FX 84-W-175 (fx84w175-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: FX 84-W-175 (fx84w175-il) Reynolds number: 500,000 Max Cl/Cd: 100.07 at α=6° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx84w175-il-500000-n5.txt Download as CSV file: xf-fx84w175-il-500000-n5.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 = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-17.750 -0.5965 0.10720 0.10410 -0.0774 0.9663 0.0200
-17.500 -0.6384 0.09400 0.09066 -0.0867 0.9595 0.0200
-17.250 -0.6648 0.08371 0.08017 -0.0951 0.9511 0.0201
-17.000 -0.6850 0.07497 0.07124 -0.1025 0.9407 0.0202
-16.500 -0.7214 0.06112 0.05704 -0.1128 0.9152 0.0204
-16.250 -0.7393 0.05521 0.05096 -0.1165 0.9037 0.0205
-16.000 -0.7530 0.05026 0.04584 -0.1194 0.8936 0.0206
-15.750 -0.7636 0.04599 0.04143 -0.1218 0.8841 0.0208
-15.500 -0.7710 0.04241 0.03770 -0.1234 0.8758 0.0209
-15.250 -0.7765 0.03929 0.03445 -0.1247 0.8675 0.0211
-15.000 -0.7797 0.03668 0.03170 -0.1253 0.8601 0.0212
-14.750 -0.7803 0.03442 0.02933 -0.1257 0.8530 0.0214
-14.500 -0.7798 0.03243 0.02722 -0.1256 0.8463 0.0216
-14.250 -0.7771 0.03074 0.02541 -0.1252 0.8402 0.0220
-14.000 -0.7735 0.02919 0.02375 -0.1247 0.8338 0.0221
-13.750 -0.7684 0.02785 0.02230 -0.1239 0.8277 0.0224
-13.500 -0.7622 0.02664 0.02098 -0.1229 0.8225 0.0228
-13.250 -0.7552 0.02550 0.01973 -0.1218 0.8170 0.0231
-13.000 -0.7465 0.02454 0.01866 -0.1206 0.8114 0.0234
-12.750 -0.7371 0.02367 0.01766 -0.1192 0.8064 0.0237
-12.500 -0.7298 0.02269 0.01663 -0.1176 0.8012 0.0240
-12.250 -0.7196 0.02194 0.01583 -0.1160 0.7961 0.0245
-12.000 -0.7090 0.02127 0.01508 -0.1142 0.7913 0.0249
-11.750 -0.6971 0.02074 0.01448 -0.1124 0.7869 0.0254
-11.500 -0.6836 0.02023 0.01390 -0.1107 0.7821 0.0258
-11.250 -0.6670 0.01969 0.01328 -0.1095 0.7776 0.0264
-11.000 -0.6489 0.01919 0.01268 -0.1084 0.7734 0.0270
-10.750 -0.6297 0.01872 0.01211 -0.1075 0.7695 0.0274
-10.500 -0.6109 0.01816 0.01152 -0.1065 0.7652 0.0280
-10.250 -0.5906 0.01768 0.01099 -0.1058 0.7610 0.0287
-10.000 -0.5690 0.01727 0.01052 -0.1051 0.7571 0.0294
-9.750 -0.5468 0.01689 0.01007 -0.1045 0.7534 0.0303
-9.500 -0.5236 0.01651 0.00964 -0.1041 0.7495 0.0312
-9.250 -0.5006 0.01612 0.00919 -0.1036 0.7452 0.0321
-9.000 -0.4777 0.01571 0.00876 -0.1031 0.7413 0.0331
-8.750 -0.4539 0.01538 0.00837 -0.1026 0.7377 0.0341
-8.500 -0.4295 0.01506 0.00799 -0.1023 0.7341 0.0352
-8.250 -0.4046 0.01475 0.00764 -0.1020 0.7300 0.0363
-8.000 -0.3801 0.01441 0.00728 -0.1017 0.7259 0.0378
-7.750 -0.3551 0.01412 0.00696 -0.1015 0.7222 0.0394
-7.500 -0.3296 0.01388 0.00664 -0.1012 0.7187 0.0410
-7.250 -0.3040 0.01359 0.00634 -0.1010 0.7147 0.0426
-7.000 -0.2782 0.01331 0.00606 -0.1009 0.7106 0.0445
-6.750 -0.2521 0.01309 0.00579 -0.1007 0.7068 0.0467
-6.500 -0.2261 0.01286 0.00552 -0.1006 0.7031 0.0492
-6.250 -0.1998 0.01263 0.00529 -0.1005 0.6994 0.0520
-6.000 -0.1730 0.01243 0.00506 -0.1004 0.6954 0.0547
-5.750 -0.1466 0.01221 0.00484 -0.1004 0.6915 0.0582
-5.500 -0.1197 0.01205 0.00464 -0.1003 0.6877 0.0619
-5.250 -0.0931 0.01185 0.00444 -0.1002 0.6840 0.0664
-5.000 -0.0659 0.01168 0.00427 -0.1003 0.6802 0.0709
-4.750 -0.0389 0.01150 0.00410 -0.1003 0.6763 0.0768
-4.500 -0.0118 0.01134 0.00394 -0.1003 0.6724 0.0826
-4.250 0.0153 0.01120 0.00378 -0.1003 0.6686 0.0896
-4.000 0.0426 0.01104 0.00365 -0.1003 0.6649 0.0977
-3.750 0.0700 0.01089 0.00352 -0.1004 0.6609 0.1065
-3.250 0.1245 0.01063 0.00329 -0.1004 0.6530 0.1298
-3.000 0.1518 0.01049 0.00318 -0.1005 0.6493 0.1448
-2.750 0.1793 0.01034 0.00310 -0.1006 0.6454 0.1620
-2.500 0.2066 0.01019 0.00301 -0.1007 0.6413 0.1825
-2.250 0.2337 0.01005 0.00293 -0.1007 0.6372 0.2079
-2.000 0.2608 0.00990 0.00285 -0.1008 0.6334 0.2374
-1.750 0.2880 0.00971 0.00279 -0.1009 0.6295 0.2743
-1.500 0.3149 0.00950 0.00273 -0.1010 0.6252 0.3214
-1.250 0.3415 0.00928 0.00267 -0.1010 0.6211 0.3779
-0.750 0.3947 0.00885 0.00263 -0.1010 0.6133 0.5081
-0.500 0.4216 0.00870 0.00265 -0.1010 0.6089 0.5623
-0.250 0.4486 0.00863 0.00268 -0.1010 0.6046 0.6040
0.000 0.4758 0.00863 0.00272 -0.1009 0.6008 0.6361
0.250 0.5034 0.00861 0.00278 -0.1009 0.5969 0.6623
0.500 0.5308 0.00862 0.00284 -0.1009 0.5924 0.6852
0.750 0.5580 0.00865 0.00290 -0.1008 0.5880 0.7037
1.000 0.5851 0.00872 0.00295 -0.1007 0.5840 0.7197
1.250 0.6126 0.00875 0.00303 -0.1007 0.5800 0.7347
1.500 0.6396 0.00881 0.00311 -0.1006 0.5754 0.7509
1.750 0.6661 0.00888 0.00319 -0.1004 0.5709 0.7679
2.000 0.6922 0.00897 0.00329 -0.1000 0.5668 0.7811
2.250 0.7192 0.00903 0.00337 -0.1000 0.5624 0.7900
2.500 0.7457 0.00910 0.00346 -0.0998 0.5576 0.7978
3.000 0.7978 0.00929 0.00364 -0.0993 0.5487 0.8121
3.250 0.8241 0.00938 0.00374 -0.0992 0.5439 0.8194
3.500 0.8496 0.00948 0.00384 -0.0989 0.5389 0.8260
3.750 0.8741 0.00960 0.00395 -0.0983 0.5343 0.8326
4.000 0.8998 0.00970 0.00408 -0.0981 0.5297 0.8396
4.250 0.9244 0.00980 0.00420 -0.0976 0.5246 0.8459
4.500 0.9478 0.00993 0.00433 -0.0969 0.5196 0.8530
4.750 0.9720 0.01006 0.00447 -0.0964 0.5150 0.8601
5.000 0.9950 0.01016 0.00462 -0.0956 0.5099 0.8669
5.250 1.0171 0.01031 0.00477 -0.0947 0.5045 0.8747
5.500 1.0379 0.01046 0.00494 -0.0935 0.4993 0.8822
5.750 1.0579 0.01058 0.00510 -0.0922 0.4931 0.8911
6.000 1.0737 0.01073 0.00527 -0.0900 0.4869 0.9008
6.250 1.0903 0.01090 0.00547 -0.0880 0.4812 0.9122
6.500 1.1061 0.01107 0.00568 -0.0859 0.4748 0.9261
6.750 1.1208 0.01130 0.00593 -0.0837 0.4684 0.9453
7.000 1.1479 0.01151 0.00618 -0.0841 0.4617 0.9699
7.250 1.1713 0.01179 0.00646 -0.0839 0.4548 1.0000
7.500 1.1902 0.01211 0.00678 -0.0828 0.4486 1.0000
7.750 1.2090 0.01243 0.00711 -0.0817 0.4414 1.0000
8.000 1.2247 0.01287 0.00752 -0.0802 0.4339 1.0000
8.250 1.2428 0.01324 0.00791 -0.0791 0.4261 1.0000
8.500 1.2567 0.01377 0.00841 -0.0773 0.4173 1.0000
8.750 1.2692 0.01436 0.00898 -0.0755 0.4049 1.0000
9.000 1.2786 0.01511 0.00969 -0.0733 0.3898 1.0000
9.250 1.2883 0.01590 0.01043 -0.0712 0.3755 1.0000
9.500 1.2979 0.01675 0.01123 -0.0692 0.3617 1.0000
9.750 1.3066 0.01767 0.01211 -0.0672 0.3482 1.0000
10.000 1.3145 0.01867 0.01308 -0.0652 0.3349 1.0000
10.250 1.3210 0.01980 0.01416 -0.0632 0.3202 1.0000
10.500 1.3268 0.02101 0.01532 -0.0611 0.3052 1.0000
10.750 1.3318 0.02232 0.01657 -0.0591 0.2899 1.0000
11.000 1.3354 0.02376 0.01796 -0.0571 0.2740 1.0000
11.250 1.3374 0.02538 0.01951 -0.0550 0.2558 1.0000
11.500 1.3388 0.02711 0.02118 -0.0530 0.2381 1.0000
11.750 1.3412 0.02885 0.02286 -0.0513 0.2225 1.0000
12.000 1.3430 0.03070 0.02465 -0.0496 0.2070 1.0000
12.250 1.3435 0.03272 0.02661 -0.0480 0.1907 1.0000
12.500 1.3456 0.03469 0.02853 -0.0466 0.1767 1.0000
12.750 1.3463 0.03682 0.03060 -0.0452 0.1613 1.0000
13.000 1.3471 0.03903 0.03276 -0.0440 0.1473 1.0000
13.250 1.3479 0.04131 0.03500 -0.0429 0.1338 1.0000
13.500 1.3490 0.04361 0.03726 -0.0419 0.1212 1.0000
13.750 1.3490 0.04609 0.03969 -0.0409 0.1087 1.0000
14.000 1.3498 0.04856 0.04214 -0.0402 0.0984 1.0000
14.250 1.3518 0.05097 0.04453 -0.0395 0.0897 1.0000
14.500 1.3547 0.05335 0.04691 -0.0390 0.0824 1.0000
14.750 1.3579 0.05575 0.04932 -0.0386 0.0761 1.0000
15.000 1.3599 0.05833 0.05189 -0.0383 0.0699 1.0000
15.250 1.3636 0.06077 0.05437 -0.0381 0.0649 1.0000
15.500 1.3663 0.06335 0.05695 -0.0379 0.0600 1.0000
15.750 1.3687 0.06602 0.05965 -0.0378 0.0556 1.0000
16.000 1.3724 0.06860 0.06225 -0.0378 0.0523 1.0000
16.250 1.3752 0.07132 0.06501 -0.0379 0.0488 1.0000
16.500 1.3780 0.07408 0.06781 -0.0380 0.0462 1.0000
16.750 1.3811 0.07683 0.07061 -0.0382 0.0435 1.0000
17.000 1.3827 0.07981 0.07362 -0.0385 0.0408 1.0000
17.250 1.3859 0.08264 0.07651 -0.0389 0.0389 1.0000
17.500 1.3884 0.08558 0.07950 -0.0393 0.0368 1.0000
17.750 1.3893 0.08878 0.08274 -0.0399 0.0349 1.0000
18.000 1.3922 0.09173 0.08576 -0.0404 0.0332 1.0000
18.250 1.3937 0.09489 0.08897 -0.0411 0.0317 1.0000
18.750 1.3964 0.10138 0.09558 -0.0427 0.0290 1.0000
19.000 1.3976 0.10467 0.09894 -0.0436 0.0277 1.0000
19.250 1.3981 0.10808 0.10240 -0.0445 0.0266 1.0000
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