FX 61-168 AIRFOIL (fx61168-il) Xfoil prediction polar at RE=100,000 Ncrit=5
| Details | Polar file |
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Airfoil: FX 61-168 AIRFOIL (fx61168-il) Reynolds number: 100,000 Max Cl/Cd: 48.38 at α=8.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx61168-il-100000-n5.txt Download as CSV file: xf-fx61168-il-100000-n5.csv |
XFOIL Version 6.96
Calculated polar for: FX 61-168 AIRFOIL
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
------ -------- --------- --------- -------- -------- --------
-11.250 -0.3838 0.09513 0.09029 -0.0582 1.0000 0.0222
-11.000 -0.4120 0.08400 0.07915 -0.0646 1.0000 0.0213
-10.750 -0.4696 0.07229 0.06725 -0.0710 1.0000 0.0202
-10.250 -0.5254 0.06402 0.05870 -0.0708 1.0000 0.0197
-10.000 -0.5473 0.06157 0.05621 -0.0685 1.0000 0.0197
-9.750 -0.5516 0.05745 0.05189 -0.0714 0.9901 0.0196
-9.500 -0.5529 0.05311 0.04722 -0.0745 0.9678 0.0197
-9.250 -0.5456 0.04904 0.04278 -0.0768 0.9464 0.0197
-9.000 -0.5342 0.04524 0.03861 -0.0784 0.9280 0.0199
-8.750 -0.5130 0.04236 0.03555 -0.0806 0.9138 0.0206
-8.500 -0.4855 0.04007 0.03305 -0.0832 0.9012 0.0218
-8.250 -0.4550 0.03725 0.02982 -0.0860 0.8894 0.0230
-8.000 -0.4228 0.03439 0.02649 -0.0883 0.8763 0.0240
-7.750 -0.3872 0.03186 0.02353 -0.0904 0.8639 0.0247
-7.500 -0.3493 0.02981 0.02106 -0.0923 0.8520 0.0256
-7.250 -0.3127 0.02797 0.01920 -0.0942 0.8404 0.0271
-7.000 -0.2774 0.02680 0.01789 -0.0960 0.8282 0.0295
-6.750 -0.2458 0.02579 0.01669 -0.0968 0.8155 0.0324
-6.500 -0.2190 0.02469 0.01554 -0.0968 0.8037 0.0343
-6.250 -0.1948 0.02380 0.01458 -0.0969 0.7929 0.0373
-6.000 -0.1698 0.02310 0.01371 -0.0971 0.7833 0.0421
-5.750 -0.1509 0.02224 0.01282 -0.0965 0.7736 0.0472
-5.500 -0.1276 0.02147 0.01192 -0.0966 0.7656 0.0558
-5.250 -0.1081 0.02065 0.01115 -0.0961 0.7569 0.0728
-5.000 -0.0897 0.01933 0.01023 -0.0961 0.7501 0.1493
-4.750 -0.0811 0.01737 0.00990 -0.0953 0.7425 0.4439
-4.500 -0.0559 0.01821 0.01100 -0.0930 0.7371 0.5488
-4.250 -0.0304 0.01950 0.01222 -0.0909 0.7307 0.5962
-4.000 -0.0045 0.02081 0.01337 -0.0887 0.7248 0.6234
-3.750 0.0238 0.02113 0.01345 -0.0885 0.7198 0.6365
-3.500 0.0483 0.02134 0.01354 -0.0874 0.7139 0.6400
-3.250 0.0753 0.02140 0.01342 -0.0872 0.7090 0.6455
-3.000 0.1046 0.02126 0.01305 -0.0881 0.7046 0.6533
-2.750 0.1283 0.02138 0.01308 -0.0872 0.6990 0.6572
-2.500 0.1558 0.02131 0.01284 -0.0876 0.6940 0.6638
-2.250 0.1849 0.02126 0.01262 -0.0881 0.6901 0.6692
-2.000 0.2080 0.02136 0.01267 -0.0872 0.6847 0.6733
-1.750 0.2361 0.02128 0.01245 -0.0880 0.6798 0.6813
-1.500 0.2626 0.02138 0.01244 -0.0875 0.6759 0.6852
-1.250 0.2872 0.02146 0.01246 -0.0869 0.6714 0.6894
-1.000 0.3145 0.02138 0.01230 -0.0876 0.6665 0.6957
-0.750 0.3414 0.02139 0.01222 -0.0877 0.6623 0.6994
-0.500 0.3689 0.02144 0.01218 -0.0876 0.6588 0.7027
-0.250 0.3925 0.02149 0.01222 -0.0872 0.6536 0.7070
0.000 0.4221 0.02143 0.01209 -0.0884 0.6489 0.7126
0.250 0.4486 0.02147 0.01207 -0.0881 0.6450 0.7152
0.500 0.4726 0.02155 0.01215 -0.0876 0.6402 0.7184
0.750 0.4981 0.02160 0.01219 -0.0876 0.6351 0.7224
1.000 0.5300 0.02158 0.01209 -0.0891 0.6309 0.7274
1.250 0.5555 0.02165 0.01215 -0.0887 0.6269 0.7297
1.500 0.5775 0.02178 0.01234 -0.0879 0.6216 0.7328
1.750 0.6043 0.02185 0.01240 -0.0880 0.6172 0.7363
2.000 0.6359 0.02188 0.01238 -0.0892 0.6136 0.7402
2.250 0.6601 0.02203 0.01259 -0.0891 0.6083 0.7436
2.500 0.6835 0.02215 0.01276 -0.0884 0.6033 0.7462
2.750 0.7115 0.02220 0.01281 -0.0886 0.5991 0.7493
3.000 0.7366 0.02235 0.01301 -0.0886 0.5938 0.7527
3.250 0.7639 0.02248 0.01318 -0.0891 0.5880 0.7565
3.500 0.7917 0.02252 0.01324 -0.0893 0.5836 0.7592
3.750 0.8135 0.02271 0.01353 -0.0885 0.5780 0.7620
4.000 0.8375 0.02286 0.01376 -0.0881 0.5723 0.7650
4.250 0.8675 0.02291 0.01382 -0.0888 0.5680 0.7683
4.500 0.8920 0.02317 0.01420 -0.0889 0.5618 0.7721
4.750 0.9150 0.02330 0.01443 -0.0882 0.5561 0.7746
5.000 0.9437 0.02330 0.01444 -0.0884 0.5518 0.7772
5.250 0.9612 0.02361 0.01494 -0.0871 0.5439 0.7804
5.500 0.9898 0.02364 0.01501 -0.0875 0.5384 0.7838
5.750 1.0137 0.02390 0.01539 -0.0874 0.5312 0.7872
6.000 1.0363 0.02400 0.01562 -0.0867 0.5249 0.7897
6.250 1.0595 0.02413 0.01586 -0.0861 0.5187 0.7925
6.500 1.0800 0.02431 0.01618 -0.0851 0.5106 0.7958
6.750 1.1041 0.02442 0.01638 -0.0848 0.5029 0.7991
7.250 1.1458 0.02474 0.01698 -0.0831 0.4855 0.8051
7.500 1.1697 0.02471 0.01701 -0.0824 0.4774 0.8082
7.750 1.1850 0.02504 0.01751 -0.0808 0.4667 0.8117
8.000 1.2053 0.02526 0.01785 -0.0799 0.4568 0.8151
8.250 1.2280 0.02538 0.01804 -0.0793 0.4476 0.8182
8.500 1.2385 0.02576 0.01859 -0.0768 0.4365 0.8215
8.750 1.2518 0.02608 0.01902 -0.0747 0.4254 0.8253
9.000 1.2681 0.02642 0.01942 -0.0732 0.4141 0.8292
9.250 1.2851 0.02680 0.01988 -0.0719 0.4026 0.8329
9.500 1.2934 0.02745 0.02067 -0.0694 0.3905 0.8364
9.750 1.3020 0.02816 0.02148 -0.0672 0.3774 0.8406
10.000 1.3103 0.02900 0.02238 -0.0651 0.3635 0.8454
10.250 1.3154 0.02995 0.02342 -0.0628 0.3493 0.8499
10.500 1.3183 0.03110 0.02463 -0.0604 0.3348 0.8548
10.750 1.3199 0.03253 0.02612 -0.0583 0.3188 0.8600
11.000 1.3190 0.03414 0.02778 -0.0562 0.3027 0.8651
11.250 1.3166 0.03598 0.02967 -0.0542 0.2863 0.8711
11.500 1.3133 0.03811 0.03181 -0.0526 0.2694 0.8778
11.750 1.3079 0.04041 0.03417 -0.0510 0.2527 0.8856
12.000 1.3030 0.04283 0.03663 -0.0497 0.2369 0.8949
12.500 1.2906 0.04781 0.04169 -0.0469 0.2090 0.9270
12.750 1.2834 0.05050 0.04444 -0.0461 0.1956 1.0000
13.000 1.2816 0.05376 0.04769 -0.0465 0.1816 1.0000
13.500 1.2773 0.06059 0.05456 -0.0477 0.1558 1.0000
13.750 1.2748 0.06420 0.05821 -0.0484 0.1435 1.0000
14.000 1.2717 0.06797 0.06201 -0.0493 0.1320 1.0000
14.250 1.2681 0.07188 0.06596 -0.0502 0.1213 1.0000
14.500 1.2636 0.07602 0.07016 -0.0513 0.1111 1.0000
14.750 1.2581 0.08040 0.07456 -0.0526 0.1013 1.0000
15.000 1.2537 0.08475 0.07896 -0.0540 0.0916 1.0000
15.250 1.2488 0.08927 0.08352 -0.0555 0.0831 1.0000
15.500 1.2421 0.09412 0.08837 -0.0572 0.0760 1.0000
15.750 1.2392 0.09853 0.09288 -0.0589 0.0688 1.0000
16.000 1.2326 0.10354 0.09789 -0.0609 0.0635 1.0000
16.250 1.2297 0.10809 0.10255 -0.0628 0.0577 1.0000
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