GOE 646 AIRFOIL (goe646-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 646 AIRFOIL (goe646-il) Reynolds number: 500,000 Max Cl/Cd: 95.93 at α=5.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe646-il-500000.txt Download as CSV file: xf-goe646-il-500000.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 = 0.500 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.500 -0.8181 0.10661 0.10281 -0.0766 1.0000 0.0407
-19.250 -0.8367 0.10035 0.09641 -0.0800 1.0000 0.0409
-19.000 -0.8510 0.09506 0.09100 -0.0827 1.0000 0.0412
-18.750 -0.8478 0.09288 0.08884 -0.0831 1.0000 0.0417
-18.500 -0.8473 0.09011 0.08606 -0.0840 1.0000 0.0421
-18.250 -0.8483 0.08712 0.08304 -0.0851 1.0000 0.0424
-18.000 -0.8510 0.08388 0.07977 -0.0864 1.0000 0.0429
-17.750 -0.8550 0.08048 0.07633 -0.0877 1.0000 0.0433
-17.500 -0.8599 0.07705 0.07285 -0.0890 1.0000 0.0437
-17.250 -0.8661 0.07352 0.06925 -0.0903 1.0000 0.0442
-17.000 -0.8731 0.06998 0.06564 -0.0916 1.0000 0.0447
-16.750 -0.8796 0.06666 0.06224 -0.0926 1.0000 0.0450
-16.500 -0.8864 0.06346 0.05897 -0.0935 1.0000 0.0453
-16.250 -0.8955 0.06012 0.05553 -0.0944 1.0000 0.0457
-16.000 -0.9013 0.05766 0.05304 -0.0942 1.0000 0.0461
-15.750 -0.9057 0.05576 0.05117 -0.0933 1.0000 0.0465
-15.500 -0.9161 0.05342 0.04883 -0.0924 1.0000 0.0469
-15.250 -0.9319 0.05115 0.04655 -0.0908 1.0000 0.0471
-15.000 -0.9307 0.04825 0.04361 -0.0930 0.9987 0.0476
-14.750 -0.9177 0.04501 0.04032 -0.0975 0.9961 0.0484
-14.500 -0.9030 0.04196 0.03718 -0.1021 0.9934 0.0491
-14.250 -0.8901 0.03888 0.03400 -0.1063 0.9901 0.0501
-14.000 -0.8756 0.03602 0.03103 -0.1103 0.9860 0.0508
-13.750 -0.8598 0.03306 0.02802 -0.1150 0.9825 0.0518
-13.500 -0.8378 0.03024 0.02517 -0.1205 0.9800 0.0529
-13.250 -0.8249 0.02784 0.02270 -0.1233 0.9718 0.0538
-13.000 -0.7989 0.02564 0.02041 -0.1282 0.9683 0.0552
-12.750 -0.7840 0.02389 0.01854 -0.1302 0.9604 0.0563
-12.500 -0.7650 0.02234 0.01694 -0.1318 0.9554 0.0578
-12.250 -0.7357 0.02120 0.01577 -0.1341 0.9531 0.0597
-12.000 -0.7180 0.02041 0.01491 -0.1335 0.9458 0.0614
-11.750 -0.6903 0.01950 0.01394 -0.1348 0.9422 0.0636
-11.500 -0.6578 0.01862 0.01306 -0.1371 0.9397 0.0663
-11.250 -0.6205 0.01801 0.01235 -0.1396 0.9379 0.0693
-11.000 -0.6002 0.01724 0.01160 -0.1393 0.9314 0.0721
-10.750 -0.5703 0.01673 0.01104 -0.1403 0.9268 0.0754
-10.500 -0.5376 0.01604 0.01031 -0.1421 0.9232 0.0790
-10.250 -0.5061 0.01557 0.00980 -0.1433 0.9188 0.0828
-10.000 -0.4845 0.01515 0.00934 -0.1425 0.9118 0.0860
-9.750 -0.4559 0.01465 0.00882 -0.1432 0.9068 0.0898
-9.500 -0.4231 0.01434 0.00842 -0.1444 0.9025 0.0933
-9.250 -0.4066 0.01390 0.00801 -0.1425 0.8953 0.0968
-9.000 -0.3804 0.01359 0.00765 -0.1424 0.8896 0.1007
-8.750 -0.3501 0.01322 0.00724 -0.1431 0.8846 0.1052
-8.500 -0.3317 0.01295 0.00697 -0.1413 0.8776 0.1094
-8.250 -0.3067 0.01269 0.00666 -0.1408 0.8714 0.1140
-8.000 -0.2781 0.01236 0.00632 -0.1411 0.8661 0.1201
-7.750 -0.2573 0.01212 0.00608 -0.1397 0.8596 0.1258
-7.500 -0.2336 0.01184 0.00582 -0.1389 0.8532 0.1333
-7.250 -0.2058 0.01157 0.00553 -0.1389 0.8476 0.1425
-7.000 -0.1831 0.01135 0.00532 -0.1379 0.8410 0.1519
-6.750 -0.1588 0.01114 0.00511 -0.1371 0.8339 0.1622
-6.500 -0.1309 0.01091 0.00488 -0.1370 0.8276 0.1744
-6.250 -0.1087 0.01071 0.00472 -0.1358 0.8196 0.1856
-6.000 -0.0831 0.01054 0.00454 -0.1352 0.8119 0.1964
-5.750 -0.0566 0.01042 0.00439 -0.1348 0.8044 0.2066
-5.500 -0.0329 0.01026 0.00426 -0.1338 0.7954 0.2160
-5.000 0.0182 0.01005 0.00401 -0.1325 0.7770 0.2337
-4.500 0.0688 0.00990 0.00380 -0.1311 0.7560 0.2505
-4.250 0.0945 0.00988 0.00370 -0.1304 0.7447 0.2584
-4.000 0.1189 0.00981 0.00360 -0.1295 0.7320 0.2657
-3.750 0.1432 0.00979 0.00354 -0.1285 0.7186 0.2732
-3.500 0.1681 0.00980 0.00347 -0.1277 0.7060 0.2800
-3.250 0.1923 0.00978 0.00342 -0.1268 0.6935 0.2873
-3.000 0.2173 0.00981 0.00339 -0.1260 0.6820 0.2939
-2.750 0.2421 0.00984 0.00334 -0.1252 0.6713 0.3003
-2.500 0.2666 0.00985 0.00334 -0.1243 0.6606 0.3074
-2.250 0.2918 0.00994 0.00334 -0.1236 0.6507 0.3146
-2.000 0.3163 0.00994 0.00332 -0.1228 0.6410 0.3220
-1.750 0.3416 0.01001 0.00334 -0.1221 0.6330 0.3290
-1.500 0.3673 0.01006 0.00336 -0.1215 0.6255 0.3352
-1.250 0.3924 0.01007 0.00334 -0.1208 0.6183 0.3415
-1.000 0.4177 0.01010 0.00337 -0.1201 0.6114 0.3475
-0.750 0.4432 0.01014 0.00338 -0.1194 0.6047 0.3534
-0.500 0.4687 0.01019 0.00338 -0.1188 0.5985 0.3595
-0.250 0.4946 0.01022 0.00342 -0.1183 0.5932 0.3662
0.000 0.5199 0.01023 0.00345 -0.1176 0.5878 0.3725
0.250 0.5456 0.01029 0.00347 -0.1170 0.5825 0.3785
0.500 0.5713 0.01032 0.00351 -0.1165 0.5776 0.3862
0.750 0.5974 0.01037 0.00357 -0.1160 0.5732 0.3938
1.000 0.6224 0.01038 0.00360 -0.1153 0.5687 0.4013
1.250 0.6470 0.01038 0.00365 -0.1145 0.5638 0.4101
1.500 0.6724 0.01047 0.00370 -0.1139 0.5587 0.4188
1.750 0.6976 0.01050 0.00377 -0.1133 0.5541 0.4288
2.000 0.7215 0.01050 0.00383 -0.1124 0.5496 0.4396
2.250 0.7453 0.01050 0.00389 -0.1114 0.5449 0.4520
2.500 0.7693 0.01055 0.00395 -0.1106 0.5400 0.4664
2.750 0.7931 0.01060 0.00405 -0.1097 0.5347 0.4857
3.000 0.8135 0.01055 0.00413 -0.1080 0.5291 0.5104
3.250 0.8327 0.01054 0.00421 -0.1062 0.5228 0.5422
3.500 0.8527 0.01059 0.00433 -0.1045 0.5163 0.5785
3.750 0.8700 0.01057 0.00444 -0.1022 0.5098 0.6125
4.000 0.8885 0.01062 0.00455 -0.1002 0.5031 0.6416
4.250 0.9079 0.01074 0.00469 -0.0984 0.4968 0.6664
4.500 0.9270 0.01078 0.00482 -0.0965 0.4905 0.6881
4.750 0.9453 0.01086 0.00495 -0.0945 0.4836 0.7092
5.000 0.9633 0.01095 0.00510 -0.0925 0.4768 0.7330
5.250 0.9798 0.01094 0.00526 -0.0901 0.4690 0.7680
5.500 1.0071 0.01084 0.00550 -0.0900 0.4600 0.9017
5.750 1.0619 0.01107 0.00575 -0.0959 0.4470 1.0000
6.000 1.0792 0.01129 0.00593 -0.0940 0.4361 1.0000
6.250 1.0939 0.01158 0.00614 -0.0916 0.4230 1.0000
6.500 1.1087 0.01190 0.00639 -0.0892 0.4075 1.0000
6.750 1.1231 0.01227 0.00669 -0.0869 0.3914 1.0000
7.000 1.1357 0.01273 0.00705 -0.0843 0.3748 1.0000
7.250 1.1493 0.01320 0.00744 -0.0820 0.3606 1.0000
7.500 1.1627 0.01371 0.00788 -0.0798 0.3487 1.0000
7.750 1.1767 0.01424 0.00834 -0.0776 0.3378 1.0000
8.000 1.1927 0.01471 0.00878 -0.0759 0.3292 1.0000
8.250 1.2075 0.01525 0.00928 -0.0740 0.3209 1.0000
8.500 1.2233 0.01577 0.00978 -0.0724 0.3136 1.0000
8.750 1.2398 0.01628 0.01027 -0.0709 0.3065 1.0000
9.000 1.2524 0.01698 0.01092 -0.0689 0.2991 1.0000
9.250 1.2714 0.01742 0.01139 -0.0678 0.2932 1.0000
9.500 1.2860 0.01806 0.01201 -0.0663 0.2865 1.0000
9.750 1.3003 0.01874 0.01267 -0.0647 0.2804 1.0000
10.000 1.3178 0.01929 0.01325 -0.0636 0.2741 1.0000
10.250 1.3312 0.02006 0.01399 -0.0620 0.2674 1.0000
10.500 1.3463 0.02076 0.01470 -0.0607 0.2619 1.0000
10.750 1.3622 0.02144 0.01540 -0.0596 0.2558 1.0000
11.000 1.3740 0.02236 0.01629 -0.0581 0.2494 1.0000
11.250 1.3891 0.02313 0.01710 -0.0569 0.2433 1.0000
11.500 1.4027 0.02400 0.01798 -0.0557 0.2368 1.0000
11.750 1.4126 0.02513 0.01908 -0.0542 0.2305 1.0000
12.000 1.4277 0.02595 0.01995 -0.0533 0.2247 1.0000
12.250 1.4376 0.02715 0.02113 -0.0519 0.2183 1.0000
12.500 1.4490 0.02827 0.02227 -0.0508 0.2121 1.0000
12.750 1.4600 0.02945 0.02347 -0.0497 0.2061 1.0000
13.000 1.4667 0.03097 0.02496 -0.0484 0.2004 1.0000
13.250 1.4790 0.03211 0.02616 -0.0475 0.1951 1.0000
13.500 1.4871 0.03362 0.02767 -0.0464 0.1894 1.0000
13.750 1.4935 0.03527 0.02933 -0.0454 0.1842 1.0000
14.000 1.5030 0.03673 0.03083 -0.0445 0.1785 1.0000
14.250 1.5071 0.03867 0.03277 -0.0435 0.1728 1.0000
14.500 1.5146 0.04036 0.03449 -0.0427 0.1673 1.0000
14.750 1.5188 0.04239 0.03654 -0.0419 0.1611 1.0000
15.000 1.5218 0.04456 0.03872 -0.0411 0.1549 1.0000
15.250 1.5250 0.04675 0.04093 -0.0404 0.1478 1.0000
15.500 1.5262 0.04917 0.04337 -0.0398 0.1402 1.0000
15.750 1.5229 0.05211 0.04629 -0.0391 0.1306 1.0000
16.000 1.5191 0.05514 0.04930 -0.0386 0.1201 1.0000
16.250 1.5129 0.05846 0.05259 -0.0381 0.1092 1.0000
16.500 1.5062 0.06190 0.05601 -0.0377 0.1006 1.0000
16.750 1.4992 0.06542 0.05954 -0.0374 0.0946 1.0000
17.000 1.4906 0.06917 0.06330 -0.0372 0.0907 1.0000
17.250 1.4862 0.07252 0.06670 -0.0371 0.0880 1.0000
17.500 1.4817 0.07590 0.07013 -0.0371 0.0858 1.0000
17.750 1.4737 0.07975 0.07402 -0.0372 0.0837 1.0000
18.000 1.4639 0.08384 0.07814 -0.0375 0.0819 1.0000
18.250 1.4623 0.08698 0.08136 -0.0377 0.0806 1.0000
18.500 1.4591 0.09035 0.08481 -0.0380 0.0794 1.0000
18.750 1.4565 0.09367 0.08819 -0.0383 0.0781 1.0000
19.000 1.4518 0.09726 0.09184 -0.0388 0.0771 1.0000
19.250 1.4465 0.10092 0.09554 -0.0394 0.0759 1.0000
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