FX 60-177 AIRFOIL (fx60177-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: FX 60-177 AIRFOIL (fx60177-il) Reynolds number: 1,000,000 Max Cl/Cd: 105.52 at α=1.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx60177-il-1000000.txt Download as CSV file: xf-fx60177-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: FX 60-177 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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-18.000 -0.6979 0.12361 0.12136 -0.0562 1.0001 0.0053
-17.750 -0.7341 0.11247 0.11006 -0.0612 1.0001 0.0052
-17.500 -0.7632 0.10326 0.10070 -0.0654 1.0001 0.0052
-17.250 -0.7847 0.09418 0.09146 -0.0710 0.9997 0.0052
-17.000 -0.8025 0.08615 0.08326 -0.0761 0.9993 0.0051
-16.750 -0.8165 0.07900 0.07594 -0.0808 0.9987 0.0051
-16.500 -0.8275 0.07265 0.06943 -0.0849 0.9980 0.0051
-16.250 -0.8354 0.06697 0.06360 -0.0886 0.9972 0.0050
-16.000 -0.8404 0.06198 0.05845 -0.0919 0.9965 0.0050
-15.750 -0.8430 0.05746 0.05378 -0.0948 0.9957 0.0050
-15.500 -0.8417 0.05352 0.04970 -0.0975 0.9950 0.0050
-15.250 -0.8386 0.04993 0.04598 -0.0999 0.9944 0.0050
-15.000 -0.8338 0.04688 0.04281 -0.1017 0.9933 0.0050
-14.750 -0.8286 0.04413 0.03994 -0.1029 0.9914 0.0050
-14.500 -0.8206 0.04159 0.03729 -0.1042 0.9898 0.0050
-14.250 -0.8099 0.03929 0.03489 -0.1057 0.9884 0.0050
-14.000 -0.7976 0.03717 0.03267 -0.1071 0.9872 0.0051
-13.750 -0.7836 0.03520 0.03060 -0.1086 0.9862 0.0051
-13.500 -0.7679 0.03335 0.02866 -0.1101 0.9853 0.0051
-13.250 -0.7509 0.03163 0.02685 -0.1116 0.9846 0.0051
-13.000 -0.7328 0.02997 0.02511 -0.1132 0.9839 0.0051
-12.750 -0.7235 0.02859 0.02366 -0.1125 0.9799 0.0051
-12.500 -0.7075 0.02719 0.02218 -0.1131 0.9776 0.0051
-12.250 -0.6882 0.02585 0.02077 -0.1142 0.9761 0.0051
-12.000 -0.6668 0.02457 0.01942 -0.1156 0.9749 0.0052
-11.750 -0.6434 0.02337 0.01815 -0.1171 0.9740 0.0052
-11.500 -0.6193 0.02222 0.01695 -0.1187 0.9731 0.0052
-11.250 -0.5946 0.02120 0.01587 -0.1202 0.9722 0.0052
-11.000 -0.5804 0.02037 0.01499 -0.1193 0.9678 0.0052
-10.750 -0.5605 0.01955 0.01413 -0.1193 0.9646 0.0052
-10.500 -0.5373 0.01871 0.01324 -0.1200 0.9623 0.0053
-10.250 -0.5131 0.01794 0.01242 -0.1208 0.9603 0.0053
-10.000 -0.4882 0.01723 0.01167 -0.1216 0.9583 0.0054
-9.750 -0.4747 0.01671 0.01111 -0.1199 0.9529 0.0054
-9.500 -0.4529 0.01611 0.01048 -0.1199 0.9494 0.0055
-9.250 -0.4290 0.01554 0.00987 -0.1202 0.9466 0.0055
-9.000 -0.4052 0.01502 0.00931 -0.1204 0.9435 0.0056
-8.750 -0.3894 0.01457 0.00884 -0.1190 0.9382 0.0058
-8.500 -0.3673 0.01410 0.00834 -0.1187 0.9345 0.0060
-8.250 -0.3433 0.01365 0.00787 -0.1189 0.9315 0.0064
-8.000 -0.3219 0.01329 0.00749 -0.1184 0.9278 0.0069
-7.750 -0.3054 0.01297 0.00716 -0.1169 0.9229 0.0079
-7.500 -0.2817 0.01257 0.00676 -0.1169 0.9194 0.0107
-7.250 -0.2555 0.01217 0.00635 -0.1174 0.9165 0.0145
-7.000 -0.2315 0.01181 0.00601 -0.1175 0.9129 0.0194
-6.750 -0.2098 0.01140 0.00566 -0.1172 0.9086 0.0301
-6.500 -0.1836 0.01100 0.00531 -0.1177 0.9051 0.0410
-6.250 -0.1543 0.01063 0.00497 -0.1188 0.9021 0.0530
-6.000 -0.1288 0.01010 0.00459 -0.1195 0.8982 0.0851
-5.750 -0.1051 0.00962 0.00427 -0.1196 0.8937 0.1216
-5.500 -0.0778 0.00905 0.00389 -0.1205 0.8897 0.1725
-5.250 -0.0468 0.00828 0.00345 -0.1226 0.8861 0.2552
-5.000 -0.0184 0.00752 0.00306 -0.1241 0.8819 0.3496
-4.750 0.0140 0.00690 0.00274 -0.1261 0.8780 0.4299
-4.500 0.0498 0.00638 0.00246 -0.1287 0.8743 0.5030
-4.250 0.0868 0.00610 0.00230 -0.1311 0.8704 0.5513
-4.000 0.1164 0.00596 0.00224 -0.1317 0.8653 0.5767
-3.750 0.1482 0.00587 0.00221 -0.1327 0.8606 0.6064
-3.500 0.1812 0.00586 0.00219 -0.1339 0.8565 0.6247
-3.250 0.2111 0.00586 0.00216 -0.1344 0.8516 0.6327
-3.000 0.2402 0.00585 0.00215 -0.1347 0.8460 0.6399
-2.750 0.2720 0.00587 0.00210 -0.1356 0.8410 0.6466
-2.500 0.3008 0.00589 0.00214 -0.1359 0.8358 0.6527
-2.250 0.3302 0.00591 0.00213 -0.1363 0.8300 0.6581
-2.000 0.3609 0.00593 0.00208 -0.1370 0.8234 0.6620
-1.750 0.3882 0.00593 0.00209 -0.1369 0.8149 0.6654
-1.500 0.4175 0.00598 0.00209 -0.1372 0.8076 0.6687
-1.250 0.4463 0.00601 0.00211 -0.1375 0.8006 0.6728
-1.000 0.4764 0.00607 0.00211 -0.1381 0.7941 0.6764
-0.750 0.5045 0.00608 0.00214 -0.1382 0.7870 0.6796
-0.500 0.5327 0.00614 0.00217 -0.1383 0.7788 0.6824
-0.250 0.5603 0.00619 0.00221 -0.1384 0.7692 0.6855
0.000 0.5882 0.00627 0.00224 -0.1384 0.7592 0.6888
0.250 0.6160 0.00636 0.00227 -0.1385 0.7480 0.6916
0.500 0.6429 0.00642 0.00230 -0.1384 0.7350 0.6942
0.750 0.6682 0.00652 0.00236 -0.1379 0.7190 0.6967
1.000 0.6921 0.00666 0.00244 -0.1372 0.6998 0.6991
1.250 0.7161 0.00683 0.00253 -0.1364 0.6793 0.7019
1.500 0.7397 0.00701 0.00263 -0.1356 0.6574 0.7047
1.750 0.7627 0.00723 0.00274 -0.1347 0.6339 0.7071
2.000 0.7850 0.00746 0.00285 -0.1337 0.6085 0.7092
2.250 0.8063 0.00768 0.00300 -0.1325 0.5842 0.7115
2.500 0.8254 0.00796 0.00318 -0.1308 0.5562 0.7136
2.750 0.8450 0.00825 0.00336 -0.1293 0.5305 0.7158
3.000 0.8645 0.00857 0.00356 -0.1278 0.5026 0.7180
3.250 0.8847 0.00890 0.00377 -0.1264 0.4765 0.7202
3.500 0.9078 0.00918 0.00397 -0.1257 0.4551 0.7222
3.750 0.9303 0.00951 0.00418 -0.1249 0.4299 0.7240
4.000 0.9517 0.00985 0.00442 -0.1239 0.4054 0.7262
4.250 0.9724 0.01021 0.00469 -0.1227 0.3800 0.7282
4.500 0.9932 0.01058 0.00496 -0.1216 0.3573 0.7302
4.750 1.0152 0.01090 0.00523 -0.1207 0.3408 0.7322
5.000 1.0375 0.01122 0.00548 -0.1199 0.3243 0.7340
5.250 1.0592 0.01158 0.00576 -0.1191 0.3048 0.7359
5.500 1.0802 0.01196 0.00606 -0.1181 0.2868 0.7377
5.750 1.1017 0.01233 0.00635 -0.1172 0.2707 0.7393
6.000 1.1236 0.01266 0.00663 -0.1164 0.2565 0.7410
6.250 1.1448 0.01301 0.00695 -0.1155 0.2432 0.7428
6.500 1.1651 0.01340 0.00729 -0.1144 0.2300 0.7444
6.750 1.1849 0.01381 0.00766 -0.1133 0.2176 0.7462
7.000 1.2047 0.01424 0.00803 -0.1122 0.2030 0.7481
7.250 1.2242 0.01469 0.00842 -0.1110 0.1891 0.7500
7.500 1.2439 0.01513 0.00882 -0.1099 0.1788 0.7519
7.750 1.2645 0.01554 0.00921 -0.1090 0.1712 0.7536
8.000 1.2836 0.01603 0.00966 -0.1079 0.1604 0.7551
8.250 1.3033 0.01648 0.01008 -0.1069 0.1489 0.7567
8.500 1.3203 0.01706 0.01059 -0.1055 0.1365 0.7586
8.750 1.3378 0.01761 0.01112 -0.1041 0.1266 0.7603
9.000 1.3544 0.01822 0.01169 -0.1026 0.1167 0.7622
9.250 1.3712 0.01881 0.01226 -0.1013 0.1063 0.7641
9.500 1.3859 0.01954 0.01293 -0.0996 0.0949 0.7661
9.750 1.4015 0.02025 0.01360 -0.0981 0.0851 0.7679
10.000 1.4153 0.02106 0.01436 -0.0964 0.0745 0.7696
10.250 1.4267 0.02205 0.01525 -0.0945 0.0615 0.7712
10.500 1.4398 0.02292 0.01609 -0.0928 0.0538 0.7729
10.750 1.4512 0.02391 0.01705 -0.0909 0.0443 0.7747
11.000 1.4594 0.02510 0.01818 -0.0887 0.0340 0.7763
11.250 1.4707 0.02612 0.01919 -0.0869 0.0287 0.7778
11.500 1.4796 0.02732 0.02037 -0.0850 0.0220 0.7794
11.750 1.4779 0.02929 0.02227 -0.0818 0.0090 0.7810
12.000 1.4811 0.03098 0.02398 -0.0793 0.0035 0.7827
12.250 1.4908 0.03224 0.02530 -0.0777 0.0030 0.7843
12.500 1.5015 0.03346 0.02658 -0.0764 0.0029 0.7859
12.750 1.5114 0.03477 0.02796 -0.0750 0.0028 0.7872
13.000 1.5195 0.03624 0.02951 -0.0735 0.0026 0.7887
13.250 1.5272 0.03777 0.03113 -0.0721 0.0025 0.7905
13.500 1.5332 0.03949 0.03294 -0.0706 0.0024 0.7920
13.750 1.5383 0.04133 0.03487 -0.0692 0.0024 0.7937
14.000 1.5420 0.04335 0.03700 -0.0678 0.0023 0.7953
14.250 1.5454 0.04547 0.03921 -0.0665 0.0022 0.7971
14.500 1.5496 0.04757 0.04140 -0.0655 0.0022 0.7987
14.750 1.5528 0.04984 0.04376 -0.0645 0.0022 0.8003
15.000 1.5551 0.05228 0.04629 -0.0637 0.0022 0.8017
15.250 1.5558 0.05497 0.04907 -0.0629 0.0021 0.8030
15.500 1.5558 0.05781 0.05200 -0.0624 0.0021 0.8044
15.750 1.5544 0.06087 0.05517 -0.0619 0.0020 0.8060
16.000 1.5515 0.06421 0.05862 -0.0617 0.0020 0.8074
16.250 1.5474 0.06779 0.06232 -0.0616 0.0020 0.8088
16.500 1.5424 0.07160 0.06624 -0.0617 0.0020 0.8101
16.750 1.5349 0.07583 0.07059 -0.0620 0.0019 0.8115
17.000 1.5261 0.08033 0.07522 -0.0626 0.0019 0.8128
17.250 1.5162 0.08512 0.08013 -0.0635 0.0019 0.8140
17.500 1.5052 0.09019 0.08532 -0.0647 0.0019 0.8153
17.750 1.4939 0.09541 0.09067 -0.0661 0.0019 0.8165
18.000 1.4798 0.10112 0.09651 -0.0678 0.0019 0.8175
18.250 1.4635 0.10732 0.10283 -0.0699 0.0018 0.8185
18.500 1.4479 0.11354 0.10919 -0.0722 0.0018 0.8195
18.750 1.4320 0.11991 0.11569 -0.0748 0.0018 0.8208
19.000 1.4155 0.12651 0.12243 -0.0777 0.0018 0.8220
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