FX 84-W-175 (fx84w175-il) Xfoil prediction polar at RE=100,000 Ncrit=5
| Details | Polar file |
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Airfoil: FX 84-W-175 (fx84w175-il) Reynolds number: 100,000 Max Cl/Cd: 34.13 at α=8° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx84w175-il-100000-n5.txt Download as CSV file: xf-fx84w175-il-100000-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 = 0.100 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-12.250 -0.1821 0.09801 0.09243 -0.1041 0.9281 0.0496
-12.000 -0.1836 0.09331 0.08772 -0.1068 0.9211 0.0505
-11.500 -0.4029 0.05099 0.04465 -0.1341 0.8977 0.0487
-11.250 -0.4125 0.04861 0.04213 -0.1338 0.8891 0.0492
-11.000 -0.4235 0.04630 0.03963 -0.1328 0.8804 0.0498
-10.750 -0.4329 0.04448 0.03762 -0.1307 0.8723 0.0504
-10.500 -0.4429 0.04282 0.03574 -0.1278 0.8642 0.0511
-10.250 -0.4464 0.04087 0.03349 -0.1255 0.8585 0.0520
-10.000 -0.4490 0.03913 0.03146 -0.1230 0.8505 0.0529
-9.750 -0.4469 0.03715 0.02904 -0.1208 0.8448 0.0541
-9.500 -0.4331 0.03599 0.02778 -0.1196 0.8405 0.0554
-9.250 -0.4207 0.03529 0.02703 -0.1181 0.8337 0.0567
-9.000 -0.4060 0.03427 0.02585 -0.1168 0.8287 0.0585
-8.750 -0.3898 0.03295 0.02423 -0.1157 0.8250 0.0606
-8.500 -0.3757 0.03185 0.02289 -0.1141 0.8191 0.0623
-8.250 -0.3577 0.03117 0.02222 -0.1132 0.8138 0.0640
-8.000 -0.3376 0.03042 0.02137 -0.1123 0.8098 0.0665
-7.750 -0.3156 0.02944 0.02013 -0.1116 0.8067 0.0697
-7.500 -0.2994 0.02884 0.01950 -0.1103 0.8003 0.0719
-7.250 -0.2798 0.02827 0.01892 -0.1093 0.7954 0.0746
-7.000 -0.2570 0.02757 0.01806 -0.1087 0.7918 0.0785
-6.750 -0.2329 0.02680 0.01723 -0.1082 0.7889 0.0822
-6.500 -0.2169 0.02651 0.01694 -0.1067 0.7824 0.0858
-6.250 -0.1957 0.02603 0.01631 -0.1058 0.7777 0.0908
-6.000 -0.1727 0.02543 0.01575 -0.1052 0.7742 0.0956
-5.750 -0.1470 0.02486 0.01507 -0.1049 0.7715 0.1022
-5.500 -0.1318 0.02464 0.01491 -0.1032 0.7650 0.1074
-5.250 -0.1106 0.02430 0.01451 -0.1023 0.7602 0.1150
-5.000 -0.0867 0.02380 0.01404 -0.1018 0.7568 0.1235
-4.750 -0.0605 0.02329 0.01349 -0.1015 0.7542 0.1340
-4.500 -0.0449 0.02323 0.01345 -0.0998 0.7478 0.1443
-4.250 -0.0243 0.02294 0.01321 -0.0989 0.7429 0.1569
-4.000 0.0006 0.02253 0.01282 -0.0985 0.7397 0.1735
-3.750 0.0276 0.02207 0.01238 -0.0984 0.7371 0.1949
-3.500 0.0429 0.02204 0.01246 -0.0967 0.7308 0.2160
-3.250 0.0630 0.02179 0.01233 -0.0956 0.7259 0.2458
-3.000 0.0878 0.02135 0.01203 -0.0953 0.7226 0.2883
-2.750 0.1138 0.02078 0.01171 -0.0951 0.7201 0.3488
-2.500 0.1273 0.02071 0.01194 -0.0930 0.7139 0.4153
-2.250 0.1448 0.02051 0.01209 -0.0912 0.7088 0.4974
-2.000 0.1686 0.02029 0.01212 -0.0900 0.7056 0.5768
-1.750 0.1957 0.02015 0.01207 -0.0892 0.7031 0.6367
-1.500 0.2100 0.02050 0.01250 -0.0867 0.6972 0.6748
-1.250 0.2278 0.02074 0.01277 -0.0847 0.6918 0.7068
-1.000 0.2531 0.02077 0.01276 -0.0836 0.6886 0.7357
-0.750 0.2810 0.02073 0.01266 -0.0829 0.6862 0.7611
-0.500 0.2929 0.02117 0.01311 -0.0801 0.6800 0.7820
-0.250 0.3091 0.02143 0.01336 -0.0778 0.6746 0.8020
0.000 0.3340 0.02143 0.01330 -0.0767 0.6715 0.8217
0.250 0.3615 0.02135 0.01315 -0.0759 0.6691 0.8414
0.500 0.3662 0.02190 0.01375 -0.0718 0.6620 0.8607
0.750 0.3824 0.02210 0.01393 -0.0693 0.6571 0.8807
1.000 0.4107 0.02201 0.01379 -0.0688 0.6542 0.8982
1.250 0.4443 0.02183 0.01352 -0.0695 0.6520 0.9113
1.500 0.4526 0.02247 0.01420 -0.0669 0.6444 0.9270
1.750 0.4854 0.02257 0.01426 -0.0680 0.6401 0.9376
2.000 0.5259 0.02247 0.01408 -0.0704 0.6374 0.9463
2.250 0.5692 0.02227 0.01381 -0.0732 0.6353 0.9543
2.500 0.5944 0.02291 0.01447 -0.0741 0.6285 0.9664
2.750 0.6316 0.02312 0.01466 -0.0765 0.6238 0.9755
3.000 0.6749 0.02302 0.01451 -0.0796 0.6208 0.9829
3.250 0.7225 0.02279 0.01422 -0.0833 0.6185 0.9881
3.500 0.7213 0.02365 0.01513 -0.0800 0.6105 1.0000
3.750 0.7240 0.02383 0.01527 -0.0762 0.6053 1.0000
4.000 0.7546 0.02364 0.01503 -0.0767 0.6026 1.0000
4.250 0.7886 0.02345 0.01477 -0.0777 0.6001 1.0000
4.500 0.7583 0.02502 0.01638 -0.0699 0.5892 1.0000
4.750 0.7922 0.02484 0.01617 -0.0708 0.5865 1.0000
5.000 0.8325 0.02450 0.01579 -0.0727 0.5844 1.0000
5.500 0.8413 0.02630 0.01761 -0.0672 0.5703 1.0000
5.750 0.8806 0.02590 0.01720 -0.0687 0.5682 1.0000
6.250 0.8924 0.02794 0.01928 -0.0641 0.5540 1.0000
6.500 0.9314 0.02746 0.01880 -0.0654 0.5517 1.0000
7.000 0.9440 0.02967 0.02109 -0.0613 0.5373 1.0000
7.250 0.9837 0.02907 0.02051 -0.0625 0.5351 1.0000
7.750 0.9973 0.03134 0.02287 -0.0587 0.5203 1.0000
8.000 1.0400 0.03047 0.02201 -0.0600 0.5180 1.0000
8.250 1.0157 0.03353 0.02515 -0.0556 0.5058 1.0000
8.500 1.0537 0.03279 0.02444 -0.0564 0.5029 1.0000
9.000 1.0710 0.03508 0.02684 -0.0534 0.4879 1.0000
9.250 1.1140 0.03394 0.02575 -0.0545 0.4852 1.0000
9.500 1.0917 0.03725 0.02915 -0.0509 0.4730 1.0000
9.750 1.1312 0.03622 0.02815 -0.0516 0.4697 1.0000
10.250 1.1508 0.03844 0.03051 -0.0490 0.4540 1.0000
10.750 1.1726 0.04055 0.03276 -0.0468 0.4381 1.0000
11.000 1.1730 0.04251 0.03480 -0.0452 0.4286 1.0000
11.250 1.1979 0.04237 0.03471 -0.0448 0.4214 1.0000
11.500 1.1947 0.04464 0.03706 -0.0432 0.4105 1.0000
11.750 1.2322 0.04322 0.03564 -0.0432 0.4028 1.0000
12.000 1.2205 0.04630 0.03881 -0.0414 0.3899 1.0000
12.250 1.2238 0.04810 0.04068 -0.0402 0.3782 1.0000
12.500 1.2410 0.04853 0.04112 -0.0395 0.3671 1.0000
12.750 1.2503 0.04978 0.04239 -0.0386 0.3548 1.0000
13.000 1.2473 0.05242 0.04510 -0.0376 0.3417 1.0000
13.250 1.2508 0.05444 0.04717 -0.0368 0.3288 1.0000
13.500 1.2565 0.05624 0.04899 -0.0361 0.3156 1.0000
13.750 1.2623 0.05807 0.05082 -0.0354 0.3021 1.0000
14.000 1.2667 0.06008 0.05283 -0.0348 0.2881 1.0000
14.250 1.2693 0.06236 0.05510 -0.0343 0.2736 1.0000
14.500 1.2700 0.06493 0.05765 -0.0338 0.2589 1.0000
14.750 1.2693 0.06777 0.06050 -0.0335 0.2441 1.0000
15.000 1.2680 0.07075 0.06347 -0.0333 0.2295 1.0000
15.250 1.2657 0.07390 0.06661 -0.0332 0.2148 1.0000
15.500 1.2631 0.07720 0.06990 -0.0332 0.2005 1.0000
15.750 1.2598 0.08066 0.07335 -0.0334 0.1865 1.0000
16.000 1.2558 0.08430 0.07697 -0.0338 0.1730 1.0000
16.250 1.2517 0.08801 0.08068 -0.0342 0.1601 1.0000
16.500 1.2476 0.09182 0.08447 -0.0348 0.1479 1.0000
16.750 1.2434 0.09568 0.08833 -0.0354 0.1370 1.0000
17.000 1.2389 0.09966 0.09226 -0.0363 0.1269 1.0000
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