GOE 646 AIRFOIL (goe646-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 646 AIRFOIL (goe646-il) Reynolds number: 1,000,000 Max Cl/Cd: 105.19 at α=5.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe646-il-1000000.txt Download as CSV file: xf-goe646-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: GOE 646 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
------ -------- --------- --------- -------- -------- --------
-18.750 -0.8802 0.09161 0.08823 -0.0794 1.0000 0.0342
-18.500 -0.8848 0.08808 0.08467 -0.0808 1.0000 0.0345
-18.250 -0.8920 0.08425 0.08079 -0.0823 1.0000 0.0347
-18.000 -0.8969 0.08079 0.07729 -0.0836 1.0000 0.0351
-17.750 -0.9051 0.07701 0.07346 -0.0850 1.0000 0.0352
-17.500 -0.9117 0.07351 0.06991 -0.0861 1.0000 0.0356
-17.250 -0.9217 0.06964 0.06597 -0.0875 1.0000 0.0359
-17.000 -0.9293 0.06626 0.06255 -0.0884 1.0000 0.0361
-16.750 -0.9411 0.06253 0.05876 -0.0894 1.0000 0.0363
-16.500 -0.9560 0.05879 0.05495 -0.0901 1.0000 0.0364
-16.250 -0.9713 0.05536 0.05146 -0.0904 1.0000 0.0366
-16.000 -0.9804 0.05034 0.04636 -0.0949 0.9989 0.0369
-15.750 -0.9854 0.04497 0.04092 -0.1007 0.9968 0.0374
-15.500 -0.9858 0.03987 0.03572 -0.1069 0.9943 0.0378
-15.250 -0.9785 0.03545 0.03122 -0.1129 0.9921 0.0382
-15.000 -0.9733 0.03139 0.02707 -0.1176 0.9875 0.0387
-14.750 -0.9581 0.02812 0.02371 -0.1227 0.9839 0.0392
-14.500 -0.9367 0.02536 0.02086 -0.1280 0.9814 0.0398
-14.250 -0.9210 0.02299 0.01839 -0.1314 0.9747 0.0404
-14.000 -0.8981 0.02111 0.01642 -0.1352 0.9694 0.0409
-13.750 -0.8868 0.01956 0.01477 -0.1358 0.9604 0.0416
-13.500 -0.8649 0.01836 0.01354 -0.1369 0.9542 0.0427
-13.250 -0.8382 0.01750 0.01264 -0.1382 0.9478 0.0438
-13.000 -0.8053 0.01679 0.01188 -0.1403 0.9423 0.0449
-12.750 -0.7650 0.01610 0.01112 -0.1438 0.9387 0.0461
-12.500 -0.7331 0.01530 0.01029 -0.1459 0.9315 0.0481
-12.250 -0.6998 0.01475 0.00969 -0.1478 0.9251 0.0499
-12.000 -0.6686 0.01426 0.00914 -0.1491 0.9184 0.0518
-11.750 -0.6448 0.01378 0.00864 -0.1490 0.9102 0.0540
-11.250 -0.5971 0.01307 0.00786 -0.1482 0.8961 0.0594
-11.000 -0.5728 0.01280 0.00755 -0.1478 0.8898 0.0623
-10.750 -0.5486 0.01247 0.00719 -0.1474 0.8840 0.0653
-10.500 -0.5272 0.01223 0.00694 -0.1462 0.8785 0.0682
-10.250 -0.5038 0.01198 0.00665 -0.1455 0.8728 0.0709
-10.000 -0.4791 0.01172 0.00636 -0.1451 0.8670 0.0739
-9.750 -0.4552 0.01155 0.00615 -0.1443 0.8619 0.0764
-9.500 -0.4327 0.01127 0.00587 -0.1433 0.8564 0.0792
-9.250 -0.4082 0.01104 0.00562 -0.1427 0.8510 0.0822
-9.000 -0.3818 0.01090 0.00542 -0.1424 0.8457 0.0846
-8.750 -0.3593 0.01061 0.00515 -0.1414 0.8408 0.0879
-8.500 -0.3349 0.01040 0.00492 -0.1407 0.8353 0.0910
-8.250 -0.3091 0.01025 0.00472 -0.1402 0.8298 0.0936
-8.000 -0.2848 0.01000 0.00447 -0.1396 0.8244 0.0980
-7.750 -0.2602 0.00981 0.00428 -0.1389 0.8184 0.1020
-7.500 -0.2355 0.00959 0.00406 -0.1382 0.8119 0.1075
-7.000 -0.1859 0.00919 0.00368 -0.1368 0.7988 0.1220
-6.750 -0.1611 0.00900 0.00349 -0.1361 0.7916 0.1315
-6.500 -0.1360 0.00882 0.00333 -0.1355 0.7846 0.1415
-6.250 -0.1110 0.00866 0.00318 -0.1348 0.7763 0.1517
-6.000 -0.0860 0.00854 0.00304 -0.1341 0.7677 0.1615
-5.750 -0.0611 0.00837 0.00291 -0.1334 0.7583 0.1724
-5.500 -0.0367 0.00827 0.00279 -0.1326 0.7479 0.1830
-5.250 -0.0116 0.00818 0.00269 -0.1318 0.7360 0.1922
-5.000 0.0125 0.00809 0.00259 -0.1309 0.7229 0.2019
-4.750 0.0364 0.00806 0.00251 -0.1299 0.7079 0.2098
-4.500 0.0596 0.00803 0.00244 -0.1288 0.6919 0.2191
-4.250 0.0840 0.00802 0.00238 -0.1279 0.6769 0.2261
-4.000 0.1081 0.00800 0.00233 -0.1269 0.6633 0.2350
-3.750 0.1322 0.00804 0.00230 -0.1260 0.6502 0.2418
-3.500 0.1562 0.00803 0.00227 -0.1250 0.6379 0.2501
-3.250 0.1813 0.00805 0.00226 -0.1243 0.6274 0.2569
-3.000 0.2056 0.00809 0.00224 -0.1234 0.6169 0.2629
-2.750 0.2312 0.00807 0.00223 -0.1228 0.6088 0.2703
-2.500 0.2566 0.00811 0.00222 -0.1221 0.6009 0.2763
-2.250 0.2816 0.00813 0.00222 -0.1213 0.5936 0.2824
-2.000 0.3079 0.00812 0.00222 -0.1208 0.5875 0.2892
-1.750 0.3334 0.00816 0.00222 -0.1201 0.5812 0.2953
-1.500 0.3581 0.00819 0.00223 -0.1193 0.5749 0.3020
-1.250 0.3846 0.00817 0.00224 -0.1189 0.5697 0.3088
-1.000 0.4104 0.00821 0.00225 -0.1183 0.5639 0.3145
-0.750 0.4348 0.00825 0.00227 -0.1174 0.5581 0.3203
-0.500 0.4606 0.00825 0.00229 -0.1168 0.5541 0.3268
-0.250 0.4870 0.00825 0.00230 -0.1163 0.5503 0.3321
0.000 0.5130 0.00829 0.00232 -0.1158 0.5460 0.3361
0.250 0.5373 0.00831 0.00234 -0.1149 0.5413 0.3433
0.500 0.5609 0.00836 0.00239 -0.1139 0.5362 0.3494
0.750 0.5865 0.00836 0.00241 -0.1132 0.5329 0.3546
1.000 0.6112 0.00837 0.00243 -0.1124 0.5290 0.3607
1.250 0.6347 0.00838 0.00246 -0.1114 0.5249 0.3679
1.500 0.6575 0.00844 0.00250 -0.1102 0.5204 0.3744
1.750 0.6810 0.00848 0.00255 -0.1092 0.5158 0.3814
2.000 0.7057 0.00847 0.00259 -0.1084 0.5116 0.3905
2.250 0.7291 0.00851 0.00263 -0.1073 0.5058 0.3975
2.500 0.7506 0.00858 0.00270 -0.1059 0.5000 0.4070
2.750 0.7743 0.00862 0.00276 -0.1050 0.4945 0.4168
3.000 0.7974 0.00865 0.00283 -0.1039 0.4883 0.4282
3.250 0.8186 0.00874 0.00292 -0.1024 0.4819 0.4406
3.500 0.8412 0.00878 0.00302 -0.1013 0.4766 0.4582
3.750 0.8645 0.00880 0.00312 -0.1003 0.4709 0.4821
4.000 0.8853 0.00886 0.00324 -0.0988 0.4641 0.5132
4.250 0.9065 0.00890 0.00338 -0.0974 0.4575 0.5508
4.500 0.9277 0.00896 0.00352 -0.0960 0.4494 0.5870
4.750 0.9464 0.00909 0.00369 -0.0942 0.4403 0.6170
5.000 0.9668 0.00920 0.00383 -0.0926 0.4293 0.6401
5.250 0.9856 0.00937 0.00400 -0.0909 0.4167 0.6592
5.500 1.0026 0.00960 0.00420 -0.0887 0.4016 0.6759
5.750 1.0176 0.00988 0.00443 -0.0863 0.3837 0.6923
6.000 1.0310 0.01020 0.00471 -0.0836 0.3636 0.7101
6.250 1.0445 0.01051 0.00501 -0.0810 0.3478 0.7314
6.500 1.0562 0.01077 0.00533 -0.0780 0.3352 0.7713
6.750 1.1349 0.01100 0.00589 -0.0894 0.3169 1.0000
7.000 1.1555 0.01127 0.00614 -0.0882 0.3099 1.0000
7.250 1.1736 0.01165 0.00646 -0.0866 0.3017 1.0000
7.500 1.1942 0.01194 0.00674 -0.0855 0.2959 1.0000
7.750 1.2144 0.01226 0.00705 -0.0843 0.2901 1.0000
8.000 1.2324 0.01269 0.00742 -0.0828 0.2830 1.0000
8.250 1.2534 0.01299 0.00773 -0.0819 0.2780 1.0000
8.500 1.2724 0.01340 0.00811 -0.0806 0.2705 1.0000
8.750 1.2904 0.01386 0.00853 -0.0793 0.2637 1.0000
9.000 1.3111 0.01421 0.00889 -0.0784 0.2584 1.0000
9.250 1.3292 0.01469 0.00934 -0.0772 0.2518 1.0000
9.500 1.3474 0.01518 0.00982 -0.0760 0.2460 1.0000
9.750 1.3664 0.01563 0.01027 -0.0749 0.2398 1.0000
10.000 1.3820 0.01627 0.01087 -0.0735 0.2317 1.0000
10.250 1.4004 0.01677 0.01137 -0.0725 0.2259 1.0000
10.500 1.4160 0.01743 0.01200 -0.0711 0.2187 1.0000
10.750 1.4317 0.01809 0.01265 -0.0698 0.2117 1.0000
11.000 1.4460 0.01885 0.01338 -0.0684 0.2038 1.0000
11.250 1.4606 0.01961 0.01413 -0.0671 0.1976 1.0000
11.500 1.4746 0.02041 0.01491 -0.0658 0.1913 1.0000
11.750 1.4863 0.02136 0.01584 -0.0642 0.1844 1.0000
12.000 1.5001 0.02222 0.01670 -0.0630 0.1789 1.0000
12.250 1.5098 0.02335 0.01780 -0.0614 0.1717 1.0000
12.500 1.5228 0.02428 0.01875 -0.0602 0.1672 1.0000
12.750 1.5331 0.02542 0.01988 -0.0588 0.1613 1.0000
13.000 1.5428 0.02663 0.02109 -0.0575 0.1561 1.0000
13.250 1.5544 0.02774 0.02221 -0.0563 0.1511 1.0000
13.500 1.5606 0.02926 0.02371 -0.0549 0.1447 1.0000
13.750 1.5709 0.03051 0.02499 -0.0538 0.1393 1.0000
14.000 1.5752 0.03225 0.02670 -0.0523 0.1311 1.0000
14.250 1.5780 0.03419 0.02859 -0.0510 0.1205 1.0000
14.500 1.5747 0.03666 0.03100 -0.0494 0.1049 1.0000
15.000 1.5622 0.04244 0.03667 -0.0465 0.0835 1.0000
15.250 1.5628 0.04487 0.03912 -0.0456 0.0797 1.0000
15.500 1.5635 0.04730 0.04158 -0.0448 0.0772 1.0000
15.750 1.5622 0.05000 0.04430 -0.0441 0.0745 1.0000
16.000 1.5650 0.05234 0.04669 -0.0435 0.0730 1.0000
16.250 1.5678 0.05470 0.04912 -0.0431 0.0717 1.0000
16.500 1.5699 0.05713 0.05160 -0.0426 0.0705 1.0000
16.750 1.5682 0.06002 0.05454 -0.0422 0.0689 1.0000
17.000 1.5658 0.06304 0.05761 -0.0419 0.0678 1.0000
17.250 1.5606 0.06639 0.06101 -0.0417 0.0664 1.0000
17.500 1.5633 0.06889 0.06358 -0.0415 0.0657 1.0000
17.750 1.5653 0.07148 0.06624 -0.0414 0.0650 1.0000
18.000 1.5659 0.07426 0.06908 -0.0414 0.0640 1.0000
18.250 1.5642 0.07734 0.07222 -0.0414 0.0631 1.0000
18.500 1.5621 0.08048 0.07541 -0.0415 0.0622 1.0000
18.750 1.5568 0.08404 0.07903 -0.0417 0.0615 1.0000
19.000 1.5497 0.08785 0.08290 -0.0420 0.0603 1.0000
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