FX 84-W-218 (fx84w218-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: FX 84-W-218 (fx84w218-il) Reynolds number: 1,000,000 Max Cl/Cd: 101.2 at α=6° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx84w218-il-1000000.txt Download as CSV file: xf-fx84w218-il-1000000.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 = 1.000 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -0.9844 0.07555 0.07167 -0.0864 1.0000 0.0381
-19.500 -0.9894 0.07178 0.06782 -0.0883 1.0000 0.0384
-19.250 -0.9923 0.06830 0.06427 -0.0899 1.0000 0.0387
-19.000 -0.9985 0.06452 0.06041 -0.0917 1.0000 0.0391
-18.750 -1.0056 0.05986 0.05568 -0.0948 0.9734 0.0397
-18.500 -0.9926 0.05548 0.05122 -0.1011 0.9608 0.0404
-18.250 -0.9755 0.05180 0.04744 -0.1068 0.9451 0.0411
-18.000 -0.9686 0.04897 0.04445 -0.1092 0.9226 0.0417
-17.750 -0.9677 0.04656 0.04191 -0.1097 0.9065 0.0422
-17.500 -0.9663 0.04431 0.03955 -0.1100 0.8945 0.0427
-17.250 -0.9626 0.04235 0.03747 -0.1102 0.8840 0.0431
-17.000 -0.9596 0.04031 0.03534 -0.1103 0.8753 0.0436
-16.750 -0.9645 0.03771 0.03265 -0.1103 0.8665 0.0443
-16.500 -0.9628 0.03572 0.03058 -0.1102 0.8592 0.0448
-16.250 -0.9589 0.03392 0.02874 -0.1101 0.8522 0.0455
-16.000 -0.9537 0.03237 0.02710 -0.1097 0.8451 0.0462
-15.750 -0.9458 0.03101 0.02568 -0.1093 0.8389 0.0469
-15.500 -0.9365 0.02976 0.02437 -0.1089 0.8330 0.0476
-15.250 -0.9250 0.02874 0.02327 -0.1084 0.8271 0.0482
-15.000 -0.9229 0.02720 0.02164 -0.1075 0.8205 0.0490
-14.750 -0.9167 0.02587 0.02031 -0.1067 0.8158 0.0501
-14.500 -0.9071 0.02482 0.01922 -0.1059 0.8103 0.0508
-14.250 -0.8964 0.02391 0.01824 -0.1050 0.8046 0.0518
-14.000 -0.8846 0.02308 0.01734 -0.1041 0.7990 0.0527
-13.750 -0.8701 0.02235 0.01657 -0.1034 0.7950 0.0535
-13.500 -0.8632 0.02128 0.01547 -0.1020 0.7899 0.0546
-13.250 -0.8526 0.02046 0.01461 -0.1008 0.7847 0.0558
-13.000 -0.8396 0.01981 0.01390 -0.0997 0.7788 0.0570
-12.750 -0.8245 0.01920 0.01327 -0.0988 0.7752 0.0582
-12.500 -0.8099 0.01860 0.01263 -0.0977 0.7710 0.0594
-12.250 -0.7987 0.01788 0.01189 -0.0962 0.7663 0.0609
-12.000 -0.7846 0.01733 0.01130 -0.0949 0.7613 0.0625
-11.750 -0.7690 0.01686 0.01079 -0.0938 0.7564 0.0639
-11.500 -0.7518 0.01642 0.01032 -0.0927 0.7528 0.0652
-11.250 -0.7389 0.01584 0.00974 -0.0911 0.7486 0.0672
-11.000 -0.7232 0.01540 0.00928 -0.0898 0.7443 0.0692
-10.750 -0.7058 0.01506 0.00888 -0.0886 0.7396 0.0710
-10.500 -0.6905 0.01464 0.00844 -0.0871 0.7352 0.0731
-10.250 -0.6746 0.01422 0.00804 -0.0856 0.7315 0.0755
-10.000 -0.6568 0.01390 0.00769 -0.0843 0.7275 0.0777
-9.750 -0.6406 0.01355 0.00732 -0.0826 0.7234 0.0802
-9.500 -0.6251 0.01323 0.00699 -0.0809 0.7188 0.0830
-9.250 -0.6077 0.01303 0.00675 -0.0792 0.7146 0.0856
-9.000 -0.5920 0.01277 0.00650 -0.0773 0.7112 0.0886
-8.750 -0.5723 0.01252 0.00627 -0.0761 0.7073 0.0920
-8.500 -0.5505 0.01231 0.00603 -0.0752 0.7033 0.0954
-8.250 -0.5295 0.01207 0.00579 -0.0742 0.6990 0.0997
-8.000 -0.5061 0.01191 0.00559 -0.0735 0.6945 0.1034
-7.750 -0.4836 0.01164 0.00537 -0.0728 0.6915 0.1085
-7.500 -0.4591 0.01145 0.00518 -0.0723 0.6879 0.1131
-7.250 -0.4358 0.01121 0.00497 -0.0717 0.6839 0.1193
-7.000 -0.4112 0.01104 0.00478 -0.0712 0.6797 0.1249
-6.750 -0.3871 0.01086 0.00461 -0.0707 0.6749 0.1318
-6.500 -0.3618 0.01065 0.00444 -0.0704 0.6721 0.1390
-6.250 -0.3360 0.01047 0.00428 -0.0701 0.6688 0.1464
-6.000 -0.3108 0.01027 0.00412 -0.0698 0.6649 0.1553
-5.750 -0.2850 0.01011 0.00397 -0.0695 0.6609 0.1642
-5.500 -0.2592 0.00998 0.00383 -0.0692 0.6561 0.1739
-5.250 -0.2331 0.00979 0.00370 -0.0690 0.6529 0.1850
-5.000 -0.2065 0.00961 0.00357 -0.0689 0.6496 0.1963
-4.750 -0.1797 0.00946 0.00346 -0.0688 0.6457 0.2081
-4.500 -0.1533 0.00930 0.00334 -0.0686 0.6416 0.2217
-4.250 -0.1270 0.00917 0.00323 -0.0684 0.6370 0.2361
-4.000 -0.1001 0.00902 0.00313 -0.0684 0.6335 0.2509
-3.750 -0.0729 0.00885 0.00303 -0.0684 0.6301 0.2673
-3.500 -0.0458 0.00869 0.00294 -0.0683 0.6261 0.2854
-3.250 -0.0189 0.00855 0.00285 -0.0683 0.6220 0.3055
-3.000 0.0077 0.00843 0.00277 -0.0681 0.6175 0.3267
-2.750 0.0349 0.00828 0.00270 -0.0681 0.6137 0.3499
-2.500 0.0625 0.00812 0.00263 -0.0682 0.6102 0.3741
-2.250 0.0900 0.00799 0.00258 -0.0682 0.6063 0.3993
-1.750 0.1444 0.00780 0.00249 -0.0682 0.5974 0.4481
-1.500 0.1723 0.00769 0.00246 -0.0682 0.5937 0.4723
-1.250 0.2005 0.00759 0.00244 -0.0684 0.5902 0.4953
-1.000 0.2287 0.00753 0.00243 -0.0685 0.5862 0.5161
-0.750 0.2565 0.00749 0.00243 -0.0686 0.5818 0.5359
-0.500 0.2841 0.00751 0.00244 -0.0686 0.5766 0.5540
-0.250 0.3129 0.00746 0.00245 -0.0688 0.5736 0.5714
0.000 0.3414 0.00742 0.00247 -0.0689 0.5698 0.5872
0.250 0.3697 0.00742 0.00249 -0.0691 0.5654 0.6013
0.500 0.3974 0.00746 0.00252 -0.0691 0.5606 0.6150
0.750 0.4252 0.00749 0.00257 -0.0691 0.5562 0.6274
1.000 0.4542 0.00750 0.00260 -0.0693 0.5527 0.6386
1.250 0.4823 0.00751 0.00265 -0.0694 0.5483 0.6500
1.500 0.5099 0.00757 0.00269 -0.0694 0.5435 0.6598
1.750 0.5365 0.00765 0.00277 -0.0693 0.5382 0.6693
2.000 0.5651 0.00767 0.00282 -0.0694 0.5348 0.6793
2.250 0.5930 0.00771 0.00288 -0.0695 0.5303 0.6881
2.500 0.6198 0.00777 0.00295 -0.0693 0.5254 0.6969
2.750 0.6456 0.00790 0.00303 -0.0690 0.5200 0.7050
3.000 0.6730 0.00792 0.00311 -0.0690 0.5161 0.7140
3.250 0.7000 0.00798 0.00319 -0.0689 0.5115 0.7225
3.500 0.7258 0.00809 0.00327 -0.0686 0.5063 0.7287
3.750 0.7492 0.00822 0.00339 -0.0679 0.5005 0.7367
4.000 0.7760 0.00826 0.00348 -0.0677 0.4965 0.7441
4.250 0.8013 0.00836 0.00357 -0.0673 0.4911 0.7503
4.500 0.8234 0.00848 0.00369 -0.0664 0.4853 0.7573
4.750 0.8458 0.00860 0.00383 -0.0655 0.4802 0.7642
5.000 0.8689 0.00869 0.00393 -0.0647 0.4753 0.7705
5.250 0.8873 0.00880 0.00404 -0.0630 0.4698 0.7768
5.500 0.9018 0.00900 0.00424 -0.0606 0.4640 0.7838
5.750 0.9232 0.00913 0.00440 -0.0596 0.4595 0.7904
6.000 0.9432 0.00932 0.00458 -0.0583 0.4542 0.7959
6.250 0.9589 0.00955 0.00483 -0.0564 0.4483 0.8033
6.500 0.9763 0.00980 0.00509 -0.0547 0.4428 0.8102
6.750 0.9966 0.01000 0.00530 -0.0536 0.4375 0.8164
7.000 1.0132 0.01027 0.00558 -0.0520 0.4316 0.8234
7.250 1.0275 0.01061 0.00593 -0.0499 0.4255 0.8306
7.500 1.0480 0.01084 0.00618 -0.0490 0.4204 0.8373
7.750 1.0637 0.01116 0.00652 -0.0473 0.4141 0.8444
8.000 1.0762 0.01160 0.00696 -0.0451 0.4076 0.8525
8.250 1.0957 0.01188 0.00726 -0.0441 0.4022 0.8595
8.500 1.1103 0.01225 0.00767 -0.0423 0.3960 0.8681
8.750 1.1216 0.01279 0.00820 -0.0402 0.3892 0.8775
9.000 1.1387 0.01312 0.00857 -0.0388 0.3831 0.8864
9.250 1.1494 0.01369 0.00914 -0.0367 0.3758 0.8974
9.500 1.1613 0.01417 0.00967 -0.0346 0.3687 0.9100
9.750 1.1725 0.01469 0.01023 -0.0325 0.3612 0.9264
10.000 1.1858 0.01535 0.01093 -0.0312 0.3532 0.9530
10.250 1.2229 0.01591 0.01152 -0.0345 0.3439 0.9828
10.500 1.2330 0.01680 0.01237 -0.0329 0.3362 1.0000
10.750 1.2489 0.01742 0.01298 -0.0320 0.3282 1.0000
11.000 1.2563 0.01845 0.01396 -0.0302 0.3198 1.0000
11.250 1.2712 0.01914 0.01466 -0.0292 0.3122 1.0000
11.500 1.2775 0.02031 0.01578 -0.0274 0.3030 1.0000
11.750 1.2906 0.02114 0.01660 -0.0264 0.2950 1.0000
12.000 1.2958 0.02244 0.01786 -0.0246 0.2859 1.0000
12.250 1.3075 0.02340 0.01881 -0.0235 0.2774 1.0000
12.500 1.3117 0.02484 0.02021 -0.0219 0.2682 1.0000
12.750 1.3229 0.02588 0.02125 -0.0209 0.2605 1.0000
13.000 1.3267 0.02744 0.02277 -0.0194 0.2516 1.0000
13.250 1.3362 0.02865 0.02398 -0.0184 0.2435 1.0000
13.500 1.3403 0.03027 0.02556 -0.0170 0.2355 1.0000
13.750 1.3481 0.03167 0.02695 -0.0160 0.2272 1.0000
14.000 1.3520 0.03337 0.02863 -0.0149 0.2194 1.0000
14.250 1.3596 0.03484 0.03010 -0.0140 0.2124 1.0000
14.500 1.3626 0.03669 0.03193 -0.0129 0.2048 1.0000
14.750 1.3703 0.03824 0.03348 -0.0122 0.1985 1.0000
15.000 1.3722 0.04025 0.03547 -0.0113 0.1909 1.0000
15.250 1.3792 0.04191 0.03714 -0.0106 0.1848 1.0000
15.500 1.3811 0.04400 0.03920 -0.0099 0.1776 1.0000
15.750 1.3867 0.04586 0.04108 -0.0093 0.1715 1.0000
16.000 1.3890 0.04801 0.04321 -0.0087 0.1649 1.0000
16.250 1.3927 0.05009 0.04529 -0.0082 0.1587 1.0000
16.500 1.3944 0.05237 0.04756 -0.0078 0.1523 1.0000
16.750 1.3978 0.05456 0.04977 -0.0075 0.1468 1.0000
17.000 1.3990 0.05698 0.05217 -0.0072 0.1405 1.0000
17.250 1.4009 0.05939 0.05460 -0.0070 0.1348 1.0000
17.500 1.4012 0.06199 0.05718 -0.0068 0.1290 1.0000
17.750 1.4032 0.06446 0.05967 -0.0068 0.1240 1.0000
18.000 1.4034 0.06718 0.06239 -0.0068 0.1188 1.0000
18.250 1.4044 0.06984 0.06507 -0.0069 0.1136 1.0000
18.500 1.4037 0.07273 0.06796 -0.0071 0.1089 1.0000
18.750 1.4048 0.07546 0.07070 -0.0073 0.1045 1.0000
19.000 1.4040 0.07847 0.07374 -0.0077 0.1003 1.0000
19.250 1.4037 0.08145 0.07672 -0.0081 0.0958 1.0000
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