.4097 0.03662 0.03192 0.0442 0.0113 1.0000
16.750 1.4094 0.03938 0.03479 0.0436 0.0112 1.0000
17.000 1.4061 0.04272 0.03824 0.0425 0.0110 1.0000
17.250 1.3992 0.04673 0.04238 0.0408 0.0109 1.0000
17.500 1.3899 0.05130 0.04707 0.0386 0.0108 1.0000
17.750 1.3767 0.05665 0.05254 0.0359 0.0107 1.0000
18.000 1.3572 0.06308 0.05912 0.0325 0.0107 1.0000
18.250 1.3350 0.07006 0.06624 0.0288 0.0106 1.0000
18.500 1.3020 0.07881 0.07516 0.0243 0.0107 1.0000
18.750 1.2687 0.08779 0.08429 0.0196 0.0106 1.0000
19.000 1.2362 0.09680 0.09345 0.0149 0.0107 1.0000
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