WORTMANN FX 60-126/1 AIRFOIL (fx601261-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: WORTMANN FX 60-126/1 AIRFOIL (fx601261-il) Reynolds number: 1,000,000 Max Cl/Cd: 88.21 at α=6.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx601261-il-1000000-n5.txt Download as CSV file: xf-fx601261-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 60-126/1 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
------ -------- --------- --------- -------- -------- --------
-11.250 -0.3535 0.11180 0.11008 -0.0348 1.0000 0.0047
-11.000 -0.3528 0.10756 0.10586 -0.0360 1.0000 0.0047
-10.750 -0.3525 0.10335 0.10166 -0.0372 1.0000 0.0047
-10.500 -0.2439 0.07644 0.07481 -0.0578 0.9543 0.0047
-10.250 -0.2308 0.07104 0.06940 -0.0642 0.9443 0.0045
-10.000 -0.2536 0.05634 0.05465 -0.0723 0.9392 0.0042
-9.750 -0.3530 0.07761 0.07596 -0.0532 0.9825 0.0046
-9.500 -0.3670 0.06482 0.06313 -0.0640 0.9566 0.0042
-9.250 -0.3610 0.04479 0.04269 -0.0960 0.9316 0.0041
-9.000 -0.3419 0.03283 0.03005 -0.1232 0.8831 0.0039
-8.750 -0.3389 0.02964 0.02653 -0.1259 0.8607 0.0038
-8.500 -0.3325 0.02653 0.02305 -0.1269 0.8454 0.0038
-8.250 -0.3190 0.02407 0.02027 -0.1274 0.8336 0.0037
-8.000 -0.3013 0.02197 0.01789 -0.1276 0.8238 0.0037
-7.750 -0.2805 0.02022 0.01588 -0.1278 0.8166 0.0038
-7.500 -0.2579 0.01872 0.01416 -0.1279 0.8093 0.0039
-7.250 -0.2338 0.01748 0.01271 -0.1279 0.8032 0.0040
-7.000 -0.2086 0.01643 0.01149 -0.1280 0.7967 0.0042
-6.500 -0.1561 0.01500 0.00976 -0.1279 0.7829 0.0045
-6.250 -0.1282 0.01502 0.00958 -0.1280 0.7751 0.0048
-6.000 -0.1032 0.01353 0.00802 -0.1279 0.7684 0.0049
-5.750 -0.0768 0.01277 0.00720 -0.1279 0.7612 0.0050
-5.500 -0.0498 0.01211 0.00649 -0.1280 0.7544 0.0051
-5.250 -0.0225 0.01156 0.00589 -0.1281 0.7465 0.0052
-5.000 0.0051 0.01109 0.00536 -0.1281 0.7380 0.0053
-4.750 0.0327 0.01068 0.00490 -0.1283 0.7289 0.0056
-4.500 0.0609 0.01030 0.00447 -0.1284 0.7206 0.0058
-4.250 0.0891 0.00996 0.00407 -0.1285 0.7123 0.0060
-4.000 0.1177 0.00962 0.00366 -0.1287 0.7025 0.0059
-3.750 0.1460 0.00933 0.00330 -0.1288 0.6920 0.0058
-3.500 0.1745 0.00909 0.00297 -0.1289 0.6814 0.0058
-3.250 0.2032 0.00887 0.00270 -0.1290 0.6723 0.0057
-3.000 0.2317 0.00869 0.00245 -0.1291 0.6626 0.0056
-2.750 0.2602 0.00855 0.00224 -0.1291 0.6513 0.0056
-2.500 0.2883 0.00845 0.00206 -0.1291 0.6352 0.0056
-2.250 0.3161 0.00841 0.00191 -0.1289 0.6163 0.0056
-2.000 0.3437 0.00839 0.00179 -0.1288 0.5955 0.0056
-1.750 0.3710 0.00842 0.00169 -0.1286 0.5712 0.0057
-1.500 0.3989 0.00843 0.00161 -0.1285 0.5536 0.0057
-1.250 0.4267 0.00845 0.00155 -0.1284 0.5375 0.0059
-1.000 0.4547 0.00848 0.00151 -0.1283 0.5226 0.0062
-0.750 0.4825 0.00853 0.00148 -0.1282 0.5060 0.0066
-0.500 0.5107 0.00851 0.00145 -0.1282 0.4919 0.0392
-0.250 0.5398 0.00817 0.00137 -0.1287 0.4781 0.1624
0.000 0.5689 0.00776 0.00135 -0.1294 0.4617 0.3198
0.250 0.5960 0.00784 0.00143 -0.1293 0.4329 0.3632
0.500 0.6222 0.00803 0.00155 -0.1291 0.3983 0.3980
0.750 0.6485 0.00826 0.00166 -0.1288 0.3656 0.4117
1.000 0.6754 0.00844 0.00177 -0.1286 0.3448 0.4255
1.250 0.7022 0.00862 0.00188 -0.1284 0.3241 0.4378
1.500 0.7286 0.00885 0.00202 -0.1281 0.2974 0.4481
1.750 0.7554 0.00904 0.00214 -0.1278 0.2810 0.4585
2.000 0.7819 0.00925 0.00228 -0.1276 0.2599 0.4655
2.250 0.8073 0.00959 0.00247 -0.1271 0.2289 0.4731
2.500 0.8331 0.00987 0.00266 -0.1268 0.2038 0.4816
2.750 0.8582 0.01022 0.00288 -0.1263 0.1767 0.4906
3.000 0.8846 0.01044 0.00306 -0.1260 0.1612 0.4987
3.250 0.9100 0.01075 0.00328 -0.1256 0.1396 0.5063
3.500 0.9362 0.01098 0.00347 -0.1253 0.1282 0.5145
3.750 0.9622 0.01122 0.00367 -0.1250 0.1174 0.5223
4.000 0.9881 0.01146 0.00389 -0.1246 0.1032 0.5300
4.250 1.0139 0.01172 0.00410 -0.1242 0.0951 0.5379
4.500 1.0401 0.01192 0.00431 -0.1240 0.0897 0.5464
4.750 1.0662 0.01213 0.00452 -0.1236 0.0847 0.5554
5.000 1.0915 0.01241 0.00478 -0.1232 0.0745 0.5646
5.250 1.1151 0.01284 0.00512 -0.1225 0.0574 0.5741
5.750 1.1661 0.01330 0.00563 -0.1218 0.0515 0.5988
6.000 1.1910 0.01357 0.00592 -0.1213 0.0475 0.6118
6.250 1.2164 0.01379 0.00618 -0.1209 0.0438 0.6251
6.500 1.2387 0.01428 0.00662 -0.1201 0.0310 0.6391
6.750 1.2627 0.01460 0.00696 -0.1195 0.0290 0.6549
7.000 1.2866 0.01491 0.00732 -0.1189 0.0265 0.6746
7.250 1.3108 0.01518 0.00766 -0.1183 0.0251 0.6998
7.500 1.3351 0.01541 0.00800 -0.1178 0.0245 0.7358
7.750 1.3587 0.01564 0.00837 -0.1172 0.0228 0.7884
8.000 1.3717 0.01578 0.00881 -0.1143 0.0154 1.0000
8.250 1.3871 0.01673 0.00969 -0.1124 0.0025 1.0000
8.500 1.4082 0.01716 0.01015 -0.1114 0.0022 1.0000
8.750 1.4287 0.01762 0.01063 -0.1102 0.0021 1.0000
9.000 1.4484 0.01810 0.01115 -0.1090 0.0020 1.0000
9.250 1.4664 0.01861 0.01170 -0.1075 0.0019 1.0000
9.500 1.4822 0.01913 0.01227 -0.1055 0.0018 1.0000
9.750 1.4968 0.01970 0.01289 -0.1035 0.0017 1.0000
10.000 1.5107 0.02030 0.01354 -0.1013 0.0017 1.0000
10.250 1.5242 0.02094 0.01422 -0.0992 0.0016 1.0000
10.500 1.5370 0.02163 0.01498 -0.0971 0.0016 1.0000
10.750 1.5491 0.02239 0.01579 -0.0951 0.0016 1.0000
11.000 1.5603 0.02323 0.01670 -0.0930 0.0015 1.0000
11.250 1.5708 0.02415 0.01767 -0.0910 0.0014 1.0000
11.500 1.5802 0.02519 0.01878 -0.0890 0.0014 1.0000
11.750 1.5891 0.02632 0.01998 -0.0871 0.0014 1.0000
12.000 1.5971 0.02758 0.02132 -0.0852 0.0013 1.0000
12.250 1.6046 0.02893 0.02275 -0.0835 0.0013 1.0000
12.500 1.6111 0.03044 0.02434 -0.0819 0.0013 1.0000
12.750 1.6168 0.03209 0.02607 -0.0803 0.0012 1.0000
13.000 1.6216 0.03388 0.02794 -0.0789 0.0012 1.0000
13.250 1.6254 0.03585 0.03000 -0.0776 0.0012 1.0000
13.500 1.6278 0.03803 0.03227 -0.0764 0.0012 1.0000
13.750 1.6295 0.04037 0.03471 -0.0754 0.0011 1.0000
14.000 1.6296 0.04301 0.03744 -0.0746 0.0011 1.0000
14.250 1.6280 0.04593 0.04048 -0.0740 0.0011 1.0000
14.500 1.6248 0.04917 0.04384 -0.0736 0.0011 1.0000
14.750 1.6190 0.05292 0.04771 -0.0735 0.0010 1.0000
15.000 1.6099 0.05729 0.05222 -0.0738 0.0010 1.0000
15.250 1.5998 0.06206 0.05713 -0.0745 0.0010 1.0000
15.500 1.5971 0.06596 0.06113 -0.0752 0.0010 1.0000
15.750 1.5954 0.06984 0.06512 -0.0761 0.0010 1.0000
16.000 1.5901 0.07440 0.06979 -0.0774 0.0009 1.0000
16.250 1.5848 0.07913 0.07463 -0.0789 0.0009 1.0000
16.500 1.5777 0.08432 0.07994 -0.0807 0.0009 1.0000
16.750 1.5697 0.08977 0.08551 -0.0827 0.0009 1.0000
17.000 1.5597 0.09575 0.09161 -0.0852 0.0009 1.0000
17.250 1.5484 0.10213 0.09812 -0.0879 0.0009 1.0000
17.500 1.5364 0.10880 0.10492 -0.0910 0.0009 1.0000
17.750 1.5254 0.11537 0.11162 -0.0942 0.0008 1.0000
18.000 1.5119 0.12259 0.11898 -0.0978 0.0008 1.0000
18.250 1.4978 0.13009 0.12661 -0.1018 0.0008 1.0000
18.500 1.4827 0.13788 0.13453 -0.1061 0.0008 1.0000
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