FX 83-W-227 (fx83w227-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: FX 83-W-227 (fx83w227-il) Reynolds number: 500,000 Max Cl/Cd: 62.91 at α=8.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx83w227-il-500000-n5.txt Download as CSV file: xf-fx83w227-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: FX 83-W-227
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -0.9120 0.08455 0.08011 -0.0918 1.0000 0.0411
-19.500 -0.9219 0.08070 0.07617 -0.0928 1.0000 0.0415
-19.250 -0.9326 0.07684 0.07223 -0.0938 1.0000 0.0421
-19.000 -0.9348 0.07241 0.06773 -0.0971 0.9993 0.0426
-18.750 -0.9341 0.06832 0.06357 -0.1002 0.9983 0.0432
-18.500 -0.9310 0.06459 0.05977 -0.1032 0.9970 0.0440
-18.250 -0.9259 0.06121 0.05631 -0.1060 0.9956 0.0448
-18.000 -0.9187 0.05811 0.05312 -0.1086 0.9939 0.0454
-17.750 -0.9095 0.05534 0.05026 -0.1110 0.9921 0.0464
-17.500 -0.9012 0.05272 0.04754 -0.1129 0.9900 0.0469
-17.250 -0.8957 0.04975 0.04454 -0.1151 0.9877 0.0479
-17.000 -0.8864 0.04715 0.04188 -0.1173 0.9855 0.0486
-16.750 -0.8740 0.04481 0.03949 -0.1196 0.9835 0.0497
-16.500 -0.8589 0.04273 0.03734 -0.1218 0.9819 0.0506
-16.250 -0.8488 0.04089 0.03543 -0.1226 0.9777 0.0517
-16.000 -0.8341 0.03920 0.03366 -0.1239 0.9739 0.0526
-15.750 -0.8214 0.03715 0.03157 -0.1257 0.9709 0.0534
-15.500 -0.8105 0.03540 0.02980 -0.1265 0.9659 0.0546
-15.250 -0.7977 0.03380 0.02815 -0.1273 0.9604 0.0556
-14.750 -0.7628 0.03106 0.02529 -0.1296 0.9498 0.0578
-14.500 -0.7406 0.02981 0.02395 -0.1314 0.9444 0.0587
-14.250 -0.7192 0.02833 0.02245 -0.1335 0.9383 0.0599
-14.000 -0.6937 0.02703 0.02110 -0.1361 0.9309 0.0611
-13.750 -0.6584 0.02582 0.01984 -0.1403 0.9258 0.0627
-13.500 -0.6270 0.02481 0.01875 -0.1434 0.9165 0.0644
-13.250 -0.5913 0.02383 0.01768 -0.1472 0.9074 0.0659
-13.000 -0.5624 0.02276 0.01655 -0.1501 0.8939 0.0677
-12.750 -0.5361 0.02195 0.01565 -0.1519 0.8790 0.0694
-12.500 -0.5146 0.02124 0.01483 -0.1525 0.8642 0.0710
-12.250 -0.4960 0.02066 0.01413 -0.1524 0.8512 0.0726
-12.000 -0.4816 0.02003 0.01342 -0.1515 0.8388 0.0741
-11.750 -0.4696 0.01943 0.01275 -0.1501 0.8271 0.0756
-11.500 -0.4564 0.01891 0.01215 -0.1488 0.8168 0.0773
-11.250 -0.4436 0.01842 0.01160 -0.1472 0.8071 0.0791
-11.000 -0.4294 0.01801 0.01109 -0.1458 0.7986 0.0810
-10.750 -0.4177 0.01752 0.01058 -0.1439 0.7902 0.0830
-10.500 -0.4056 0.01708 0.01009 -0.1421 0.7820 0.0854
-10.250 -0.3922 0.01669 0.00965 -0.1403 0.7746 0.0875
-10.000 -0.3781 0.01635 0.00926 -0.1386 0.7672 0.0898
-9.750 -0.3653 0.01599 0.00884 -0.1366 0.7604 0.0921
-9.500 -0.3525 0.01562 0.00846 -0.1346 0.7535 0.0950
-9.250 -0.3386 0.01532 0.00812 -0.1326 0.7467 0.0982
-9.000 -0.3240 0.01506 0.00780 -0.1307 0.7404 0.1009
-8.750 -0.3110 0.01474 0.00747 -0.1285 0.7342 0.1041
-8.500 -0.2971 0.01448 0.00718 -0.1264 0.7276 0.1076
-8.250 -0.2820 0.01428 0.00692 -0.1244 0.7218 0.1111
-8.000 -0.2685 0.01400 0.00665 -0.1221 0.7157 0.1150
-7.750 -0.2546 0.01378 0.00641 -0.1198 0.7095 0.1197
-7.250 -0.2265 0.01336 0.00595 -0.1152 0.6981 0.1283
-7.000 -0.2122 0.01318 0.00576 -0.1128 0.6922 0.1331
-6.750 -0.1988 0.01303 0.00556 -0.1102 0.6864 0.1384
-6.500 -0.1861 0.01285 0.00539 -0.1075 0.6814 0.1442
-6.250 -0.1726 0.01273 0.00526 -0.1048 0.6759 0.1498
-6.000 -0.1612 0.01261 0.00514 -0.1017 0.6704 0.1557
-5.750 -0.1475 0.01250 0.00501 -0.0991 0.6652 0.1630
-5.500 -0.1320 0.01234 0.00487 -0.0968 0.6602 0.1715
-5.250 -0.1157 0.01221 0.00475 -0.0947 0.6550 0.1805
-5.000 -0.1006 0.01207 0.00461 -0.0923 0.6496 0.1907
-4.750 -0.0840 0.01193 0.00449 -0.0902 0.6449 0.2018
-4.500 -0.0669 0.01178 0.00438 -0.0882 0.6401 0.2157
-4.250 -0.0508 0.01162 0.00426 -0.0860 0.6352 0.2307
-4.000 -0.0349 0.01147 0.00414 -0.0838 0.6302 0.2474
-3.750 -0.0185 0.01131 0.00403 -0.0816 0.6256 0.2661
-3.500 -0.0016 0.01114 0.00393 -0.0796 0.6209 0.2864
-3.250 0.0149 0.01098 0.00383 -0.0774 0.6161 0.3075
-3.000 0.0305 0.01083 0.00373 -0.0751 0.6113 0.3304
-2.750 0.0467 0.01066 0.00364 -0.0729 0.6067 0.3551
-2.500 0.0636 0.01050 0.00356 -0.0708 0.6023 0.3795
-2.250 0.0792 0.01037 0.00349 -0.0684 0.5974 0.4030
-2.000 0.0938 0.01025 0.00341 -0.0658 0.5928 0.4260
-1.750 0.1088 0.01011 0.00335 -0.0632 0.5885 0.4515
-1.500 0.1251 0.00999 0.00331 -0.0610 0.5837 0.4760
-1.250 0.1416 0.00991 0.00329 -0.0587 0.5788 0.4988
-1.000 0.1588 0.00987 0.00328 -0.0566 0.5743 0.5191
-0.750 0.1773 0.00984 0.00329 -0.0548 0.5700 0.5386
-0.500 0.1965 0.00982 0.00331 -0.0531 0.5651 0.5558
-0.250 0.2152 0.00983 0.00335 -0.0513 0.5601 0.5710
0.000 0.2340 0.00987 0.00339 -0.0496 0.5554 0.5848
0.250 0.2544 0.00990 0.00344 -0.0481 0.5510 0.5998
0.500 0.2742 0.00992 0.00351 -0.0466 0.5462 0.6144
0.750 0.2932 0.00997 0.00358 -0.0449 0.5409 0.6275
1.000 0.3119 0.01007 0.00364 -0.0432 0.5360 0.6396
1.250 0.3326 0.01011 0.00372 -0.0418 0.5316 0.6498
1.500 0.3531 0.01019 0.00380 -0.0405 0.5264 0.6602
1.750 0.3719 0.01027 0.00389 -0.0388 0.5211 0.6687
2.000 0.3909 0.01038 0.00398 -0.0372 0.5164 0.6772
2.250 0.4119 0.01045 0.00407 -0.0360 0.5116 0.6848
2.500 0.4314 0.01055 0.00418 -0.0345 0.5064 0.6928
2.750 0.4503 0.01068 0.00429 -0.0329 0.5015 0.7006
3.000 0.4693 0.01079 0.00442 -0.0314 0.4966 0.7077
3.250 0.4889 0.01090 0.00454 -0.0300 0.4913 0.7154
3.500 0.5078 0.01105 0.00468 -0.0285 0.4862 0.7232
3.750 0.5252 0.01120 0.00484 -0.0267 0.4817 0.7314
4.000 0.5449 0.01133 0.00498 -0.0253 0.4772 0.7401
4.250 0.5637 0.01147 0.00515 -0.0239 0.4720 0.7478
4.500 0.5809 0.01164 0.00533 -0.0221 0.4668 0.7563
5.000 0.6173 0.01198 0.00572 -0.0190 0.4580 0.7728
5.250 0.6354 0.01217 0.00592 -0.0175 0.4531 0.7817
5.500 0.6522 0.01238 0.00615 -0.0158 0.4485 0.7910
5.750 0.6684 0.01261 0.00640 -0.0140 0.4440 0.8012
6.000 0.6874 0.01278 0.00663 -0.0127 0.4396 0.8116
6.250 0.7049 0.01299 0.00689 -0.0112 0.4349 0.8245
6.500 0.7217 0.01324 0.00719 -0.0096 0.4305 0.8392
6.750 0.7408 0.01350 0.00750 -0.0086 0.4261 0.8575
7.000 0.7694 0.01371 0.00783 -0.0094 0.4215 0.8798
7.250 0.8152 0.01406 0.00828 -0.0141 0.4161 0.9052
7.500 0.8710 0.01455 0.00879 -0.0210 0.4109 0.9262
7.750 0.9244 0.01498 0.00925 -0.0272 0.4058 0.9422
8.000 0.9687 0.01542 0.00972 -0.0317 0.4005 0.9577
8.250 1.0021 0.01593 0.01023 -0.0339 0.3956 0.9736
8.500 1.0303 0.01647 0.01076 -0.0351 0.3909 0.9860
9.000 1.0831 0.01754 0.01186 -0.0366 0.3820 1.0000
9.250 1.0933 0.01805 0.01235 -0.0343 0.3778 1.0000
9.500 1.1035 0.01860 0.01289 -0.0321 0.3738 1.0000
9.750 1.1174 0.01906 0.01338 -0.0305 0.3697 1.0000
10.000 1.1307 0.01957 0.01391 -0.0288 0.3655 1.0000
10.250 1.1413 0.02023 0.01456 -0.0269 0.3609 1.0000
10.500 1.1521 0.02092 0.01524 -0.0250 0.3566 1.0000
10.750 1.1661 0.02151 0.01587 -0.0237 0.3520 1.0000
11.000 1.1780 0.02222 0.01659 -0.0221 0.3469 1.0000
11.250 1.1885 0.02302 0.01739 -0.0204 0.3423 1.0000
11.500 1.1999 0.02382 0.01820 -0.0190 0.3379 1.0000
11.750 1.2134 0.02454 0.01895 -0.0178 0.3331 1.0000
12.000 1.2232 0.02548 0.01991 -0.0163 0.3277 1.0000
12.250 1.2314 0.02655 0.02096 -0.0147 0.3220 1.0000
12.500 1.2403 0.02764 0.02207 -0.0133 0.3138 1.0000
13.000 1.2541 0.03014 0.02457 -0.0103 0.2986 1.0000
13.250 1.2585 0.03161 0.02603 -0.0088 0.2912 1.0000
13.500 1.2674 0.03283 0.02727 -0.0077 0.2848 1.0000
13.750 1.2756 0.03412 0.02858 -0.0066 0.2790 1.0000
14.000 1.2798 0.03572 0.03017 -0.0052 0.2733 1.0000
14.250 1.2898 0.03694 0.03143 -0.0044 0.2675 1.0000
14.500 1.2936 0.03865 0.03315 -0.0032 0.2601 1.0000
14.750 1.2988 0.04030 0.03481 -0.0021 0.2540 1.0000
15.000 1.3044 0.04193 0.03647 -0.0012 0.2470 1.0000
15.250 1.3047 0.04403 0.03856 -0.0001 0.2399 1.0000
15.500 1.3096 0.04579 0.04035 0.0008 0.2321 1.0000
15.750 1.3073 0.04820 0.04275 0.0019 0.2242 1.0000
16.000 1.3097 0.05025 0.04481 0.0026 0.2160 1.0000
16.250 1.3068 0.05280 0.04737 0.0036 0.2079 1.0000
16.500 1.3038 0.05541 0.04997 0.0044 0.1986 1.0000
16.750 1.3011 0.05803 0.05260 0.0051 0.1898 1.0000
17.000 1.2936 0.06120 0.05575 0.0059 0.1806 1.0000
17.250 1.2900 0.06402 0.05859 0.0064 0.1714 1.0000
17.500 1.2819 0.06734 0.06188 0.0070 0.1615 1.0000
17.750 1.2738 0.07072 0.06526 0.0074 0.1533 1.0000
18.000 1.2671 0.07404 0.06858 0.0077 0.1442 1.0000
18.250 1.2577 0.07769 0.07222 0.0079 0.1346 1.0000
18.750 1.2450 0.08448 0.07903 0.0080 0.1205 1.0000
19.000 1.2380 0.08801 0.08256 0.0079 0.1136 1.0000
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