GOE 646 AIRFOIL (goe646-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 646 AIRFOIL (goe646-il) Reynolds number: 1,000,000 Max Cl/Cd: 85.4 at α=6° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe646-il-1000000-n5.txt Download as CSV file: xf-goe646-il-1000000-n5.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 = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-18.250 -0.8848 0.08574 0.08221 -0.0811 1.0000 0.0304
-18.000 -0.8959 0.08143 0.07785 -0.0828 1.0000 0.0306
-17.750 -0.9079 0.07711 0.07347 -0.0845 1.0000 0.0309
-17.500 -0.9152 0.07233 0.06862 -0.0878 0.9996 0.0310
-17.250 -0.9186 0.06776 0.06398 -0.0915 0.9990 0.0314
-17.000 -0.9233 0.06304 0.05918 -0.0954 0.9982 0.0316
-16.750 -0.9297 0.05820 0.05424 -0.0996 0.9970 0.0317
-16.500 -0.9344 0.05358 0.04953 -0.1037 0.9955 0.0320
-16.250 -0.9388 0.04894 0.04480 -0.1081 0.9936 0.0321
-16.000 -0.9445 0.04445 0.04022 -0.1119 0.9911 0.0323
-15.750 -0.9519 0.03985 0.03552 -0.1156 0.9876 0.0325
-15.500 -0.9554 0.03512 0.03070 -0.1204 0.9838 0.0329
-15.000 -0.9515 0.02773 0.02312 -0.1276 0.9714 0.0335
-14.750 -0.9443 0.02490 0.02021 -0.1305 0.9621 0.0339
-14.500 -0.9250 0.02252 0.01774 -0.1347 0.9540 0.0344
-14.250 -0.8976 0.02056 0.01567 -0.1396 0.9434 0.0349
-14.000 -0.8575 0.01924 0.01427 -0.1450 0.9343 0.0357
-13.750 -0.8112 0.01826 0.01319 -0.1507 0.9263 0.0364
-13.500 -0.7724 0.01728 0.01213 -0.1550 0.9160 0.0372
-13.250 -0.7438 0.01654 0.01130 -0.1567 0.9035 0.0382
-13.000 -0.7292 0.01604 0.01071 -0.1553 0.8905 0.0391
-12.750 -0.7123 0.01560 0.01019 -0.1541 0.8807 0.0399
-12.500 -0.6955 0.01521 0.00974 -0.1527 0.8711 0.0406
-12.250 -0.6783 0.01481 0.00927 -0.1513 0.8637 0.0417
-12.000 -0.6609 0.01440 0.00884 -0.1498 0.8580 0.0430
-11.750 -0.6418 0.01405 0.00845 -0.1486 0.8518 0.0443
-11.500 -0.6213 0.01375 0.00809 -0.1475 0.8456 0.0457
-11.250 -0.6014 0.01339 0.00772 -0.1463 0.8402 0.0475
-11.000 -0.5803 0.01308 0.00738 -0.1453 0.8343 0.0497
-10.750 -0.5585 0.01279 0.00706 -0.1444 0.8287 0.0517
-10.500 -0.5363 0.01251 0.00676 -0.1435 0.8237 0.0543
-10.250 -0.5133 0.01224 0.00648 -0.1427 0.8189 0.0570
-10.000 -0.4903 0.01198 0.00621 -0.1418 0.8131 0.0600
-9.750 -0.4667 0.01178 0.00596 -0.1411 0.8070 0.0625
-9.500 -0.4432 0.01153 0.00570 -0.1403 0.8014 0.0652
-9.250 -0.4189 0.01132 0.00548 -0.1396 0.7947 0.0677
-9.000 -0.3948 0.01115 0.00526 -0.1389 0.7878 0.0698
-8.750 -0.3704 0.01094 0.00503 -0.1382 0.7818 0.0724
-8.500 -0.3456 0.01076 0.00483 -0.1376 0.7746 0.0747
-8.250 -0.3211 0.01063 0.00465 -0.1369 0.7670 0.0766
-8.000 -0.2964 0.01042 0.00443 -0.1362 0.7594 0.0794
-7.750 -0.2720 0.01027 0.00425 -0.1354 0.7501 0.0821
-7.500 -0.2470 0.01015 0.00408 -0.1348 0.7406 0.0842
-7.250 -0.2237 0.01001 0.00389 -0.1338 0.7283 0.0873
-7.000 -0.1995 0.00988 0.00372 -0.1330 0.7143 0.0903
-6.750 -0.1757 0.00979 0.00358 -0.1320 0.6991 0.0933
-6.500 -0.1526 0.00968 0.00342 -0.1310 0.6838 0.0977
-6.000 -0.1058 0.00948 0.00314 -0.1290 0.6549 0.1104
-5.750 -0.0820 0.00934 0.00300 -0.1282 0.6432 0.1213
-5.500 -0.0586 0.00922 0.00288 -0.1272 0.6321 0.1335
-5.250 -0.0337 0.00909 0.00277 -0.1265 0.6229 0.1444
-4.750 0.0165 0.00893 0.00259 -0.1252 0.6070 0.1614
-4.500 0.0417 0.00886 0.00252 -0.1245 0.5993 0.1689
-4.250 0.0668 0.00882 0.00245 -0.1238 0.5923 0.1762
-4.000 0.0928 0.00873 0.00238 -0.1233 0.5861 0.1851
-3.750 0.1183 0.00870 0.00233 -0.1227 0.5791 0.1925
-3.500 0.1432 0.00866 0.00229 -0.1219 0.5724 0.2011
-3.250 0.1694 0.00862 0.00225 -0.1214 0.5656 0.2082
-3.000 0.1946 0.00859 0.00221 -0.1207 0.5587 0.2164
-2.750 0.2198 0.00858 0.00219 -0.1200 0.5530 0.2242
-2.500 0.2463 0.00853 0.00216 -0.1196 0.5492 0.2319
-2.250 0.2723 0.00851 0.00215 -0.1190 0.5437 0.2404
-2.000 0.2973 0.00852 0.00214 -0.1183 0.5375 0.2470
-1.750 0.3225 0.00851 0.00214 -0.1176 0.5322 0.2560
-1.500 0.3489 0.00849 0.00213 -0.1171 0.5283 0.2632
-1.250 0.3745 0.00849 0.00213 -0.1165 0.5231 0.2700
-1.000 0.3993 0.00851 0.00214 -0.1157 0.5176 0.2765
-0.750 0.4241 0.00853 0.00215 -0.1149 0.5128 0.2843
-0.500 0.4500 0.00852 0.00217 -0.1144 0.5087 0.2904
-0.250 0.4751 0.00853 0.00218 -0.1136 0.5047 0.2950
0.000 0.4993 0.00856 0.00219 -0.1127 0.5008 0.2987
0.250 0.5225 0.00857 0.00221 -0.1116 0.4968 0.3048
0.500 0.5466 0.00859 0.00224 -0.1106 0.4933 0.3103
0.750 0.5716 0.00861 0.00226 -0.1099 0.4894 0.3150
1.000 0.5958 0.00864 0.00229 -0.1090 0.4843 0.3191
1.250 0.6190 0.00867 0.00233 -0.1079 0.4795 0.3257
1.500 0.6423 0.00873 0.00238 -0.1068 0.4749 0.3315
1.750 0.6671 0.00877 0.00243 -0.1061 0.4695 0.3370
2.000 0.6900 0.00882 0.00249 -0.1050 0.4626 0.3438
2.250 0.7120 0.00892 0.00257 -0.1036 0.4556 0.3504
2.500 0.7353 0.00900 0.00265 -0.1026 0.4471 0.3561
2.750 0.7562 0.00913 0.00275 -0.1011 0.4371 0.3625
3.000 0.7780 0.00924 0.00286 -0.0998 0.4253 0.3693
3.250 0.7978 0.00943 0.00299 -0.0982 0.4089 0.3753
3.500 0.8162 0.00966 0.00314 -0.0963 0.3903 0.3816
3.750 0.8339 0.00989 0.00332 -0.0943 0.3730 0.3898
4.000 0.8521 0.01014 0.00351 -0.0924 0.3576 0.3969
4.250 0.8706 0.01038 0.00371 -0.0906 0.3443 0.4044
4.750 0.9084 0.01080 0.00410 -0.0872 0.3241 0.4230
5.000 0.9268 0.01102 0.00432 -0.0854 0.3158 0.4371
5.250 0.9467 0.01118 0.00451 -0.0839 0.3093 0.4533
5.500 0.9661 0.01134 0.00472 -0.0824 0.3033 0.4743
5.750 0.9829 0.01158 0.00499 -0.0804 0.2957 0.5004
6.000 1.0017 0.01173 0.00522 -0.0788 0.2888 0.5347
6.250 1.0180 0.01200 0.00553 -0.0768 0.2802 0.5688
6.500 1.0357 0.01221 0.00580 -0.0750 0.2737 0.5988
6.750 1.0539 0.01244 0.00608 -0.0733 0.2679 0.6215
7.000 1.0709 0.01273 0.00638 -0.0715 0.2620 0.6388
7.250 1.0888 0.01300 0.00667 -0.0699 0.2564 0.6541
7.500 1.1061 0.01328 0.00698 -0.0682 0.2502 0.6688
7.750 1.1209 0.01365 0.00736 -0.0661 0.2426 0.6849
8.000 1.1388 0.01391 0.00768 -0.0645 0.2389 0.7021
8.250 1.1531 0.01430 0.00809 -0.0625 0.2302 0.7221
8.500 1.1673 0.01462 0.00851 -0.0603 0.2249 0.7557
9.000 1.2845 0.01558 0.00980 -0.0750 0.2018 1.0000
9.250 1.3005 0.01619 0.01038 -0.0736 0.1937 1.0000
9.500 1.3175 0.01678 0.01093 -0.0723 0.1865 1.0000
9.750 1.3327 0.01746 0.01158 -0.0709 0.1798 1.0000
10.000 1.3489 0.01811 0.01221 -0.0697 0.1733 1.0000
10.250 1.3626 0.01890 0.01298 -0.0682 0.1668 1.0000
10.500 1.3793 0.01955 0.01362 -0.0671 0.1625 1.0000
10.750 1.3927 0.02039 0.01444 -0.0657 0.1565 1.0000
11.000 1.4070 0.02119 0.01524 -0.0644 0.1520 1.0000
11.250 1.4219 0.02198 0.01604 -0.0633 0.1476 1.0000
11.500 1.4344 0.02294 0.01698 -0.0619 0.1428 1.0000
11.750 1.4479 0.02385 0.01790 -0.0607 0.1388 1.0000
12.000 1.4609 0.02480 0.01886 -0.0596 0.1340 1.0000
12.250 1.4702 0.02603 0.02006 -0.0581 0.1274 1.0000
12.500 1.4796 0.02729 0.02130 -0.0568 0.1190 1.0000
12.750 1.4815 0.02911 0.02305 -0.0549 0.1053 1.0000
13.000 1.4785 0.03138 0.02522 -0.0529 0.0887 1.0000
13.250 1.4798 0.03341 0.02722 -0.0514 0.0806 1.0000
13.500 1.4857 0.03514 0.02896 -0.0502 0.0765 1.0000
13.750 1.4922 0.03687 0.03071 -0.0492 0.0738 1.0000
14.000 1.4972 0.03876 0.03263 -0.0482 0.0711 1.0000
14.250 1.5052 0.04043 0.03433 -0.0475 0.0691 1.0000
14.500 1.5120 0.04227 0.03620 -0.0467 0.0676 1.0000
14.750 1.5179 0.04420 0.03817 -0.0460 0.0662 1.0000
15.000 1.5228 0.04624 0.04024 -0.0454 0.0648 1.0000
15.250 1.5278 0.04832 0.04237 -0.0448 0.0636 1.0000
15.500 1.5348 0.05022 0.04432 -0.0443 0.0628 1.0000
15.750 1.5404 0.05229 0.04645 -0.0439 0.0620 1.0000
16.000 1.5452 0.05446 0.04867 -0.0435 0.0611 1.0000
16.250 1.5491 0.05673 0.05098 -0.0431 0.0602 1.0000
16.500 1.5513 0.05920 0.05351 -0.0427 0.0594 1.0000
16.750 1.5532 0.06172 0.05606 -0.0424 0.0583 1.0000
17.000 1.5536 0.06446 0.05886 -0.0422 0.0574 1.0000
17.250 1.5572 0.06684 0.06129 -0.0420 0.0566 1.0000
17.500 1.5590 0.06945 0.06397 -0.0419 0.0560 1.0000
17.750 1.5611 0.07202 0.06659 -0.0418 0.0552 1.0000
18.000 1.5613 0.07487 0.06950 -0.0418 0.0543 1.0000
18.250 1.5612 0.07775 0.07244 -0.0418 0.0536 1.0000
18.500 1.5595 0.08087 0.07560 -0.0420 0.0527 1.0000
18.750 1.5559 0.08421 0.07900 -0.0421 0.0517 1.0000
19.000 1.5538 0.08740 0.08225 -0.0424 0.0512 1.0000
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