FX 84-W-218 (fx84w218-il) Xfoil prediction polar at RE=100,000 Ncrit=5
| Details | Polar file |
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Airfoil: FX 84-W-218 (fx84w218-il) Reynolds number: 100,000 Max Cl/Cd: 24.66 at α=6.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx84w218-il-100000-n5.txt Download as CSV file: xf-fx84w218-il-100000-n5.csv |
XFOIL Version 6.96
Calculated polar for: FX 84-W-218
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
------ -------- --------- --------- -------- -------- --------
-15.750 -0.6350 0.07318 0.06643 -0.1013 0.9806 0.0777
-15.500 -0.6604 0.06562 0.05852 -0.1075 0.9704 0.0788
-15.250 -0.6405 0.06371 0.05663 -0.1102 0.9629 0.0801
-15.000 -0.6352 0.06031 0.05311 -0.1136 0.9544 0.0816
-14.750 -0.6361 0.05642 0.04901 -0.1171 0.9463 0.0833
-14.500 -0.6400 0.05271 0.04502 -0.1197 0.9374 0.0849
-14.250 -0.6390 0.04991 0.04201 -0.1214 0.9287 0.0866
-14.000 -0.6255 0.04850 0.04060 -0.1221 0.9206 0.0881
-13.750 -0.6187 0.04678 0.03879 -0.1224 0.9123 0.0898
-13.500 -0.6158 0.04493 0.03679 -0.1224 0.9036 0.0917
-13.250 -0.6154 0.04301 0.03462 -0.1221 0.8957 0.0938
-13.000 -0.6059 0.04185 0.03344 -0.1215 0.8879 0.0956
-12.750 -0.5966 0.04072 0.03228 -0.1209 0.8816 0.0976
-12.500 -0.5899 0.03953 0.03100 -0.1201 0.8738 0.0999
-12.250 -0.5841 0.03824 0.02953 -0.1191 0.8667 0.1024
-12.000 -0.5740 0.03725 0.02848 -0.1181 0.8612 0.1047
-11.750 -0.5637 0.03637 0.02761 -0.1173 0.8541 0.1072
-11.500 -0.5540 0.03541 0.02656 -0.1162 0.8477 0.1102
-11.250 -0.5438 0.03444 0.02544 -0.1150 0.8425 0.1132
-11.000 -0.5324 0.03371 0.02474 -0.1140 0.8361 0.1160
-10.750 -0.5217 0.03295 0.02394 -0.1127 0.8297 0.1194
-10.500 -0.5102 0.03216 0.02298 -0.1113 0.8246 0.1233
-10.250 -0.4980 0.03146 0.02231 -0.1099 0.8201 0.1264
-10.000 -0.4867 0.03087 0.02170 -0.1086 0.8133 0.1304
-9.750 -0.4742 0.03023 0.02096 -0.1072 0.8075 0.1350
-9.500 -0.4622 0.02959 0.02034 -0.1056 0.8029 0.1390
-9.250 -0.4493 0.02900 0.01968 -0.1040 0.7987 0.1440
-9.000 -0.4374 0.02855 0.01923 -0.1024 0.7921 0.1489
-8.750 -0.4264 0.02807 0.01875 -0.1005 0.7865 0.1540
-8.500 -0.4126 0.02759 0.01815 -0.0987 0.7821 0.1603
-8.250 -0.4010 0.02709 0.01768 -0.0966 0.7786 0.1658
-8.000 -0.3917 0.02694 0.01751 -0.0943 0.7719 0.1723
-7.750 -0.3805 0.02661 0.01721 -0.0921 0.7664 0.1786
-7.500 -0.3660 0.02622 0.01678 -0.0903 0.7620 0.1866
-7.250 -0.3497 0.02576 0.01631 -0.0886 0.7587 0.1947
-7.000 -0.3367 0.02559 0.01613 -0.0867 0.7531 0.2036
-6.750 -0.3242 0.02538 0.01597 -0.0847 0.7473 0.2122
-6.500 -0.3072 0.02508 0.01562 -0.0831 0.7429 0.2232
-6.250 -0.2898 0.02465 0.01524 -0.0816 0.7393 0.2341
-6.000 -0.2693 0.02423 0.01479 -0.0804 0.7366 0.2467
-5.750 -0.2597 0.02432 0.01493 -0.0780 0.7292 0.2585
-5.500 -0.2443 0.02408 0.01476 -0.0762 0.7243 0.2718
-5.250 -0.2251 0.02375 0.01446 -0.0749 0.7205 0.2874
-5.000 -0.2033 0.02336 0.01408 -0.0739 0.7175 0.3048
-4.750 -0.1875 0.02325 0.01402 -0.0722 0.7127 0.3223
-4.500 -0.1755 0.02328 0.01413 -0.0699 0.7063 0.3400
-4.250 -0.1566 0.02306 0.01397 -0.0685 0.7021 0.3609
-4.000 -0.1342 0.02273 0.01372 -0.0675 0.6988 0.3841
-3.750 -0.1093 0.02238 0.01343 -0.0668 0.6963 0.4093
-3.500 -0.0997 0.02261 0.01377 -0.0642 0.6896 0.4303
-3.250 -0.0838 0.02264 0.01390 -0.0623 0.6842 0.4539
-3.000 -0.0608 0.02249 0.01380 -0.0613 0.6805 0.4795
-2.750 -0.0342 0.02227 0.01361 -0.0608 0.6777 0.5053
-2.500 -0.0050 0.02205 0.01339 -0.0607 0.6754 0.5306
-2.250 -0.0025 0.02265 0.01412 -0.0569 0.6670 0.5479
-2.000 0.0181 0.02273 0.01424 -0.0556 0.6625 0.5687
-1.750 0.0451 0.02266 0.01417 -0.0551 0.6593 0.5890
-1.500 0.0754 0.02253 0.01403 -0.0550 0.6568 0.6082
-1.250 0.0938 0.02276 0.01428 -0.0534 0.6521 0.6248
-1.000 0.0995 0.02327 0.01482 -0.0501 0.6447 0.6405
-0.750 0.1248 0.02333 0.01488 -0.0493 0.6410 0.6554
-0.500 0.1549 0.02325 0.01478 -0.0491 0.6382 0.6700
-0.250 0.1877 0.02309 0.01454 -0.0495 0.6361 0.6856
0.000 0.1807 0.02401 0.01558 -0.0444 0.6271 0.6964
0.250 0.2002 0.02417 0.01571 -0.0429 0.6224 0.7097
0.500 0.2293 0.02412 0.01564 -0.0426 0.6195 0.7223
0.750 0.2626 0.02398 0.01545 -0.0429 0.6172 0.7343
1.250 0.2644 0.02519 0.01674 -0.0348 0.6033 0.7573
1.500 0.2935 0.02509 0.01660 -0.0345 0.6003 0.7690
1.750 0.3284 0.02490 0.01637 -0.0351 0.5981 0.7788
2.000 0.3666 0.02468 0.01609 -0.0362 0.5963 0.7885
2.250 0.3196 0.02646 0.01802 -0.0260 0.5834 0.8013
2.500 0.3493 0.02627 0.01780 -0.0257 0.5807 0.8113
2.750 0.3844 0.02592 0.01739 -0.0263 0.5786 0.8207
3.000 0.4236 0.02556 0.01698 -0.0274 0.5770 0.8285
3.500 0.4094 0.02764 0.01918 -0.0184 0.5609 0.8526
3.750 0.4453 0.02718 0.01866 -0.0191 0.5591 0.8617
4.000 0.4856 0.02666 0.01810 -0.0202 0.5576 0.8692
4.500 0.4739 0.02901 0.02057 -0.0125 0.5412 0.8967
4.750 0.5140 0.02843 0.01996 -0.0137 0.5396 0.9046
5.250 0.5217 0.03097 0.02262 -0.0100 0.5235 0.9330
5.500 0.5678 0.03039 0.02201 -0.0124 0.5218 0.9404
5.750 0.6147 0.02968 0.02127 -0.0147 0.5203 0.9488
6.250 0.6538 0.03243 0.02415 -0.0175 0.5044 0.9729
6.500 0.7043 0.03168 0.02337 -0.0205 0.5026 0.9804
6.750 0.7584 0.03076 0.02241 -0.0239 0.5009 0.9871
7.250 0.7394 0.03377 0.02543 -0.0179 0.4842 1.0000
7.500 0.7798 0.03281 0.02442 -0.0189 0.4825 1.0000
8.000 0.7726 0.03619 0.02781 -0.0146 0.4658 1.0000
8.250 0.8146 0.03511 0.02668 -0.0155 0.4640 1.0000
8.750 0.8127 0.03870 0.03030 -0.0122 0.4474 1.0000
9.000 0.8547 0.03754 0.02910 -0.0130 0.4456 1.0000
9.500 0.8536 0.04136 0.03298 -0.0101 0.4290 1.0000
9.750 0.8963 0.04004 0.03162 -0.0108 0.4270 1.0000
10.250 0.8952 0.04406 0.03572 -0.0082 0.4105 1.0000
10.500 0.9385 0.04260 0.03423 -0.0088 0.4084 1.0000
11.000 0.9386 0.04670 0.03841 -0.0066 0.3919 1.0000
11.500 0.9429 0.05078 0.04257 -0.0050 0.3757 1.0000
11.750 0.9839 0.04924 0.04099 -0.0052 0.3731 1.0000
12.250 0.9873 0.05352 0.04536 -0.0038 0.3568 1.0000
12.750 0.9936 0.05779 0.04971 -0.0028 0.3409 1.0000
13.000 1.0331 0.05617 0.04805 -0.0028 0.3377 1.0000
13.250 1.0040 0.06179 0.05379 -0.0022 0.3255 1.0000
13.500 1.0378 0.06067 0.05264 -0.0020 0.3214 1.0000
13.750 1.0213 0.06516 0.05722 -0.0018 0.3111 1.0000
14.000 1.0451 0.06511 0.05716 -0.0016 0.3055 1.0000
14.250 1.0564 0.06651 0.05858 -0.0015 0.2987 1.0000
14.500 1.0539 0.06955 0.06167 -0.0014 0.2899 1.0000
14.750 1.0915 0.06781 0.05986 -0.0011 0.2856 1.0000
15.000 1.0647 0.07388 0.06608 -0.0015 0.2749 1.0000
15.250 1.0952 0.07293 0.06506 -0.0012 0.2699 1.0000
15.500 1.0779 0.07804 0.07029 -0.0017 0.2605 1.0000
15.750 1.0983 0.07833 0.07056 -0.0016 0.2546 1.0000
16.000 1.0938 0.08191 0.07420 -0.0020 0.2467 1.0000
16.250 1.1016 0.08388 0.07619 -0.0022 0.2398 1.0000
16.500 1.1132 0.08535 0.07766 -0.0024 0.2336 1.0000
16.750 1.1061 0.08942 0.08182 -0.0032 0.2256 1.0000
17.000 1.1354 0.08842 0.08071 -0.0028 0.2207 1.0000
17.250 1.1113 0.09497 0.08745 -0.0043 0.2120 1.0000
17.500 1.1331 0.09498 0.08738 -0.0042 0.2067 1.0000
17.750 1.1176 0.10045 0.09299 -0.0056 0.1990 1.0000
18.000 1.1296 0.10189 0.09441 -0.0060 0.1931 1.0000
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