FX S 02-196 AIRFOIL (fxs02196-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: FX S 02-196 AIRFOIL (fxs02196-il) Reynolds number: 1,000,000 Max Cl/Cd: 54.86 at α=4.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fxs02196-il-1000000-n5.txt Download as CSV file: xf-fxs02196-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: FX S 02-196 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 -0.8158 0.10885 0.10603 -0.0564 1.0000 0.0053
-19.500 -0.8410 0.10058 0.09762 -0.0610 1.0000 0.0054
-19.250 -0.8594 0.09366 0.09058 -0.0648 1.0000 0.0054
-19.000 -0.8719 0.08798 0.08479 -0.0679 1.0000 0.0054
-18.750 -0.8821 0.08273 0.07943 -0.0708 1.0000 0.0054
-18.500 -0.8921 0.07766 0.07426 -0.0735 1.0000 0.0054
-18.250 -0.8978 0.07339 0.06990 -0.0757 1.0000 0.0054
-18.000 -0.9010 0.06940 0.06583 -0.0779 0.9999 0.0054
-17.750 -0.9103 0.06591 0.06227 -0.0776 0.9812 0.0055
-17.500 -0.8734 0.06058 0.05678 -0.0895 0.9471 0.0056
-17.250 -0.8268 0.05576 0.05178 -0.1022 0.9309 0.0057
-17.000 -0.7927 0.05214 0.04789 -0.1109 0.8901 0.0059
-16.750 -0.7886 0.05003 0.04554 -0.1115 0.8517 0.0059
-16.500 -0.7857 0.04795 0.04331 -0.1118 0.8287 0.0060
-16.250 -0.7818 0.04600 0.04123 -0.1120 0.8093 0.0061
-16.000 -0.7767 0.04420 0.03930 -0.1122 0.7927 0.0061
-15.500 -0.7633 0.04085 0.03576 -0.1125 0.7665 0.0062
-15.250 -0.7547 0.03943 0.03425 -0.1125 0.7524 0.0064
-15.000 -0.7428 0.03825 0.03301 -0.1126 0.7401 0.0066
-14.750 -0.7351 0.03681 0.03147 -0.1125 0.7297 0.0066
-14.500 -0.7206 0.03588 0.03052 -0.1127 0.7191 0.0070
-14.250 -0.7064 0.03503 0.02963 -0.1127 0.7050 0.0073
-14.000 -0.6918 0.03416 0.02875 -0.1129 0.6961 0.0077
-13.750 -0.6790 0.03325 0.02778 -0.1128 0.6828 0.0080
-13.500 -0.6708 0.03204 0.02645 -0.1123 0.6677 0.0079
-13.250 -0.6595 0.03098 0.02531 -0.1120 0.6594 0.0095
-13.000 -0.6498 0.02993 0.02412 -0.1114 0.6406 0.0100
-12.750 -0.6388 0.02884 0.02295 -0.1109 0.6387 0.0106
-12.500 -0.6291 0.02781 0.02182 -0.1102 0.6241 0.0106
-12.250 -0.6152 0.02699 0.02093 -0.1099 0.6184 0.0111
-12.000 -0.6023 0.02615 0.02001 -0.1093 0.6106 0.0115
-11.750 -0.5905 0.02523 0.01903 -0.1087 0.6058 0.0115
-11.500 -0.5762 0.02446 0.01819 -0.1082 0.5993 0.0120
-11.250 -0.5615 0.02374 0.01740 -0.1077 0.5948 0.0124
-11.000 -0.5486 0.02297 0.01655 -0.1070 0.5871 0.0125
-10.750 -0.5326 0.02236 0.01585 -0.1065 0.5785 0.0128
-10.500 -0.5171 0.02177 0.01516 -0.1060 0.5714 0.0130
-10.250 -0.5033 0.02108 0.01441 -0.1052 0.5669 0.0132
-10.000 -0.4903 0.02032 0.01363 -0.1042 0.5632 0.0132
-9.750 -0.4778 0.01959 0.01287 -0.1031 0.5588 0.0134
-9.500 -0.4667 0.01884 0.01209 -0.1017 0.5554 0.0134
-9.250 -0.4572 0.01825 0.01147 -0.1000 0.5505 0.0136
-8.750 -0.4311 0.01722 0.01036 -0.0974 0.5430 0.0139
-8.500 -0.4121 0.01679 0.00990 -0.0967 0.5386 0.0142
-8.250 -0.3926 0.01637 0.00943 -0.0960 0.5322 0.0142
-8.000 -0.3716 0.01602 0.00902 -0.0955 0.5243 0.0145
-7.750 -0.3494 0.01565 0.00861 -0.0951 0.5203 0.0147
-7.500 -0.3267 0.01528 0.00821 -0.0948 0.5147 0.0149
-7.250 -0.3032 0.01498 0.00785 -0.0946 0.5082 0.0151
-7.000 -0.2789 0.01470 0.00752 -0.0944 0.5030 0.0153
-6.750 -0.2536 0.01447 0.00724 -0.0944 0.4972 0.0155
-6.500 -0.2270 0.01442 0.00711 -0.0944 0.4887 0.0157
-6.250 -0.2047 0.01388 0.00654 -0.0942 0.4811 0.0160
-6.000 -0.1818 0.01341 0.00601 -0.0940 0.4697 0.0165
-5.750 -0.1563 0.01309 0.00566 -0.0941 0.4617 0.0169
-5.500 -0.1308 0.01288 0.00536 -0.0942 0.4444 0.0172
-5.250 -0.1139 0.01348 0.00544 -0.0928 0.3113 0.0173
-5.000 -0.0909 0.01362 0.00536 -0.0924 0.2473 0.0175
-4.750 -0.0654 0.01357 0.00521 -0.0924 0.2220 0.0175
-4.500 -0.0400 0.01358 0.00509 -0.0924 0.1778 0.0176
-4.250 -0.0129 0.01347 0.00493 -0.0926 0.1672 0.0177
-4.000 0.0148 0.01333 0.00477 -0.0928 0.1625 0.0178
-3.750 0.0415 0.01332 0.00467 -0.0929 0.1305 0.0179
-3.500 0.0692 0.01324 0.00455 -0.0932 0.1262 0.0180
-3.250 0.0971 0.01316 0.00445 -0.0935 0.1226 0.0181
-3.000 0.1251 0.01308 0.00435 -0.0938 0.1206 0.0181
-2.750 0.1532 0.01302 0.00427 -0.0941 0.1177 0.0182
-2.500 0.1802 0.01306 0.00423 -0.0942 0.0905 0.0183
-2.250 0.2080 0.01305 0.00419 -0.0944 0.0853 0.0183
-2.000 0.2358 0.01304 0.00416 -0.0947 0.0821 0.0184
-1.750 0.2636 0.01304 0.00414 -0.0949 0.0794 0.0184
-1.500 0.2916 0.01303 0.00411 -0.0952 0.0780 0.0187
-1.250 0.3190 0.01307 0.00410 -0.0953 0.0603 0.0189
-0.750 0.3738 0.01315 0.00414 -0.0957 0.0542 0.0193
-0.500 0.4012 0.01320 0.00417 -0.0958 0.0534 0.0194
-0.250 0.4285 0.01325 0.00422 -0.0959 0.0525 0.0195
0.000 0.4556 0.01332 0.00427 -0.0961 0.0518 0.0197
0.250 0.4825 0.01340 0.00435 -0.0961 0.0507 0.0200
0.500 0.5093 0.01347 0.00441 -0.0962 0.0499 0.0204
1.000 0.5625 0.01364 0.00459 -0.0963 0.0488 0.0310
1.250 0.5887 0.01375 0.00470 -0.0962 0.0478 0.0332
1.500 0.6147 0.01386 0.00481 -0.0962 0.0467 0.0347
1.750 0.6403 0.01398 0.00493 -0.0960 0.0454 0.0359
2.000 0.6657 0.01410 0.00505 -0.0959 0.0444 0.0371
2.250 0.6909 0.01422 0.00517 -0.0957 0.0432 0.0394
2.500 0.7149 0.01439 0.00531 -0.0953 0.0321 0.0412
2.750 0.7386 0.01456 0.00546 -0.0949 0.0313 0.0438
3.000 0.7618 0.01473 0.00565 -0.0944 0.0303 0.0617
3.250 0.7845 0.01491 0.00584 -0.0938 0.0299 0.0667
3.500 0.8061 0.01510 0.00604 -0.0930 0.0295 0.0698
3.750 0.8248 0.01527 0.00624 -0.0916 0.0292 0.0738
4.000 0.8422 0.01547 0.00646 -0.0901 0.0288 0.0955
4.250 0.8598 0.01572 0.00674 -0.0886 0.0286 0.1012
4.500 0.8774 0.01602 0.00706 -0.0873 0.0285 0.1066
4.750 0.8953 0.01632 0.00742 -0.0861 0.0284 0.1415
5.000 0.9121 0.01669 0.00782 -0.0847 0.0283 0.1500
5.250 0.9291 0.01704 0.00826 -0.0836 0.0282 0.1931
5.500 0.9452 0.01748 0.00875 -0.0823 0.0282 0.2064
5.750 0.9615 0.01790 0.00927 -0.0813 0.0281 0.2569
6.250 0.9955 0.01864 0.01048 -0.0799 0.0279 0.4372
6.500 1.0096 0.01931 0.01121 -0.0787 0.0279 0.4509
6.750 1.0232 0.02004 0.01200 -0.0775 0.0278 0.4606
7.000 1.0367 0.02082 0.01286 -0.0764 0.0277 0.4780
7.250 1.0497 0.02167 0.01376 -0.0753 0.0276 0.4868
7.500 1.0619 0.02262 0.01475 -0.0742 0.0276 0.4955
7.750 1.0738 0.02363 0.01580 -0.0731 0.0275 0.5011
8.000 1.0857 0.02467 0.01690 -0.0722 0.0274 0.5099
8.250 1.0971 0.02578 0.01807 -0.0712 0.0273 0.5166
8.750 1.1183 0.02822 0.02062 -0.0694 0.0272 0.5292
9.000 1.1280 0.02956 0.02202 -0.0685 0.0271 0.5374
9.250 1.1375 0.03094 0.02346 -0.0676 0.0270 0.5434
9.500 1.1468 0.03236 0.02494 -0.0668 0.0268 0.5555
9.750 1.1548 0.03393 0.02655 -0.0660 0.0267 0.5588
10.000 1.1640 0.03543 0.02811 -0.0653 0.0266 0.5654
10.250 1.1713 0.03715 0.02989 -0.0646 0.0264 0.5729
10.500 1.1783 0.03892 0.03171 -0.0639 0.0261 0.5786
10.750 1.1851 0.04076 0.03362 -0.0633 0.0259 0.5831
11.000 1.1937 0.04247 0.03538 -0.0629 0.0258 0.5884
11.250 1.2002 0.04444 0.03742 -0.0624 0.0257 0.5948
11.500 1.2074 0.04633 0.03938 -0.0620 0.0255 0.6026
11.750 1.2129 0.04848 0.04159 -0.0616 0.0254 0.6090
12.000 1.2169 0.05080 0.04397 -0.0612 0.0251 0.6164
12.250 1.2263 0.05262 0.04584 -0.0610 0.0250 0.6210
12.500 1.2384 0.05420 0.04749 -0.0610 0.0248 0.6315
12.750 1.2504 0.05577 0.04913 -0.0610 0.0245 0.6427
13.000 1.2609 0.05752 0.05096 -0.0610 0.0243 0.6533
13.250 1.2705 0.05942 0.05297 -0.0611 0.0239 0.6769
13.500 1.2793 0.06144 0.05507 -0.0611 0.0237 0.6934
13.750 1.2885 0.06340 0.05713 -0.0612 0.0236 0.7085
14.000 1.2987 0.06526 0.05910 -0.0613 0.0231 0.7333
14.250 1.3064 0.06749 0.06143 -0.0615 0.0229 0.7534
14.500 1.3159 0.06948 0.06352 -0.0617 0.0224 0.7780
14.750 1.3248 0.07150 0.06568 -0.0619 0.0222 0.8146
15.000 1.3287 0.07325 0.06779 -0.0611 0.0219 1.0000
15.250 1.3348 0.07578 0.07036 -0.0614 0.0217 1.0000
15.500 1.3407 0.07834 0.07296 -0.0618 0.0215 1.0000
15.750 1.3479 0.08074 0.07540 -0.0622 0.0213 1.0000
16.000 1.3586 0.08276 0.07747 -0.0626 0.0211 1.0000
16.250 1.3667 0.08513 0.07989 -0.0631 0.0210 1.0000
16.500 1.3777 0.08710 0.08190 -0.0636 0.0207 1.0000
16.750 1.3879 0.08915 0.08400 -0.0641 0.0204 1.0000
17.000 1.3988 0.09112 0.08601 -0.0646 0.0198 1.0000
17.250 1.4061 0.09364 0.08859 -0.0652 0.0194 1.0000
17.500 1.4143 0.09602 0.09101 -0.0659 0.0190 1.0000
17.750 1.4233 0.09829 0.09332 -0.0665 0.0185 1.0000
18.000 1.4335 0.10039 0.09546 -0.0671 0.0181 1.0000
18.250 1.4416 0.10279 0.09790 -0.0679 0.0178 1.0000
18.500 1.4461 0.10573 0.10090 -0.0688 0.0175 1.0000
18.750 1.4529 0.10833 0.10356 -0.0696 0.0169 1.0000
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