GOE 13K AIRFOIL (goe13k-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 13K AIRFOIL (goe13k-il) Reynolds number: 1,000,000 Max Cl/Cd: 93.89 at α=3.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe13k-il-1000000-n5.txt Download as CSV file: xf-goe13k-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 13K 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
------ -------- --------- --------- -------- -------- --------
-17.250 -0.8354 0.03301 0.02971 -0.2006 0.9384 0.0321
-17.000 -0.8322 0.03065 0.02724 -0.2021 0.9357 0.0324
-16.750 -0.8190 0.02909 0.02562 -0.2035 0.9339 0.0328
-16.500 -0.8016 0.02783 0.02429 -0.2049 0.9327 0.0331
-16.250 -0.7867 0.02720 0.02362 -0.2046 0.9291 0.0337
-16.000 -0.7805 0.02563 0.02192 -0.2044 0.9256 0.0338
-15.750 -0.7587 0.02492 0.02114 -0.2052 0.9234 0.0344
-15.500 -0.7381 0.02397 0.02009 -0.2061 0.9214 0.0347
-15.250 -0.7123 0.02325 0.01928 -0.2076 0.9198 0.0353
-15.000 -0.6986 0.02235 0.01826 -0.2069 0.9163 0.0356
-14.750 -0.6823 0.02166 0.01746 -0.2062 0.9128 0.0358
-14.500 -0.6608 0.02110 0.01680 -0.2063 0.9099 0.0361
-14.250 -0.6402 0.02036 0.01595 -0.2065 0.9071 0.0365
-14.000 -0.6173 0.01972 0.01523 -0.2069 0.9046 0.0368
-13.750 -0.6076 0.01963 0.01512 -0.2038 0.9007 0.0372
-13.500 -0.5991 0.01916 0.01458 -0.2009 0.8966 0.0374
-13.250 -0.5770 0.01912 0.01452 -0.2002 0.8939 0.0378
-13.000 -0.5574 0.01877 0.01410 -0.1993 0.8911 0.0380
-12.750 -0.5326 0.01857 0.01385 -0.1993 0.8888 0.0384
-12.500 -0.5373 0.01835 0.01359 -0.1931 0.8849 0.0385
-12.250 -0.5257 0.01819 0.01340 -0.1901 0.8817 0.0389
-12.000 -0.5111 0.01784 0.01298 -0.1879 0.8787 0.0392
-11.750 -0.4938 0.01738 0.01243 -0.1864 0.8761 0.0394
-11.500 -0.4731 0.01694 0.01191 -0.1855 0.8739 0.0397
-11.250 -0.4518 0.01654 0.01143 -0.1847 0.8718 0.0400
-11.000 -0.4457 0.01629 0.01113 -0.1805 0.8691 0.0403
-10.750 -0.4360 0.01598 0.01077 -0.1770 0.8662 0.0405
-10.500 -0.4216 0.01566 0.01038 -0.1745 0.8633 0.0407
-10.250 -0.4046 0.01527 0.00991 -0.1727 0.8607 0.0408
-10.000 -0.3838 0.01492 0.00948 -0.1715 0.8585 0.0410
-9.750 -0.3600 0.01460 0.00909 -0.1710 0.8565 0.0413
-9.500 -0.3422 0.01437 0.00880 -0.1692 0.8544 0.0414
-9.250 -0.3331 0.01421 0.00861 -0.1653 0.8518 0.0415
-9.000 -0.3221 0.01380 0.00815 -0.1620 0.8491 0.0418
-8.750 -0.3069 0.01341 0.00770 -0.1596 0.8465 0.0421
-8.500 -0.2882 0.01309 0.00735 -0.1579 0.8441 0.0424
-8.250 -0.2669 0.01280 0.00701 -0.1567 0.8419 0.0426
-8.000 -0.2424 0.01256 0.00672 -0.1562 0.8397 0.0429
-7.750 -0.2260 0.01235 0.00649 -0.1539 0.8374 0.0431
-7.500 -0.2119 0.01220 0.00633 -0.1511 0.8348 0.0434
-7.250 -0.1952 0.01205 0.00615 -0.1488 0.8322 0.0437
-7.000 -0.1762 0.01187 0.00595 -0.1470 0.8297 0.0439
-6.750 -0.1555 0.01168 0.00572 -0.1456 0.8273 0.0442
-6.500 -0.1331 0.01148 0.00548 -0.1445 0.8252 0.0445
-6.250 -0.1084 0.01128 0.00524 -0.1440 0.8232 0.0448
-6.000 -0.0931 0.01115 0.00510 -0.1413 0.8208 0.0451
-5.750 -0.0782 0.01105 0.00498 -0.1385 0.8182 0.0455
-5.500 -0.0602 0.01094 0.00485 -0.1365 0.8156 0.0458
-5.250 -0.0402 0.01081 0.00470 -0.1348 0.8130 0.0461
-5.000 -0.0192 0.01064 0.00449 -0.1334 0.8102 0.0464
-4.750 0.0045 0.01048 0.00429 -0.1326 0.8075 0.0465
-4.500 0.0207 0.01040 0.00419 -0.1301 0.8042 0.0469
-4.250 0.0370 0.01030 0.00408 -0.1276 0.8007 0.0471
-4.000 0.0558 0.01022 0.00397 -0.1256 0.7973 0.0474
-3.750 0.0764 0.01012 0.00385 -0.1241 0.7945 0.0475
-3.500 0.0990 0.01001 0.00370 -0.1230 0.7916 0.0477
-3.250 0.1142 0.00990 0.00359 -0.1202 0.7883 0.0481
-3.000 0.1318 0.00978 0.00347 -0.1180 0.7854 0.0487
-2.750 0.1517 0.00968 0.00336 -0.1163 0.7828 0.0492
-2.500 0.1729 0.00960 0.00328 -0.1149 0.7803 0.0497
-2.250 0.1952 0.00953 0.00319 -0.1138 0.7775 0.0503
-2.000 0.2182 0.00947 0.00312 -0.1128 0.7750 0.0509
-1.750 0.2368 0.00944 0.00310 -0.1108 0.7722 0.0514
-1.500 0.2549 0.00941 0.00307 -0.1087 0.7686 0.0520
-1.250 0.2753 0.00938 0.00305 -0.1071 0.7660 0.0527
-1.000 0.2969 0.00935 0.00301 -0.1058 0.7634 0.0532
-0.750 0.3200 0.00932 0.00296 -0.1048 0.7610 0.0540
-0.500 0.3420 0.00930 0.00294 -0.1036 0.7586 0.0543
-0.250 0.3619 0.00930 0.00296 -0.1019 0.7560 0.0547
0.000 0.3807 0.00929 0.00296 -0.1000 0.7518 0.0556
0.250 0.4030 0.00927 0.00295 -0.0989 0.7493 0.0568
0.500 0.4259 0.00926 0.00294 -0.0979 0.7465 0.0580
0.750 0.4496 0.00925 0.00293 -0.0971 0.7436 0.0599
1.000 0.4701 0.00927 0.00298 -0.0956 0.7413 0.0614
1.250 0.4905 0.00931 0.00305 -0.0941 0.7385 0.0625
1.500 0.5116 0.00934 0.00310 -0.0927 0.7352 0.0654
1.750 0.5341 0.00935 0.00314 -0.0917 0.7321 0.0704
2.000 0.5574 0.00935 0.00318 -0.0908 0.7281 0.0833
2.250 0.5815 0.00931 0.00329 -0.0903 0.7252 0.1277
2.500 0.6037 0.00934 0.00341 -0.0893 0.7214 0.1457
2.750 0.6267 0.00939 0.00351 -0.0884 0.7177 0.1611
3.000 0.6495 0.00944 0.00360 -0.0876 0.7132 0.1807
3.500 0.9164 0.00976 0.00586 -0.1383 0.6458 0.9970
3.750 0.8878 0.01181 0.00741 -0.1275 0.5370 1.0000
4.000 0.8555 0.01362 0.00882 -0.1159 0.4584 1.0000
4.250 0.8566 0.01448 0.00951 -0.1110 0.4249 1.0000
4.500 0.8644 0.01513 0.01006 -0.1074 0.4047 1.0000
4.750 0.8758 0.01568 0.01052 -0.1046 0.3865 1.0000
5.000 0.8940 0.01599 0.01082 -0.1030 0.3817 1.0000
5.250 0.9101 0.01640 0.01120 -0.1010 0.3716 1.0000
5.500 0.9251 0.01685 0.01161 -0.0989 0.3621 1.0000
5.750 0.9418 0.01725 0.01198 -0.0971 0.3525 1.0000
6.000 0.9581 0.01767 0.01236 -0.0952 0.3433 1.0000
6.250 0.9728 0.01817 0.01281 -0.0931 0.3295 1.0000
6.500 0.9857 0.01876 0.01333 -0.0908 0.3122 1.0000
6.750 0.9983 0.01937 0.01385 -0.0884 0.2922 1.0000
7.000 1.0072 0.02015 0.01448 -0.0854 0.2620 1.0000
7.500 1.0231 0.02190 0.01590 -0.0794 0.1993 1.0000
7.750 1.0347 0.02262 0.01650 -0.0771 0.1750 1.0000
8.000 1.0479 0.02328 0.01705 -0.0750 0.1555 1.0000
8.250 1.0623 0.02389 0.01760 -0.0732 0.1413 1.0000
8.500 1.0765 0.02453 0.01817 -0.0713 0.1281 1.0000
8.750 1.0915 0.02514 0.01872 -0.0696 0.1172 1.0000
9.000 1.1078 0.02568 0.01923 -0.0681 0.1103 1.0000
9.250 1.1239 0.02624 0.01976 -0.0666 0.1023 1.0000
9.500 1.1401 0.02680 0.02029 -0.0652 0.0974 1.0000
9.750 1.1561 0.02738 0.02086 -0.0638 0.0926 1.0000
10.000 1.1718 0.02798 0.02144 -0.0623 0.0874 1.0000
10.250 1.1876 0.02858 0.02203 -0.0608 0.0832 1.0000
10.500 1.2041 0.02914 0.02258 -0.0596 0.0795 1.0000
10.750 1.2192 0.02978 0.02320 -0.0581 0.0749 1.0000
11.000 1.2346 0.03043 0.02385 -0.0567 0.0723 1.0000
11.250 1.2500 0.03108 0.02450 -0.0553 0.0688 1.0000
11.500 1.2655 0.03173 0.02515 -0.0540 0.0667 1.0000
11.750 1.2806 0.03240 0.02582 -0.0526 0.0646 1.0000
12.000 1.2961 0.03306 0.02650 -0.0513 0.0628 1.0000
12.250 1.3108 0.03375 0.02722 -0.0500 0.0612 1.0000
12.500 1.3253 0.03448 0.02797 -0.0486 0.0589 1.0000
12.750 1.3396 0.03523 0.02872 -0.0472 0.0573 1.0000
13.000 1.3535 0.03601 0.02951 -0.0459 0.0553 1.0000
13.250 1.3675 0.03678 0.03032 -0.0445 0.0538 1.0000
13.500 1.3810 0.03760 0.03117 -0.0432 0.0522 1.0000
13.750 1.3943 0.03844 0.03202 -0.0419 0.0502 1.0000
14.000 1.4068 0.03935 0.03293 -0.0405 0.0484 1.0000
14.250 1.4194 0.04025 0.03387 -0.0391 0.0463 1.0000
14.500 1.4312 0.04121 0.03484 -0.0377 0.0442 1.0000
14.750 1.4420 0.04225 0.03588 -0.0363 0.0412 1.0000
15.000 1.4534 0.04326 0.03691 -0.0349 0.0387 1.0000
15.250 1.4624 0.04447 0.03813 -0.0334 0.0360 1.0000
15.500 1.4724 0.04561 0.03930 -0.0319 0.0335 1.0000
15.750 1.4811 0.04687 0.04056 -0.0305 0.0311 1.0000
16.000 1.4886 0.04824 0.04196 -0.0289 0.0287 1.0000
16.250 1.4964 0.04960 0.04334 -0.0275 0.0270 1.0000
16.500 1.5036 0.05102 0.04479 -0.0260 0.0255 1.0000
16.750 1.5101 0.05253 0.04634 -0.0246 0.0240 1.0000
17.000 1.5164 0.05406 0.04791 -0.0232 0.0228 1.0000
17.250 1.5216 0.05573 0.04962 -0.0218 0.0219 1.0000
17.500 1.5281 0.05731 0.05125 -0.0206 0.0211 1.0000
17.750 1.5323 0.05911 0.05310 -0.0192 0.0197 1.0000
18.000 1.5348 0.06111 0.05514 -0.0179 0.0187 1.0000
18.250 1.5393 0.06294 0.05703 -0.0168 0.0185 1.0000
18.500 1.5427 0.06490 0.05905 -0.0157 0.0175 1.0000
18.750 1.5463 0.06687 0.06108 -0.0147 0.0173 1.0000
19.000 1.5478 0.06910 0.06338 -0.0137 0.0166 1.0000
19.250 1.5481 0.07149 0.06583 -0.0127 0.0160 1.0000
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