FX 66-S-196 AIRFOIL (fx66s196-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: FX 66-S-196 AIRFOIL (fx66s196-il) Reynolds number: 1,000,000 Max Cl/Cd: 130.83 at α=7.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx66s196-il-1000000-n5.txt Download as CSV file: xf-fx66s196-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: FX 66-S-196 AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 1.000 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -0.6221 0.12126 0.11872 -0.0738 0.9113 0.0065
-19.500 -0.6462 0.10977 0.10696 -0.0827 0.8869 0.0066
-19.250 -0.6773 0.09964 0.09656 -0.0889 0.8642 0.0066
-19.000 -0.6980 0.09212 0.08881 -0.0932 0.8416 0.0066
-18.750 -0.7205 0.08473 0.08121 -0.0973 0.8228 0.0066
-18.500 -0.7333 0.07908 0.07538 -0.1005 0.8066 0.0067
-18.250 -0.7504 0.07302 0.06914 -0.1038 0.7936 0.0067
-18.000 -0.7637 0.06773 0.06367 -0.1066 0.7792 0.0067
-17.750 -0.7679 0.06390 0.05970 -0.1085 0.7652 0.0067
-17.500 -0.7768 0.05963 0.05527 -0.1105 0.7549 0.0067
-17.250 -0.7728 0.05707 0.05262 -0.1118 0.7442 0.0069
-17.000 -0.7705 0.05438 0.04982 -0.1130 0.7349 0.0070
-16.750 -0.7760 0.05095 0.04625 -0.1142 0.7259 0.0071
-16.500 -0.7795 0.04794 0.04311 -0.1151 0.7182 0.0071
-16.250 -0.7760 0.04574 0.04081 -0.1157 0.7108 0.0072
-16.000 -0.7730 0.04357 0.03854 -0.1162 0.7044 0.0073
-15.750 -0.7710 0.04141 0.03628 -0.1165 0.6985 0.0074
-15.500 -0.7623 0.03991 0.03470 -0.1167 0.6925 0.0075
-15.250 -0.7556 0.03827 0.03298 -0.1168 0.6877 0.0076
-15.000 -0.7550 0.03621 0.03083 -0.1167 0.6824 0.0076
-14.750 -0.7473 0.03483 0.02936 -0.1165 0.6768 0.0077
-14.500 -0.7363 0.03368 0.02814 -0.1164 0.6718 0.0078
-14.250 -0.7315 0.03213 0.02650 -0.1160 0.6663 0.0078
-14.000 -0.7245 0.03078 0.02509 -0.1156 0.6610 0.0081
-13.750 -0.7204 0.02924 0.02345 -0.1149 0.6567 0.0081
-13.500 -0.7117 0.02805 0.02222 -0.1144 0.6520 0.0084
-13.250 -0.7058 0.02672 0.02080 -0.1136 0.6475 0.0084
-13.000 -0.6933 0.02584 0.01989 -0.1131 0.6435 0.0087
-12.750 -0.6824 0.02486 0.01885 -0.1125 0.6398 0.0089
-12.500 -0.6729 0.02381 0.01774 -0.1117 0.6361 0.0089
-12.250 -0.6604 0.02298 0.01686 -0.1110 0.6322 0.0091
-12.000 -0.6497 0.02205 0.01587 -0.1101 0.6287 0.0093
-11.750 -0.6368 0.02124 0.01502 -0.1093 0.6254 0.0095
-11.500 -0.6241 0.02046 0.01419 -0.1085 0.6216 0.0097
-11.250 -0.6133 0.01960 0.01326 -0.1074 0.6175 0.0098
-11.000 -0.6011 0.01886 0.01246 -0.1063 0.6140 0.0100
-10.750 -0.5876 0.01821 0.01177 -0.1053 0.6111 0.0102
-10.500 -0.5759 0.01752 0.01103 -0.1040 0.6079 0.0104
-10.250 -0.5697 0.01679 0.01024 -0.1018 0.6045 0.0104
-10.000 -0.5601 0.01636 0.00976 -0.0996 0.6013 0.0106
-9.750 -0.5467 0.01580 0.00914 -0.0981 0.5983 0.0110
-9.500 -0.5292 0.01533 0.00863 -0.0971 0.5958 0.0113
-9.250 -0.5098 0.01492 0.00819 -0.0963 0.5931 0.0116
-9.000 -0.4894 0.01454 0.00777 -0.0956 0.5904 0.0120
-8.750 -0.4677 0.01421 0.00740 -0.0950 0.5877 0.0124
-8.500 -0.4455 0.01389 0.00703 -0.0946 0.5851 0.0127
-8.250 -0.4224 0.01360 0.00669 -0.0942 0.5828 0.0132
-8.000 -0.3984 0.01331 0.00637 -0.0939 0.5809 0.0136
-7.750 -0.3748 0.01298 0.00602 -0.0937 0.5789 0.0143
-7.500 -0.3504 0.01269 0.00572 -0.0935 0.5769 0.0152
-7.250 -0.3255 0.01243 0.00543 -0.0933 0.5748 0.0162
-7.000 -0.3002 0.01220 0.00517 -0.0932 0.5725 0.0174
-6.750 -0.2750 0.01196 0.00492 -0.0932 0.5700 0.0197
-6.500 -0.2492 0.01177 0.00470 -0.0931 0.5672 0.0220
-6.250 -0.2230 0.01153 0.00446 -0.0932 0.5654 0.0254
-6.000 -0.1963 0.01133 0.00425 -0.0933 0.5635 0.0282
-5.750 -0.1698 0.01111 0.00405 -0.0934 0.5616 0.0323
-5.500 -0.1433 0.01089 0.00385 -0.0935 0.5598 0.0393
-5.250 -0.1167 0.01067 0.00365 -0.0936 0.5580 0.0487
-5.000 -0.0896 0.01051 0.00349 -0.0938 0.5563 0.0563
-4.750 -0.0630 0.01029 0.00332 -0.0939 0.5546 0.0696
-4.500 -0.0363 0.01008 0.00315 -0.0941 0.5529 0.0888
-4.250 -0.0099 0.00982 0.00297 -0.0942 0.5513 0.1170
-4.000 0.0165 0.00948 0.00278 -0.0944 0.5502 0.1552
-3.750 0.0432 0.00919 0.00261 -0.0946 0.5490 0.1934
-3.500 0.0675 0.00860 0.00234 -0.0946 0.5476 0.2841
-3.250 0.0925 0.00812 0.00211 -0.0946 0.5462 0.3592
-3.000 0.1183 0.00776 0.00194 -0.0947 0.5448 0.4261
-2.750 0.1454 0.00760 0.00197 -0.0948 0.5434 0.4826
-2.500 0.1746 0.00765 0.00196 -0.0952 0.5420 0.4973
-2.250 0.2033 0.00766 0.00198 -0.0955 0.5406 0.5073
-2.000 0.2322 0.00771 0.00197 -0.0959 0.5392 0.5138
-1.750 0.2607 0.00772 0.00197 -0.0962 0.5379 0.5172
-1.250 0.3182 0.00778 0.00199 -0.0968 0.5355 0.5249
-1.000 0.3471 0.00780 0.00201 -0.0972 0.5344 0.5316
-0.750 0.3759 0.00782 0.00204 -0.0976 0.5332 0.5355
-0.500 0.4047 0.00784 0.00205 -0.0979 0.5320 0.5376
-0.250 0.4335 0.00787 0.00207 -0.0983 0.5308 0.5393
0.000 0.4623 0.00790 0.00208 -0.0987 0.5297 0.5403
0.250 0.4909 0.00793 0.00210 -0.0990 0.5285 0.5413
0.500 0.5195 0.00797 0.00212 -0.0994 0.5274 0.5421
0.750 0.5480 0.00801 0.00214 -0.0997 0.5262 0.5430
1.000 0.5764 0.00805 0.00217 -0.1000 0.5251 0.5435
1.500 0.6328 0.00814 0.00225 -0.1006 0.5228 0.5442
1.750 0.6608 0.00820 0.00230 -0.1008 0.5216 0.5447
2.000 0.6891 0.00823 0.00235 -0.1012 0.5207 0.5452
2.250 0.7175 0.00826 0.00240 -0.1015 0.5199 0.5457
2.500 0.7458 0.00830 0.00246 -0.1018 0.5191 0.5462
2.750 0.7740 0.00834 0.00252 -0.1021 0.5182 0.5469
3.000 0.8021 0.00838 0.00258 -0.1024 0.5171 0.5476
3.250 0.8301 0.00843 0.00266 -0.1027 0.5160 0.5484
3.500 0.8580 0.00847 0.00273 -0.1030 0.5146 0.5491
3.750 0.8856 0.00853 0.00280 -0.1032 0.5130 0.5498
4.000 0.9131 0.00859 0.00288 -0.1034 0.5113 0.5504
4.250 0.9402 0.00866 0.00296 -0.1035 0.5096 0.5510
4.500 0.9672 0.00874 0.00306 -0.1036 0.5080 0.5517
4.750 0.9940 0.00885 0.00317 -0.1037 0.5059 0.5524
5.000 1.0215 0.00888 0.00326 -0.1039 0.5045 0.5533
5.250 1.0488 0.00893 0.00335 -0.1041 0.5026 0.5544
5.500 1.0758 0.00897 0.00345 -0.1042 0.5001 0.5556
5.750 1.1025 0.00904 0.00355 -0.1043 0.4977 0.5566
6.000 1.1286 0.00912 0.00365 -0.1042 0.4949 0.5576
6.250 1.1533 0.00923 0.00377 -0.1039 0.4911 0.5585
6.500 1.1798 0.00928 0.00388 -0.1039 0.4874 0.5593
6.750 1.2050 0.00933 0.00397 -0.1037 0.4805 0.5605
7.000 1.2285 0.00943 0.00409 -0.1032 0.4729 0.5619
7.250 1.2507 0.00956 0.00423 -0.1025 0.4623 0.5633
7.500 1.2705 0.00976 0.00441 -0.1012 0.4491 0.5648
7.750 1.2825 0.01014 0.00471 -0.0986 0.4255 0.5664
8.000 1.2779 0.01084 0.00522 -0.0929 0.3875 0.5680
8.250 1.2693 0.01185 0.00604 -0.0868 0.3504 0.5697
8.500 1.2590 0.01304 0.00708 -0.0810 0.3178 0.5714
8.750 1.2452 0.01458 0.00847 -0.0754 0.2826 0.5729
9.000 1.2409 0.01600 0.00980 -0.0716 0.2607 0.5746
9.250 1.2267 0.01818 0.01185 -0.0673 0.2287 0.5764
9.500 1.2100 0.02087 0.01439 -0.0634 0.1968 0.5785
9.750 1.2082 0.02284 0.01633 -0.0613 0.1788 0.5808
10.000 1.2005 0.02536 0.01876 -0.0590 0.1562 0.5830
10.250 1.1931 0.02794 0.02127 -0.0569 0.1353 0.5853
10.500 1.1874 0.03048 0.02374 -0.0551 0.1149 0.5876
10.750 1.1821 0.03308 0.02626 -0.0535 0.0967 0.5895
11.000 1.1812 0.03543 0.02857 -0.0523 0.0809 0.5920
11.250 1.1823 0.03769 0.03080 -0.0514 0.0688 0.5945
11.500 1.1844 0.03994 0.03303 -0.0506 0.0567 0.5978
11.750 1.1884 0.04205 0.03512 -0.0499 0.0472 0.6010
12.000 1.1926 0.04419 0.03725 -0.0493 0.0397 0.6039
12.250 1.1986 0.04616 0.03922 -0.0488 0.0332 0.6070
12.500 1.2033 0.04837 0.04142 -0.0484 0.0257 0.6106
12.750 1.2098 0.05041 0.04346 -0.0481 0.0207 0.6145
13.000 1.2186 0.05229 0.04539 -0.0480 0.0186 0.6195
13.500 1.2366 0.05607 0.04925 -0.0479 0.0141 0.6307
13.750 1.2444 0.05814 0.05136 -0.0479 0.0124 0.6375
14.000 1.2540 0.06008 0.05335 -0.0480 0.0106 0.6449
14.250 1.2623 0.06213 0.05545 -0.0481 0.0091 0.6533
14.500 1.2716 0.06417 0.05756 -0.0484 0.0084 0.6615
15.000 1.2909 0.06838 0.06190 -0.0492 0.0071 0.6839
15.250 1.3009 0.07061 0.06422 -0.0498 0.0067 0.6974
15.500 1.3121 0.07280 0.06650 -0.0506 0.0064 0.7135
15.750 1.3222 0.07522 0.06901 -0.0517 0.0058 0.7311
16.000 1.3371 0.07784 0.07177 -0.0537 0.0058 0.7601
16.250 1.3510 0.08080 0.07489 -0.0562 0.0053 0.7915
16.500 1.4133 0.08619 0.08076 -0.0704 0.0049 0.9436
16.750 1.4143 0.08832 0.08294 -0.0690 0.0048 0.9983
17.000 1.4258 0.09137 0.08604 -0.0708 0.0046 0.9999
17.250 1.4319 0.09392 0.08864 -0.0712 0.0044 1.0000
17.500 1.4356 0.09660 0.09137 -0.0714 0.0043 1.0000
17.750 1.4387 0.09935 0.09416 -0.0715 0.0041 1.0000
18.000 1.4414 0.10215 0.09701 -0.0717 0.0040 1.0000
18.250 1.4424 0.10524 0.10017 -0.0720 0.0038 1.0000
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