FX S 02/1-158 AIRFOIL (fxs21158-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
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Airfoil: FX S 02/1-158 AIRFOIL (fxs21158-il) Reynolds number: 200,000 Max Cl/Cd: 72.12 at α=7.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fxs21158-il-200000-n5.txt Download as CSV file: xf-fxs21158-il-200000-n5.csv |
XFOIL Version 6.96
Calculated polar for: FX S 02/1-158 AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.200 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-11.000 -0.4192 0.08012 0.07703 -0.0498 0.9320 0.0130
-10.750 -0.4968 0.05859 0.05527 -0.0655 0.9284 0.0114
-10.500 -0.4959 0.04778 0.04383 -0.0834 0.8449 0.0121
-10.250 -0.5100 0.04215 0.03771 -0.0886 0.7903 0.0127
-10.000 -0.5294 0.03765 0.03267 -0.0897 0.7569 0.0139
-9.750 -0.5325 0.03426 0.02858 -0.0894 0.7314 0.0154
-9.500 -0.5230 0.03264 0.02671 -0.0891 0.7092 0.0161
-9.250 -0.5059 0.03218 0.02612 -0.0888 0.6888 0.0170
-9.000 -0.4879 0.03175 0.02551 -0.0886 0.6717 0.0182
-8.750 -0.4695 0.03108 0.02458 -0.0884 0.6572 0.0202
-8.500 -0.4511 0.02989 0.02303 -0.0880 0.6439 0.0217
-8.250 -0.4318 0.02876 0.02155 -0.0877 0.6318 0.0229
-7.750 -0.3897 0.02725 0.01982 -0.0877 0.6107 0.0265
-7.500 -0.3670 0.02634 0.01868 -0.0875 0.6021 0.0280
-7.250 -0.3438 0.02527 0.01736 -0.0872 0.5940 0.0290
-7.000 -0.3201 0.02403 0.01589 -0.0868 0.5866 0.0294
-6.750 -0.2959 0.02297 0.01462 -0.0865 0.5796 0.0298
-6.500 -0.2714 0.02200 0.01350 -0.0861 0.5729 0.0302
-6.250 -0.2467 0.02118 0.01253 -0.0858 0.5665 0.0306
-6.000 -0.2219 0.02043 0.01165 -0.0854 0.5610 0.0310
-5.750 -0.1969 0.01976 0.01084 -0.0851 0.5556 0.0314
-5.500 -0.1717 0.01917 0.01014 -0.0849 0.5512 0.0317
-5.250 -0.1478 0.01827 0.00919 -0.0847 0.5469 0.0331
-5.000 -0.1225 0.01765 0.00852 -0.0847 0.5423 0.0344
-4.750 -0.0965 0.01714 0.00792 -0.0847 0.5380 0.0354
-4.500 -0.0701 0.01669 0.00734 -0.0848 0.5343 0.0362
-4.250 -0.0429 0.01626 0.00681 -0.0850 0.5299 0.0374
-4.000 -0.0154 0.01590 0.00634 -0.0852 0.5258 0.0389
-3.750 0.0122 0.01561 0.00591 -0.0854 0.5223 0.0412
-3.500 0.0400 0.01532 0.00551 -0.0855 0.5193 0.0459
-3.250 0.0680 0.01498 0.00518 -0.0858 0.5158 0.0612
-3.000 0.0957 0.01448 0.00481 -0.0863 0.5125 0.1135
-2.750 0.1210 0.01318 0.00460 -0.0873 0.5096 0.4022
-2.500 0.1495 0.01332 0.00463 -0.0873 0.5071 0.4412
-2.250 0.1777 0.01358 0.00485 -0.0873 0.5048 0.4726
-2.000 0.2060 0.01384 0.00506 -0.0872 0.5021 0.4946
-1.750 0.2341 0.01401 0.00519 -0.0871 0.4995 0.5060
-1.500 0.2627 0.01409 0.00515 -0.0872 0.4970 0.5125
-1.250 0.2908 0.01414 0.00514 -0.0873 0.4948 0.5156
-1.000 0.3192 0.01419 0.00510 -0.0874 0.4928 0.5183
-0.750 0.3477 0.01426 0.00508 -0.0875 0.4909 0.5210
-0.500 0.3762 0.01430 0.00507 -0.0877 0.4887 0.5236
-0.250 0.4048 0.01437 0.00508 -0.0879 0.4865 0.5271
0.000 0.4328 0.01443 0.00515 -0.0880 0.4843 0.5305
0.250 0.4609 0.01452 0.00520 -0.0881 0.4820 0.5348
0.500 0.4892 0.01461 0.00523 -0.0882 0.4797 0.5395
0.750 0.5174 0.01472 0.00527 -0.0883 0.4777 0.5432
1.000 0.5453 0.01479 0.00537 -0.0884 0.4751 0.5461
1.250 0.5733 0.01486 0.00546 -0.0885 0.4725 0.5487
1.500 0.6013 0.01492 0.00552 -0.0886 0.4696 0.5510
1.750 0.6294 0.01500 0.00558 -0.0888 0.4670 0.5533
2.000 0.6575 0.01510 0.00563 -0.0889 0.4647 0.5556
2.250 0.6856 0.01522 0.00572 -0.0891 0.4627 0.5577
2.500 0.7131 0.01529 0.00589 -0.0891 0.4603 0.5601
2.750 0.7407 0.01540 0.00607 -0.0892 0.4579 0.5627
3.000 0.7684 0.01551 0.00622 -0.0893 0.4556 0.5655
3.250 0.7961 0.01562 0.00636 -0.0894 0.4534 0.5683
3.500 0.8239 0.01574 0.00650 -0.0895 0.4511 0.5710
3.750 0.8514 0.01583 0.00663 -0.0896 0.4489 0.5736
4.000 0.8783 0.01594 0.00684 -0.0896 0.4460 0.5767
4.250 0.9052 0.01604 0.00704 -0.0895 0.4425 0.5803
4.500 0.9322 0.01609 0.00716 -0.0895 0.4384 0.5840
4.750 0.9591 0.01611 0.00717 -0.0894 0.4343 0.5872
5.000 0.9850 0.01613 0.00736 -0.0892 0.4280 0.5906
5.250 1.0113 0.01612 0.00739 -0.0890 0.4221 0.5947
5.500 1.0375 0.01620 0.00755 -0.0888 0.4170 0.5992
5.750 1.0635 0.01631 0.00780 -0.0887 0.4127 0.6033
6.000 1.0896 0.01641 0.00799 -0.0885 0.4088 0.6083
6.250 1.1158 0.01654 0.00817 -0.0883 0.4057 0.6144
6.500 1.1416 0.01669 0.00851 -0.0882 0.4021 0.6203
6.750 1.1672 0.01686 0.00887 -0.0880 0.3981 0.6277
7.000 1.1917 0.01690 0.00900 -0.0875 0.3902 0.6353
7.500 1.2333 0.01710 0.00919 -0.0855 0.3321 0.6542
7.750 1.2452 0.01792 0.00973 -0.0835 0.2766 0.6658
8.000 1.2440 0.01971 0.01115 -0.0800 0.1944 0.6793
8.250 1.2470 0.02111 0.01245 -0.0770 0.1632 0.6976
8.500 1.2445 0.02256 0.01387 -0.0734 0.1294 0.7246
9.000 1.2296 0.02534 0.01692 -0.0653 0.0857 1.0000
9.250 1.2263 0.02723 0.01882 -0.0631 0.0610 1.0000
9.500 1.2219 0.02955 0.02114 -0.0616 0.0558 1.0000
9.750 1.2191 0.03208 0.02371 -0.0608 0.0499 1.0000
10.000 1.2249 0.03402 0.02577 -0.0603 0.0408 1.0000
10.250 1.2197 0.03712 0.02891 -0.0599 0.0365 1.0000
10.500 1.2147 0.04032 0.03215 -0.0597 0.0323 1.0000
10.750 1.2137 0.04316 0.03506 -0.0595 0.0298 1.0000
11.000 1.2102 0.04631 0.03827 -0.0594 0.0266 1.0000
11.250 1.2068 0.04949 0.04150 -0.0593 0.0238 1.0000
11.500 1.2107 0.05191 0.04403 -0.0593 0.0193 1.0000
11.750 1.2079 0.05507 0.04721 -0.0593 0.0125 1.0000
12.000 1.2047 0.05831 0.05048 -0.0594 0.0095 1.0000
12.250 1.2029 0.06153 0.05378 -0.0596 0.0077 1.0000
12.500 1.2034 0.06456 0.05686 -0.0599 0.0071 1.0000
12.750 1.2045 0.06760 0.05999 -0.0601 0.0066 1.0000
13.000 1.2063 0.07061 0.06309 -0.0605 0.0063 1.0000
13.250 1.2077 0.07372 0.06629 -0.0609 0.0059 1.0000
13.500 1.2096 0.07683 0.06950 -0.0614 0.0056 1.0000
13.750 1.2103 0.08014 0.07289 -0.0620 0.0052 1.0000
14.000 1.2105 0.08357 0.07640 -0.0626 0.0049 1.0000
14.250 1.2108 0.08705 0.07996 -0.0633 0.0046 1.0000
14.500 1.2126 0.09038 0.08340 -0.0641 0.0045 1.0000
14.750 1.2146 0.09369 0.08681 -0.0649 0.0041 1.0000
15.000 1.2163 0.09711 0.09034 -0.0657 0.0041 1.0000
15.250 1.2175 0.10064 0.09398 -0.0666 0.0039 1.0000
15.500 1.2192 0.10412 0.09755 -0.0676 0.0038 1.0000
15.750 1.2203 0.10774 0.10132 -0.0687 0.0038 1.0000
16.000 1.2212 0.11142 0.10510 -0.0698 0.0037 1.0000
16.250 1.2222 0.11510 0.10889 -0.0710 0.0036 1.0000
16.500 1.2235 0.11878 0.11267 -0.0723 0.0036 1.0000
16.750 1.2241 0.12259 0.11658 -0.0736 0.0035 1.0000
17.000 1.2253 0.12631 0.12041 -0.0750 0.0035 1.0000
17.250 1.2265 0.13005 0.12425 -0.0765 0.0034 1.0000
17.500 1.2273 0.13387 0.12818 -0.0781 0.0034 1.0000
17.750 1.2282 0.13767 0.13209 -0.0797 0.0033 1.0000
18.000 1.2289 0.14154 0.13605 -0.0814 0.0033 1.0000
18.250 1.2303 0.14532 0.13994 -0.0832 0.0032 1.0000
18.500 1.2313 0.14916 0.14389 -0.0850 0.0032 1.0000
18.750 1.2317 0.15318 0.14802 -0.0870 0.0032 1.0000
19.000 1.2323 0.15717 0.15213 -0.0891 0.0032 1.0000
19.250 1.2317 0.16141 0.15649 -0.0914 0.0031 1.0000
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