FX 84-W-175 (fx84w175-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: FX 84-W-175 (fx84w175-il) Reynolds number: 1,000,000 Max Cl/Cd: 135.12 at α=6.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx84w175-il-1000000.txt Download as CSV file: xf-fx84w175-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: FX 84-W-175
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 1.000 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-18.500 -0.7025 0.10200 0.09954 -0.0773 1.0000 0.0195
-18.250 -0.7355 0.09270 0.09010 -0.0827 1.0000 0.0196
-18.000 -0.7659 0.08415 0.08142 -0.0879 1.0000 0.0196
-17.750 -0.7953 0.07607 0.07321 -0.0928 1.0000 0.0197
-17.500 -0.8177 0.06917 0.06620 -0.0970 1.0000 0.0197
-17.250 -0.8263 0.06195 0.05883 -0.1043 0.9749 0.0198
-17.000 -0.8266 0.05502 0.05172 -0.1129 0.9645 0.0199
-16.750 -0.8188 0.04968 0.04619 -0.1203 0.9509 0.0201
-16.500 -0.8205 0.04537 0.04168 -0.1243 0.9309 0.0201
-16.250 -0.8313 0.04151 0.03763 -0.1260 0.9142 0.0202
-16.000 -0.8465 0.03764 0.03359 -0.1271 0.9011 0.0204
-15.750 -0.8558 0.03462 0.03043 -0.1276 0.8906 0.0206
-15.500 -0.8603 0.03220 0.02790 -0.1276 0.8812 0.0209
-15.250 -0.8616 0.03018 0.02578 -0.1274 0.8733 0.0211
-15.000 -0.8593 0.02854 0.02405 -0.1268 0.8655 0.0213
-14.750 -0.8552 0.02716 0.02257 -0.1261 0.8584 0.0215
-14.500 -0.8506 0.02579 0.02114 -0.1252 0.8521 0.0217
-14.250 -0.8427 0.02476 0.02002 -0.1242 0.8458 0.0220
-14.000 -0.8330 0.02387 0.01905 -0.1232 0.8399 0.0224
-13.750 -0.8248 0.02290 0.01800 -0.1220 0.8342 0.0226
-13.500 -0.8137 0.02215 0.01716 -0.1207 0.8286 0.0230
-13.250 -0.8039 0.02138 0.01629 -0.1192 0.8231 0.0233
-13.000 -0.7919 0.02070 0.01554 -0.1179 0.8183 0.0235
-12.750 -0.7802 0.02006 0.01482 -0.1163 0.8129 0.0237
-12.500 -0.7803 0.01900 0.01365 -0.1131 0.8071 0.0242
-12.250 -0.7719 0.01839 0.01301 -0.1106 0.8027 0.0247
-12.000 -0.7568 0.01789 0.01247 -0.1091 0.7982 0.0251
-11.750 -0.7386 0.01744 0.01197 -0.1080 0.7936 0.0255
-11.500 -0.7193 0.01705 0.01149 -0.1070 0.7889 0.0260
-11.250 -0.6987 0.01662 0.01102 -0.1062 0.7854 0.0265
-11.000 -0.6770 0.01623 0.01058 -0.1056 0.7814 0.0270
-10.750 -0.6541 0.01591 0.01019 -0.1050 0.7772 0.0275
-10.500 -0.6360 0.01527 0.00948 -0.1039 0.7728 0.0283
-10.250 -0.6138 0.01485 0.00904 -0.1033 0.7690 0.0291
-10.000 -0.5899 0.01451 0.00868 -0.1029 0.7654 0.0298
-9.750 -0.5656 0.01419 0.00832 -0.1026 0.7615 0.0306
-9.500 -0.5410 0.01391 0.00798 -0.1022 0.7574 0.0314
-9.250 -0.5167 0.01361 0.00760 -0.1019 0.7531 0.0320
-9.000 -0.4936 0.01312 0.00711 -0.1014 0.7498 0.0333
-8.750 -0.4681 0.01283 0.00680 -0.1012 0.7460 0.0343
-8.500 -0.4423 0.01258 0.00652 -0.1010 0.7421 0.0355
-8.250 -0.4159 0.01241 0.00628 -0.1009 0.7380 0.0364
-8.000 -0.3914 0.01201 0.00586 -0.1005 0.7343 0.0381
-7.750 -0.3650 0.01174 0.00560 -0.1005 0.7307 0.0396
-7.500 -0.3381 0.01153 0.00536 -0.1004 0.7268 0.0411
-7.250 -0.3119 0.01128 0.00507 -0.1003 0.7229 0.0428
-7.000 -0.2857 0.01106 0.00482 -0.1002 0.7187 0.0450
-6.750 -0.2581 0.01087 0.00463 -0.1002 0.7156 0.0471
-6.500 -0.2313 0.01061 0.00437 -0.1002 0.7117 0.0498
-6.250 -0.2041 0.01042 0.00417 -0.1002 0.7078 0.0526
-6.000 -0.1769 0.01026 0.00397 -0.1002 0.7039 0.0555
-5.750 -0.1496 0.01006 0.00379 -0.1003 0.7003 0.0595
-5.500 -0.1218 0.00989 0.00362 -0.1004 0.6967 0.0634
-5.250 -0.0942 0.00970 0.00345 -0.1004 0.6927 0.0684
-5.000 -0.0666 0.00955 0.00329 -0.1005 0.6888 0.0736
-4.750 -0.0390 0.00945 0.00316 -0.1006 0.6847 0.0794
-4.500 -0.0110 0.00925 0.00302 -0.1007 0.6815 0.0871
-4.250 0.0171 0.00911 0.00290 -0.1009 0.6776 0.0949
-4.000 0.0451 0.00898 0.00278 -0.1010 0.6736 0.1035
-3.750 0.0727 0.00885 0.00267 -0.1011 0.6697 0.1153
-3.500 0.1008 0.00871 0.00257 -0.1013 0.6660 0.1287
-3.250 0.1290 0.00855 0.00248 -0.1015 0.6623 0.1448
-2.750 0.1847 0.00827 0.00231 -0.1018 0.6542 0.1869
-2.250 0.2405 0.00794 0.00217 -0.1022 0.6466 0.2502
-2.000 0.2682 0.00772 0.00210 -0.1024 0.6426 0.2946
-1.750 0.2954 0.00749 0.00204 -0.1026 0.6385 0.3531
-1.500 0.3222 0.00725 0.00199 -0.1027 0.6340 0.4237
-1.250 0.3499 0.00698 0.00196 -0.1029 0.6306 0.4971
-1.000 0.3778 0.00680 0.00195 -0.1031 0.6267 0.5559
-0.750 0.4059 0.00671 0.00196 -0.1032 0.6226 0.5997
-0.500 0.4337 0.00669 0.00198 -0.1033 0.6181 0.6323
-0.250 0.4624 0.00666 0.00202 -0.1035 0.6144 0.6585
0.000 0.4910 0.00664 0.00205 -0.1037 0.6105 0.6804
0.250 0.5194 0.00665 0.00208 -0.1039 0.6063 0.6985
0.500 0.5474 0.00671 0.00212 -0.1040 0.6018 0.7139
0.750 0.5760 0.00674 0.00217 -0.1042 0.5979 0.7277
1.000 0.6045 0.00675 0.00222 -0.1044 0.5938 0.7407
1.250 0.6327 0.00680 0.00227 -0.1045 0.5894 0.7519
1.500 0.6601 0.00689 0.00233 -0.1045 0.5846 0.7625
1.750 0.6885 0.00692 0.00239 -0.1047 0.5808 0.7725
2.000 0.7166 0.00697 0.00246 -0.1048 0.5764 0.7832
2.250 0.7438 0.00703 0.00253 -0.1047 0.5717 0.7944
2.500 0.7708 0.00716 0.00262 -0.1047 0.5669 0.8052
2.750 0.7984 0.00718 0.00270 -0.1047 0.5629 0.8133
3.000 0.8260 0.00725 0.00277 -0.1047 0.5582 0.8207
3.250 0.8526 0.00734 0.00285 -0.1046 0.5534 0.8270
3.500 0.8791 0.00743 0.00295 -0.1045 0.5488 0.8336
3.750 0.9067 0.00749 0.00303 -0.1046 0.5444 0.8401
4.000 0.9329 0.00757 0.00312 -0.1044 0.5395 0.8463
4.250 0.9577 0.00771 0.00324 -0.1039 0.5342 0.8528
4.500 0.9849 0.00778 0.00333 -0.1040 0.5298 0.8591
4.750 1.0101 0.00785 0.00343 -0.1036 0.5242 0.8654
5.000 1.0336 0.00800 0.00356 -0.1029 0.5182 0.8723
5.250 1.0594 0.00808 0.00367 -0.1027 0.5130 0.8789
5.500 1.0829 0.00818 0.00379 -0.1020 0.5072 0.8857
5.750 1.1049 0.00835 0.00394 -0.1010 0.5011 0.8934
6.000 1.1283 0.00842 0.00407 -0.1003 0.4959 0.9007
6.250 1.1502 0.00855 0.00421 -0.0993 0.4900 0.9092
6.500 1.1662 0.00871 0.00437 -0.0972 0.4841 0.9194
6.750 1.1850 0.00877 0.00450 -0.0955 0.4787 0.9307
7.000 1.1979 0.00891 0.00467 -0.0927 0.4726 0.9481
7.250 1.2190 0.00910 0.00489 -0.0917 0.4663 0.9753
7.500 1.2473 0.00928 0.00508 -0.0924 0.4587 1.0000
7.750 1.2646 0.00960 0.00537 -0.0910 0.4497 1.0000
8.000 1.2821 0.00993 0.00566 -0.0896 0.4386 1.0000
8.250 1.2992 0.01028 0.00599 -0.0881 0.4281 1.0000
8.500 1.3132 0.01073 0.00640 -0.0862 0.4178 1.0000
8.750 1.3312 0.01109 0.00675 -0.0850 0.4084 1.0000
9.000 1.3456 0.01158 0.00721 -0.0833 0.3987 1.0000
9.250 1.3591 0.01212 0.00773 -0.0815 0.3879 1.0000
9.500 1.3737 0.01265 0.00824 -0.0799 0.3766 1.0000
9.750 1.3847 0.01334 0.00888 -0.0778 0.3635 1.0000
10.000 1.3951 0.01409 0.00959 -0.0758 0.3509 1.0000
10.250 1.4041 0.01494 0.01038 -0.0736 0.3366 1.0000
10.500 1.4117 0.01589 0.01128 -0.0714 0.3217 1.0000
10.750 1.4178 0.01695 0.01228 -0.0691 0.3049 1.0000
11.000 1.4232 0.01811 0.01337 -0.0668 0.2879 1.0000
11.250 1.4277 0.01935 0.01454 -0.0645 0.2708 1.0000
11.500 1.4306 0.02073 0.01585 -0.0621 0.2533 1.0000
11.750 1.4319 0.02228 0.01732 -0.0598 0.2349 1.0000
12.000 1.4332 0.02390 0.01886 -0.0576 0.2177 1.0000
12.250 1.4358 0.02550 0.02040 -0.0556 0.2024 1.0000
12.500 1.4370 0.02727 0.02210 -0.0536 0.1867 1.0000
12.750 1.4377 0.02914 0.02391 -0.0518 0.1715 1.0000
13.000 1.4373 0.03117 0.02586 -0.0500 0.1558 1.0000
13.250 1.4372 0.03324 0.02787 -0.0484 0.1408 1.0000
13.500 1.4371 0.03540 0.02996 -0.0468 0.1269 1.0000
13.750 1.4366 0.03767 0.03217 -0.0455 0.1137 1.0000
14.000 1.4365 0.03996 0.03442 -0.0442 0.1016 1.0000
14.250 1.4374 0.04224 0.03666 -0.0432 0.0914 1.0000
14.500 1.4395 0.04447 0.03888 -0.0423 0.0834 1.0000
14.750 1.4425 0.04668 0.04108 -0.0415 0.0762 1.0000
15.000 1.4437 0.04913 0.04351 -0.0408 0.0692 1.0000
15.250 1.4468 0.05144 0.04582 -0.0403 0.0640 1.0000
15.500 1.4505 0.05372 0.04811 -0.0398 0.0591 1.0000
15.750 1.4522 0.05627 0.05066 -0.0394 0.0549 1.0000
16.000 1.4566 0.05857 0.05299 -0.0391 0.0508 1.0000
16.250 1.4577 0.06130 0.05573 -0.0389 0.0473 1.0000
16.500 1.4625 0.06363 0.05809 -0.0388 0.0444 1.0000
16.750 1.4640 0.06640 0.06088 -0.0387 0.0417 1.0000
17.000 1.4676 0.06897 0.06349 -0.0387 0.0393 1.0000
17.250 1.4700 0.07172 0.06627 -0.0388 0.0371 1.0000
17.500 1.4705 0.07474 0.06933 -0.0390 0.0349 1.0000
17.750 1.4745 0.07735 0.07199 -0.0393 0.0332 1.0000
18.000 1.4755 0.08040 0.07507 -0.0396 0.0315 1.0000
18.250 1.4761 0.08354 0.07825 -0.0400 0.0300 1.0000
18.500 1.4791 0.08642 0.08119 -0.0405 0.0286 1.0000
18.750 1.4804 0.08952 0.08433 -0.0411 0.0274 1.0000
19.000 1.4778 0.09320 0.08806 -0.0418 0.0261 1.0000
19.250 1.4811 0.09610 0.09102 -0.0425 0.0252 1.0000
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