WORTMANN FX 77-W-153 AIRFOIL (fx77w153-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: WORTMANN FX 77-W-153 AIRFOIL (fx77w153-il) Reynolds number: 1,000,000 Max Cl/Cd: 123.98 at α=7° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx77w153-il-1000000-n5.txt Download as CSV file: xf-fx77w153-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 77-W-153 AIRFOIL
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
------ -------- --------- --------- -------- -------- --------
-12.250 -0.9075 0.03948 0.03547 -0.0397 0.4740 0.0092
-12.000 -0.9177 0.03601 0.03175 -0.0378 0.4696 0.0092
-11.750 -0.9149 0.03339 0.02889 -0.0363 0.4631 0.0092
-11.500 -0.9071 0.03118 0.02644 -0.0350 0.4568 0.0092
-11.250 -0.8947 0.02940 0.02446 -0.0337 0.4495 0.0092
-11.000 -0.8787 0.02801 0.02289 -0.0327 0.4417 0.0093
-10.750 -0.8608 0.02679 0.02150 -0.0317 0.4351 0.0093
-10.500 -0.8412 0.02575 0.02031 -0.0308 0.4285 0.0094
-10.250 -0.8201 0.02488 0.01930 -0.0301 0.4234 0.0094
-10.000 -0.7986 0.02402 0.01831 -0.0293 0.4191 0.0095
-9.750 -0.7762 0.02325 0.01742 -0.0286 0.4149 0.0095
-9.500 -0.7539 0.02243 0.01646 -0.0279 0.4108 0.0096
-9.250 -0.7328 0.02136 0.01524 -0.0270 0.4079 0.0096
-9.000 -0.7120 0.02017 0.01386 -0.0260 0.4053 0.0097
-8.750 -0.6897 0.01918 0.01271 -0.0252 0.4024 0.0097
-8.500 -0.6663 0.01837 0.01176 -0.0245 0.3993 0.0098
-8.250 -0.6421 0.01768 0.01095 -0.0239 0.3963 0.0098
-8.000 -0.6173 0.01706 0.01022 -0.0233 0.3934 0.0098
-7.750 -0.5921 0.01647 0.00953 -0.0228 0.3916 0.0099
-7.500 -0.5667 0.01592 0.00890 -0.0222 0.3896 0.0099
-7.250 -0.5408 0.01542 0.00832 -0.0218 0.3873 0.0099
-7.000 -0.5148 0.01495 0.00777 -0.0213 0.3849 0.0100
-6.750 -0.4885 0.01453 0.00728 -0.0209 0.3825 0.0100
-6.500 -0.4619 0.01414 0.00681 -0.0205 0.3804 0.0101
-6.000 -0.4082 0.01344 0.00600 -0.0199 0.3769 0.0102
-5.750 -0.3811 0.01313 0.00564 -0.0196 0.3757 0.0103
-5.500 -0.3538 0.01283 0.00530 -0.0193 0.3744 0.0104
-5.250 -0.3264 0.01256 0.00498 -0.0190 0.3729 0.0105
-5.000 -0.2989 0.01231 0.00469 -0.0188 0.3716 0.0107
-4.750 -0.2712 0.01208 0.00442 -0.0186 0.3704 0.0108
-4.500 -0.2435 0.01186 0.00417 -0.0184 0.3694 0.0110
-4.250 -0.2156 0.01167 0.00394 -0.0182 0.3685 0.0112
-4.000 -0.1877 0.01148 0.00372 -0.0180 0.3676 0.0114
-3.750 -0.1597 0.01132 0.00352 -0.0179 0.3667 0.0117
-3.500 -0.1316 0.01117 0.00334 -0.0177 0.3659 0.0120
-3.250 -0.1035 0.01103 0.00318 -0.0176 0.3650 0.0123
-3.000 -0.0753 0.01090 0.00304 -0.0175 0.3641 0.0130
-2.750 -0.0471 0.01078 0.00292 -0.0174 0.3631 0.0142
-2.250 0.0098 0.01064 0.00283 -0.0173 0.3614 0.0213
-2.000 0.0385 0.01060 0.00277 -0.0173 0.3611 0.0225
-1.750 0.0669 0.01052 0.00270 -0.0173 0.3607 0.0237
-1.500 0.0955 0.01046 0.00264 -0.0173 0.3602 0.0248
-1.250 0.1241 0.01040 0.00258 -0.0173 0.3595 0.0257
-1.000 0.1528 0.01036 0.00253 -0.0174 0.3587 0.0265
-0.750 0.1813 0.01028 0.00245 -0.0174 0.3578 0.0274
-0.500 0.2097 0.01020 0.00238 -0.0174 0.3567 0.0287
-0.250 0.2382 0.01014 0.00232 -0.0174 0.3555 0.0298
0.000 0.2668 0.01010 0.00227 -0.0174 0.3542 0.0305
0.250 0.2954 0.01008 0.00223 -0.0175 0.3529 0.0311
0.500 0.3240 0.01005 0.00220 -0.0175 0.3520 0.0323
0.750 0.3525 0.01002 0.00219 -0.0176 0.3513 0.0349
1.250 0.4094 0.00999 0.00220 -0.0177 0.3495 0.0504
1.500 0.4378 0.00998 0.00221 -0.0177 0.3487 0.0585
1.750 0.4660 0.00994 0.00224 -0.0177 0.3478 0.0852
2.000 0.4939 0.00989 0.00228 -0.0178 0.3468 0.1194
2.250 0.5216 0.00981 0.00232 -0.0178 0.3460 0.1727
2.500 0.5484 0.00954 0.00235 -0.0177 0.3455 0.2846
2.750 0.5746 0.00922 0.00239 -0.0175 0.3449 0.4094
3.000 0.5997 0.00886 0.00243 -0.0171 0.3443 0.5494
3.250 0.6218 0.00836 0.00248 -0.0160 0.3437 0.7266
3.500 0.6584 0.00791 0.00272 -0.0175 0.3429 0.9491
3.750 0.6936 0.00804 0.00285 -0.0190 0.3420 0.9682
4.000 0.7214 0.00815 0.00295 -0.0189 0.3409 0.9788
4.250 0.7698 0.00828 0.00307 -0.0233 0.3395 0.9839
4.500 0.8170 0.00842 0.00320 -0.0275 0.3381 0.9908
4.750 0.8579 0.00851 0.00328 -0.0303 0.3364 0.9935
5.000 0.9008 0.00858 0.00333 -0.0337 0.3345 0.9957
5.250 0.9378 0.00867 0.00340 -0.0357 0.3328 0.9975
5.500 0.9706 0.00878 0.00350 -0.0369 0.3310 0.9985
5.750 1.0023 0.00885 0.00358 -0.0379 0.3299 0.9992
6.000 1.0347 0.00890 0.00366 -0.0389 0.3287 0.9999
6.250 1.0620 0.00894 0.00373 -0.0389 0.3261 1.0000
6.500 1.0887 0.00898 0.00377 -0.0388 0.3205 1.0000
6.750 1.1151 0.00904 0.00380 -0.0386 0.3121 1.0000
7.000 1.1406 0.00920 0.00386 -0.0384 0.2959 1.0000
7.250 1.1652 0.00947 0.00406 -0.0380 0.2839 1.0000
7.500 1.1898 0.00973 0.00428 -0.0376 0.2754 1.0000
7.750 1.2146 0.00994 0.00448 -0.0373 0.2702 1.0000
8.000 1.2392 0.01016 0.00469 -0.0369 0.2615 1.0000
8.250 1.2625 0.01050 0.00497 -0.0364 0.2499 1.0000
8.500 1.2848 0.01091 0.00531 -0.0357 0.2378 1.0000
8.750 1.3070 0.01129 0.00566 -0.0351 0.2292 1.0000
9.000 1.3301 0.01157 0.00594 -0.0345 0.2226 1.0000
9.250 1.3508 0.01203 0.00634 -0.0336 0.2120 1.0000
9.500 1.3708 0.01251 0.00677 -0.0326 0.1970 1.0000
9.750 1.3884 0.01314 0.00731 -0.0313 0.1819 1.0000
10.000 1.4066 0.01367 0.00779 -0.0301 0.1718 1.0000
10.250 1.4261 0.01408 0.00820 -0.0290 0.1648 1.0000
10.500 1.4391 0.01486 0.00890 -0.0271 0.1454 1.0000
10.750 1.4467 0.01588 0.00979 -0.0245 0.1267 1.0000
11.000 1.4462 0.01720 0.01100 -0.0208 0.1005 1.0000
11.250 1.4495 0.01821 0.01197 -0.0177 0.0901 1.0000
11.500 1.4516 0.01909 0.01285 -0.0144 0.0821 1.0000
11.750 1.4486 0.02047 0.01424 -0.0112 0.0716 1.0000
12.000 1.4391 0.02299 0.01675 -0.0094 0.0599 1.0000
12.250 1.4360 0.02596 0.01979 -0.0098 0.0531 1.0000
12.500 1.4300 0.02997 0.02386 -0.0113 0.0477 1.0000
12.750 1.4245 0.03396 0.02794 -0.0126 0.0433 1.0000
13.000 1.4027 0.03968 0.03374 -0.0138 0.0360 1.0000
13.250 1.3807 0.04514 0.03927 -0.0146 0.0319 1.0000
13.500 1.3668 0.04954 0.04375 -0.0151 0.0303 1.0000
13.750 1.3521 0.05403 0.04831 -0.0156 0.0284 1.0000
14.000 1.3378 0.05844 0.05279 -0.0161 0.0266 1.0000
14.250 1.3305 0.06215 0.05657 -0.0165 0.0251 1.0000
14.500 1.3215 0.06619 0.06066 -0.0171 0.0221 1.0000
14.750 1.3073 0.07098 0.06549 -0.0180 0.0167 1.0000
15.000 1.2982 0.07517 0.06970 -0.0187 0.0144 1.0000
15.250 1.2941 0.07880 0.07338 -0.0194 0.0137 1.0000
15.500 1.2918 0.08221 0.07684 -0.0200 0.0131 1.0000
15.750 1.2882 0.08584 0.08053 -0.0208 0.0127 1.0000
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