FX 84-W-218 (fx84w218-il) Xfoil prediction polar at RE=100,000 Ncrit=9
| Details | Polar file |
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Airfoil: FX 84-W-218 (fx84w218-il) Reynolds number: 100,000 Max Cl/Cd: 7.06 at α=11.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx84w218-il-100000.txt Download as CSV file: xf-fx84w218-il-100000.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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-13.750 -0.1893 0.14289 0.13759 -0.0677 0.9773 0.1816
-13.500 -0.2315 0.14054 0.13526 -0.0741 0.9719 0.1898
-13.250 -0.6058 0.07021 0.06433 -0.1056 0.9694 0.1241
-13.000 -0.3913 0.09120 0.08571 -0.0982 0.9675 0.1346
-12.750 -0.5434 0.06720 0.06134 -0.1110 0.9615 0.1304
-12.500 -0.6269 0.05795 0.05160 -0.1139 0.9520 0.1289
-12.250 -0.6585 0.05464 0.04802 -0.1127 0.9425 0.1296
-12.000 -0.6766 0.05167 0.04472 -0.1122 0.9356 0.1313
-11.750 -0.7080 0.05065 0.04350 -0.1062 0.9244 0.1318
-11.500 -0.7216 0.04843 0.04086 -0.1038 0.9178 0.1337
-11.250 -0.7553 0.04813 0.04039 -0.0955 0.9059 0.1341
-11.000 -0.7206 0.04645 0.03874 -0.0981 0.9025 0.1379
-10.750 -0.6875 0.04505 0.03725 -0.1005 0.8997 0.1426
-10.500 -0.7238 0.04531 0.03743 -0.0909 0.8874 0.1429
-10.250 -0.7165 0.04379 0.03545 -0.0895 0.8826 0.1467
-10.000 -0.7468 0.04386 0.03543 -0.0809 0.8725 0.1472
-9.750 -0.7142 0.04295 0.03472 -0.0823 0.8680 0.1518
-9.500 -0.6876 0.04192 0.03350 -0.0831 0.8641 0.1575
-9.250 -0.7071 0.04181 0.03320 -0.0761 0.8554 0.1593
-9.000 -0.6958 0.04112 0.03255 -0.0741 0.8493 0.1631
-8.750 -0.6675 0.04049 0.03191 -0.0748 0.8454 0.1694
-8.500 -0.6307 0.03937 0.03064 -0.0769 0.8426 0.1772
-8.250 -0.6643 0.03977 0.03103 -0.0676 0.8321 0.1777
-8.000 -0.6437 0.03934 0.03063 -0.0669 0.8270 0.1842
-7.750 -0.6132 0.03855 0.02972 -0.0678 0.8236 0.1927
-7.500 -0.5705 0.03792 0.02906 -0.0705 0.8213 0.2037
-7.250 -0.6132 0.03850 0.02964 -0.0600 0.8100 0.2032
-7.000 -0.5884 0.03795 0.02915 -0.0599 0.8054 0.2120
-6.750 -0.5561 0.03745 0.02850 -0.0608 0.8021 0.2240
-6.500 -0.5117 0.03687 0.02803 -0.0636 0.8000 0.2387
-6.250 -0.5559 0.03761 0.02877 -0.0533 0.7889 0.2380
-6.000 -0.5305 0.03718 0.02844 -0.0531 0.7842 0.2502
-5.750 -0.4960 0.03668 0.02797 -0.0543 0.7810 0.2664
-5.500 -0.4541 0.03621 0.02759 -0.0565 0.7788 0.2863
-5.250 -0.4955 0.03712 0.02850 -0.0471 0.7683 0.2866
-5.000 -0.4722 0.03687 0.02831 -0.0466 0.7634 0.3043
-4.750 -0.4371 0.03644 0.02800 -0.0476 0.7599 0.3273
-4.500 -0.3959 0.03604 0.02771 -0.0495 0.7577 0.3557
-4.250 -0.4336 0.03712 0.02878 -0.0411 0.7476 0.3590
-4.000 -0.4113 0.03698 0.02880 -0.0404 0.7426 0.3838
-3.750 -0.3767 0.03668 0.02870 -0.0411 0.7391 0.4163
-3.500 -0.3347 0.03640 0.02863 -0.0426 0.7368 0.4546
-3.250 -0.3701 0.03763 0.02988 -0.0351 0.7268 0.4630
-3.000 -0.3475 0.03772 0.03017 -0.0342 0.7218 0.4956
-2.750 -0.3118 0.03771 0.03030 -0.0346 0.7183 0.5347
-2.500 -0.2981 0.03835 0.03106 -0.0325 0.7132 0.5625
-2.250 -0.3061 0.03929 0.03210 -0.0283 0.7057 0.5825
-2.000 -0.2820 0.03970 0.03257 -0.0273 0.7008 0.6125
-1.750 -0.2448 0.03996 0.03286 -0.0274 0.6975 0.6422
-1.500 -0.2453 0.04103 0.03395 -0.0240 0.6909 0.6620
-1.250 -0.2434 0.04203 0.03504 -0.0207 0.6844 0.6792
-1.000 -0.2171 0.04252 0.03555 -0.0195 0.6798 0.7006
-0.750 -0.1795 0.04285 0.03587 -0.0192 0.6767 0.7216
-0.500 -0.1940 0.04424 0.03731 -0.0145 0.6688 0.7357
-0.250 -0.1861 0.04509 0.03815 -0.0120 0.6632 0.7535
0.000 -0.1590 0.04549 0.03852 -0.0107 0.6589 0.7719
0.250 -0.1219 0.04573 0.03874 -0.0099 0.6561 0.7880
0.500 -0.1486 0.04732 0.04040 -0.0044 0.6469 0.8019
0.750 -0.1371 0.04800 0.04105 -0.0021 0.6420 0.8193
1.000 -0.1099 0.04826 0.04129 -0.0005 0.6383 0.8355
1.250 -0.0700 0.04825 0.04122 0.0001 0.6357 0.8511
1.500 -0.1078 0.05007 0.04313 0.0061 0.6254 0.8666
1.750 -0.0907 0.05059 0.04362 0.0080 0.6210 0.8837
2.000 -0.0538 0.05067 0.04364 0.0081 0.6176 0.9008
2.250 -0.0541 0.05208 0.04507 0.0101 0.6097 0.9174
2.500 -0.0316 0.05327 0.04626 0.0093 0.6036 0.9329
2.750 0.0333 0.05414 0.04706 0.0035 0.5993 0.9421
3.000 0.1074 0.05431 0.04715 -0.0027 0.5966 0.9509
3.250 0.1103 0.05752 0.05041 -0.0054 0.5849 0.9607
3.500 0.1739 0.05825 0.05109 -0.0117 0.5805 0.9669
3.750 0.2493 0.05818 0.05095 -0.0185 0.5778 0.9726
4.000 0.2492 0.06161 0.05443 -0.0210 0.5659 0.9822
4.250 0.3062 0.06207 0.05486 -0.0264 0.5614 0.9893
4.500 0.3747 0.06174 0.05448 -0.0322 0.5588 0.9954
4.750 0.3409 0.06507 0.05785 -0.0298 0.5472 1.0000
5.000 0.3433 0.06477 0.05749 -0.0267 0.5428 1.0000
5.250 0.3606 0.06389 0.05654 -0.0246 0.5401 1.0000
5.500 0.3867 0.06281 0.05539 -0.0230 0.5383 1.0000
5.750 0.3017 0.06626 0.05883 -0.0142 0.5248 1.0000
6.000 0.3340 0.06584 0.05834 -0.0141 0.5215 1.0000
6.250 0.3785 0.06506 0.05748 -0.0148 0.5195 1.0000
6.500 0.3340 0.06947 0.06191 -0.0121 0.5060 1.0000
6.750 0.3738 0.06907 0.06145 -0.0127 0.5026 1.0000
7.000 0.4212 0.06823 0.06056 -0.0135 0.5006 1.0000
7.250 0.3806 0.07306 0.06541 -0.0116 0.4867 1.0000
7.500 0.4227 0.07246 0.06477 -0.0122 0.4836 1.0000
7.750 0.4704 0.07149 0.06374 -0.0128 0.4817 1.0000
8.000 0.4295 0.07677 0.06907 -0.0114 0.4673 1.0000
8.250 0.4727 0.07596 0.06823 -0.0118 0.4645 1.0000
8.500 0.4440 0.08080 0.07310 -0.0110 0.4522 1.0000
8.750 0.4794 0.08049 0.07277 -0.0112 0.4479 1.0000
9.000 0.5238 0.07944 0.07170 -0.0114 0.4456 1.0000
9.250 0.4898 0.08503 0.07733 -0.0109 0.4321 1.0000
9.500 0.5289 0.08429 0.07657 -0.0109 0.4287 1.0000
9.750 0.5746 0.08294 0.07521 -0.0110 0.4267 1.0000
10.000 0.5360 0.08927 0.08159 -0.0108 0.4124 1.0000
10.250 0.5781 0.08809 0.08040 -0.0107 0.4096 1.0000
10.500 0.5493 0.09388 0.08624 -0.0109 0.3969 1.0000
10.750 0.5833 0.09343 0.08579 -0.0108 0.3930 1.0000
11.000 0.6280 0.09176 0.08412 -0.0105 0.3908 1.0000
11.250 0.5903 0.09882 0.09124 -0.0111 0.3770 1.0000
11.500 0.6299 0.09758 0.09000 -0.0108 0.3740 1.0000
11.750 0.6754 0.09560 0.08803 -0.0103 0.3723 1.0000
12.000 0.6324 0.10367 0.09616 -0.0114 0.3577 1.0000
12.250 0.6752 0.10185 0.09435 -0.0109 0.3554 1.0000
12.500 0.6356 0.10997 0.10254 -0.0124 0.3422 1.0000
12.750 0.6748 0.10840 0.10097 -0.0118 0.3389 1.0000
13.000 0.7201 0.10599 0.09858 -0.0109 0.3371 1.0000
13.250 0.6758 0.11507 0.10772 -0.0130 0.3229 1.0000
13.500 0.7185 0.11282 0.10549 -0.0121 0.3205 1.0000
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