FX 83-W-227 (fx83w227-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: FX 83-W-227 (fx83w227-il) Reynolds number: 1,000,000 Max Cl/Cd: 73.5 at α=9.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx83w227-il-1000000-n5.txt Download as CSV file: xf-fx83w227-il-1000000-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 = 1.000 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -1.0270 0.06227 0.05800 -0.1094 0.9958 0.0334
-19.500 -1.0267 0.05862 0.05428 -0.1120 0.9947 0.0340
-19.250 -1.0244 0.05533 0.05093 -0.1143 0.9935 0.0348
-19.000 -1.0204 0.05242 0.04795 -0.1162 0.9922 0.0354
-18.750 -1.0158 0.04982 0.04529 -0.1176 0.9907 0.0363
-18.500 -1.0088 0.04737 0.04278 -0.1190 0.9891 0.0368
-18.250 -1.0018 0.04489 0.04023 -0.1207 0.9874 0.0373
-18.000 -0.9936 0.04248 0.03778 -0.1224 0.9857 0.0381
-17.750 -0.9833 0.04029 0.03554 -0.1241 0.9842 0.0386
-17.500 -0.9700 0.03835 0.03356 -0.1258 0.9829 0.0394
-17.250 -0.9549 0.03651 0.03167 -0.1276 0.9816 0.0402
-17.000 -0.9486 0.03491 0.03002 -0.1273 0.9771 0.0410
-16.750 -0.9348 0.03344 0.02850 -0.1281 0.9735 0.0417
-16.250 -0.9093 0.03031 0.02530 -0.1297 0.9650 0.0432
-16.000 -0.8922 0.02896 0.02391 -0.1309 0.9602 0.0439
-15.750 -0.8693 0.02766 0.02257 -0.1330 0.9563 0.0452
-15.500 -0.8480 0.02654 0.02141 -0.1344 0.9489 0.0462
-15.250 -0.8181 0.02541 0.02022 -0.1375 0.9421 0.0472
-15.000 -0.7877 0.02422 0.01900 -0.1409 0.9324 0.0486
-14.750 -0.7477 0.02314 0.01787 -0.1459 0.9243 0.0504
-14.500 -0.7085 0.02223 0.01688 -0.1504 0.9124 0.0515
-14.250 -0.6719 0.02144 0.01599 -0.1542 0.8960 0.0527
-13.750 -0.6291 0.01995 0.01427 -0.1560 0.8553 0.0552
-13.500 -0.6154 0.01935 0.01357 -0.1550 0.8394 0.0561
-13.250 -0.6018 0.01879 0.01294 -0.1539 0.8272 0.0571
-13.000 -0.5884 0.01829 0.01235 -0.1526 0.8160 0.0582
-12.750 -0.5748 0.01781 0.01180 -0.1513 0.8053 0.0588
-12.500 -0.5634 0.01726 0.01120 -0.1496 0.7958 0.0603
-12.250 -0.5509 0.01676 0.01066 -0.1481 0.7870 0.0617
-12.000 -0.5379 0.01633 0.01017 -0.1464 0.7788 0.0628
-11.750 -0.5238 0.01591 0.00971 -0.1449 0.7713 0.0642
-11.500 -0.5099 0.01555 0.00929 -0.1433 0.7630 0.0652
-11.250 -0.4963 0.01515 0.00885 -0.1416 0.7562 0.0668
-11.000 -0.4829 0.01476 0.00844 -0.1398 0.7492 0.0684
-10.500 -0.4544 0.01411 0.00771 -0.1362 0.7361 0.0718
-10.250 -0.4391 0.01385 0.00740 -0.1345 0.7291 0.0730
-9.750 -0.4110 0.01326 0.00677 -0.1305 0.7173 0.0770
-9.500 -0.3958 0.01302 0.00649 -0.1286 0.7108 0.0791
-9.250 -0.3810 0.01282 0.00625 -0.1266 0.7043 0.0813
-9.000 -0.3660 0.01256 0.00599 -0.1246 0.6987 0.0840
-8.750 -0.3509 0.01234 0.00575 -0.1226 0.6928 0.0866
-8.500 -0.3357 0.01217 0.00554 -0.1204 0.6865 0.0889
-8.250 -0.3198 0.01199 0.00534 -0.1184 0.6811 0.0914
-8.000 -0.3052 0.01177 0.00513 -0.1162 0.6754 0.0954
-7.750 -0.2903 0.01162 0.00495 -0.1139 0.6694 0.0986
-7.500 -0.2750 0.01148 0.00478 -0.1117 0.6641 0.1015
-7.250 -0.2602 0.01130 0.00461 -0.1093 0.6593 0.1053
-7.000 -0.2458 0.01117 0.00446 -0.1068 0.6534 0.1090
-6.750 -0.2326 0.01108 0.00434 -0.1040 0.6481 0.1127
-6.500 -0.2200 0.01097 0.00424 -0.1011 0.6436 0.1172
-6.250 -0.2052 0.01087 0.00414 -0.0986 0.6386 0.1217
-6.000 -0.1885 0.01078 0.00403 -0.0965 0.6331 0.1259
-5.750 -0.1731 0.01067 0.00392 -0.0941 0.6279 0.1320
-5.250 -0.1361 0.01044 0.00371 -0.0906 0.6189 0.1435
-5.000 -0.1181 0.01036 0.00362 -0.0887 0.6137 0.1495
-4.750 -0.1012 0.01026 0.00352 -0.0866 0.6090 0.1568
-4.500 -0.0816 0.01014 0.00343 -0.0850 0.6049 0.1650
-4.250 -0.0634 0.01001 0.00333 -0.0832 0.6003 0.1746
-4.000 -0.0454 0.00992 0.00325 -0.0813 0.5953 0.1838
-3.750 -0.0291 0.00982 0.00316 -0.0790 0.5903 0.1959
-3.500 -0.0104 0.00968 0.00307 -0.0773 0.5866 0.2094
-3.250 0.0064 0.00954 0.00298 -0.0751 0.5822 0.2248
-3.000 0.0210 0.00942 0.00289 -0.0725 0.5774 0.2390
-2.750 0.0354 0.00932 0.00281 -0.0698 0.5728 0.2541
-2.500 0.0527 0.00917 0.00273 -0.0677 0.5684 0.2735
-2.250 0.0702 0.00903 0.00266 -0.0657 0.5642 0.2945
-2.000 0.0867 0.00890 0.00260 -0.0635 0.5597 0.3172
-1.750 0.1026 0.00882 0.00256 -0.0612 0.5546 0.3387
-1.500 0.1216 0.00870 0.00252 -0.0595 0.5505 0.3636
-1.000 0.1592 0.00853 0.00249 -0.0560 0.5411 0.4095
-0.750 0.1765 0.00850 0.00249 -0.0540 0.5361 0.4316
-0.500 0.1965 0.00842 0.00250 -0.0525 0.5318 0.4567
-0.250 0.2168 0.00838 0.00251 -0.0511 0.5270 0.4798
0.000 0.2359 0.00837 0.00255 -0.0494 0.5215 0.5013
0.250 0.2544 0.00839 0.00260 -0.0477 0.5167 0.5210
0.500 0.2758 0.00837 0.00264 -0.0465 0.5124 0.5389
0.750 0.2959 0.00839 0.00269 -0.0450 0.5066 0.5557
1.000 0.3153 0.00845 0.00276 -0.0434 0.5013 0.5701
1.250 0.3353 0.00848 0.00283 -0.0420 0.4968 0.5884
1.500 0.3565 0.00851 0.00290 -0.0408 0.4922 0.6039
1.750 0.3763 0.00858 0.00298 -0.0393 0.4867 0.6161
2.000 0.3947 0.00869 0.00309 -0.0376 0.4808 0.6265
2.250 0.4171 0.00875 0.00317 -0.0366 0.4766 0.6369
2.500 0.4379 0.00883 0.00326 -0.0354 0.4719 0.6461
2.750 0.4571 0.00895 0.00338 -0.0339 0.4668 0.6546
3.250 0.4980 0.00917 0.00361 -0.0314 0.4574 0.6691
3.500 0.5185 0.00929 0.00373 -0.0301 0.4525 0.6772
3.750 0.5366 0.00946 0.00389 -0.0285 0.4474 0.6838
4.000 0.5561 0.00959 0.00403 -0.0271 0.4434 0.6912
4.250 0.5774 0.00970 0.00417 -0.0261 0.4394 0.6989
4.500 0.5968 0.00985 0.00432 -0.0247 0.4346 0.7068
4.750 0.6134 0.01005 0.00453 -0.0228 0.4294 0.7156
5.250 0.6528 0.01036 0.00488 -0.0203 0.4215 0.7309
5.500 0.6721 0.01053 0.00507 -0.0190 0.4173 0.7388
5.750 0.6888 0.01077 0.00531 -0.0173 0.4126 0.7460
6.000 0.7061 0.01099 0.00555 -0.0156 0.4085 0.7540
6.250 0.7261 0.01117 0.00576 -0.0145 0.4042 0.7623
6.500 0.7438 0.01138 0.00601 -0.0130 0.4002 0.7713
6.750 0.7602 0.01165 0.00629 -0.0114 0.3959 0.7807
7.000 0.7759 0.01194 0.00660 -0.0096 0.3918 0.7903
7.250 0.7946 0.01215 0.00686 -0.0083 0.3880 0.8019
7.500 0.8116 0.01239 0.00715 -0.0068 0.3840 0.8148
7.750 0.8277 0.01268 0.00749 -0.0052 0.3796 0.8300
8.000 0.8419 0.01302 0.00790 -0.0033 0.3751 0.8507
8.250 0.8683 0.01323 0.00827 -0.0038 0.3711 0.8866
8.500 0.9336 0.01356 0.00872 -0.0127 0.3661 0.9211
8.750 1.0018 0.01407 0.00925 -0.0224 0.3601 0.9392
9.000 1.0576 0.01454 0.00974 -0.0293 0.3549 0.9562
9.250 1.1010 0.01498 0.01019 -0.0336 0.3503 0.9746
9.500 1.1287 0.01553 0.01073 -0.0348 0.3447 0.9867
10.000 1.1784 0.01681 0.01200 -0.0359 0.3349 1.0000
10.250 1.1909 0.01735 0.01254 -0.0341 0.3299 1.0000
10.500 1.2007 0.01805 0.01323 -0.0320 0.3248 1.0000
10.750 1.2140 0.01863 0.01382 -0.0304 0.3206 1.0000
11.000 1.2273 0.01925 0.01445 -0.0289 0.3150 1.0000
11.250 1.2340 0.02023 0.01539 -0.0267 0.3068 1.0000
11.500 1.2466 0.02096 0.01612 -0.0253 0.3000 1.0000
11.750 1.2509 0.02217 0.01727 -0.0231 0.2894 1.0000
12.000 1.2610 0.02309 0.01819 -0.0215 0.2806 1.0000
12.250 1.2701 0.02412 0.01920 -0.0200 0.2749 1.0000
12.500 1.2810 0.02507 0.02017 -0.0187 0.2690 1.0000
12.750 1.2914 0.02608 0.02118 -0.0174 0.2630 1.0000
13.000 1.2980 0.02736 0.02245 -0.0158 0.2565 1.0000
13.250 1.3079 0.02845 0.02354 -0.0146 0.2494 1.0000
13.500 1.3152 0.02974 0.02483 -0.0133 0.2435 1.0000
13.750 1.3212 0.03116 0.02624 -0.0119 0.2347 1.0000
14.000 1.3265 0.03266 0.02774 -0.0105 0.2279 1.0000
14.250 1.3317 0.03420 0.02926 -0.0092 0.2195 1.0000
14.500 1.3354 0.03589 0.03095 -0.0079 0.2127 1.0000
14.750 1.3377 0.03770 0.03274 -0.0066 0.2027 1.0000
15.000 1.3365 0.03984 0.03486 -0.0052 0.1936 1.0000
15.250 1.3353 0.04204 0.03704 -0.0039 0.1832 1.0000
15.500 1.3374 0.04400 0.03899 -0.0028 0.1754 1.0000
15.750 1.3293 0.04685 0.04180 -0.0013 0.1625 1.0000
16.000 1.3255 0.04943 0.04435 -0.0002 0.1537 1.0000
16.250 1.3223 0.05199 0.04689 0.0008 0.1433 1.0000
16.500 1.3196 0.05458 0.04948 0.0017 0.1364 1.0000
16.750 1.3140 0.05747 0.05235 0.0025 0.1278 1.0000
17.000 1.3070 0.06055 0.05540 0.0033 0.1173 1.0000
17.250 1.3014 0.06359 0.05844 0.0040 0.1094 1.0000
17.500 1.2971 0.06652 0.06138 0.0044 0.1032 1.0000
17.750 1.2897 0.06981 0.06465 0.0049 0.0948 1.0000
18.000 1.2847 0.07295 0.06780 0.0052 0.0887 1.0000
18.250 1.2810 0.07598 0.07083 0.0054 0.0834 1.0000
18.500 1.2785 0.07895 0.07383 0.0055 0.0793 1.0000
18.750 1.2743 0.08209 0.07698 0.0055 0.0750 1.0000
19.000 1.2720 0.08509 0.08001 0.0054 0.0711 1.0000
19.250 1.2699 0.08807 0.08302 0.0053 0.0683 1.0000
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