GOE 256 (JUNKERS E) AIRFOIL (goe256-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 256 (JUNKERS E) AIRFOIL (goe256-il) Reynolds number: 1,000,000 Max Cl/Cd: 112.88 at α=5.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe256-il-1000000.txt Download as CSV file: xf-goe256-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: GOE 256 (JUNKERS E) 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
------ -------- --------- --------- -------- -------- --------
-15.000 -0.8570 0.03917 0.03633 -0.1193 0.9950 0.0294
-14.750 -0.8590 0.03477 0.03171 -0.1240 0.9873 0.0295
-14.500 -0.8550 0.03201 0.02877 -0.1257 0.9774 0.0297
-14.250 -0.8514 0.03000 0.02659 -0.1252 0.9639 0.0299
-14.000 -0.8491 0.02849 0.02491 -0.1232 0.9492 0.0301
-13.750 -0.8455 0.02724 0.02349 -0.1207 0.9363 0.0302
-13.500 -0.8392 0.02619 0.02229 -0.1183 0.9254 0.0304
-13.250 -0.8271 0.02520 0.02115 -0.1167 0.9169 0.0306
-13.000 -0.8128 0.02433 0.02013 -0.1152 0.9087 0.0307
-12.750 -0.7954 0.02366 0.01932 -0.1141 0.9017 0.0309
-12.500 -0.7873 0.02187 0.01733 -0.1121 0.8936 0.0313
-12.250 -0.7711 0.02088 0.01622 -0.1108 0.8866 0.0317
-12.000 -0.7513 0.02019 0.01547 -0.1099 0.8798 0.0319
-11.750 -0.7305 0.01963 0.01482 -0.1090 0.8728 0.0322
-11.500 -0.7087 0.01910 0.01423 -0.1083 0.8664 0.0325
-11.250 -0.6863 0.01858 0.01365 -0.1076 0.8596 0.0328
-11.000 -0.6639 0.01809 0.01305 -0.1069 0.8530 0.0331
-10.750 -0.6408 0.01757 0.01246 -0.1063 0.8467 0.0335
-10.500 -0.6175 0.01708 0.01187 -0.1057 0.8398 0.0338
-10.250 -0.5940 0.01661 0.01129 -0.1050 0.8335 0.0342
-10.000 -0.5698 0.01614 0.01075 -0.1046 0.8271 0.0345
-9.750 -0.5453 0.01574 0.01025 -0.1041 0.8206 0.0348
-9.500 -0.5203 0.01539 0.00981 -0.1036 0.8147 0.0351
-9.250 -0.4974 0.01468 0.00901 -0.1030 0.8086 0.0357
-9.000 -0.4735 0.01416 0.00844 -0.1024 0.8029 0.0363
-8.750 -0.4480 0.01385 0.00808 -0.1020 0.7979 0.0368
-8.500 -0.4219 0.01355 0.00776 -0.1018 0.7932 0.0373
-8.250 -0.3958 0.01327 0.00743 -0.1015 0.7885 0.0378
-8.000 -0.3698 0.01300 0.00710 -0.1012 0.7838 0.0384
-7.750 -0.3433 0.01274 0.00678 -0.1010 0.7796 0.0390
-7.500 -0.3166 0.01248 0.00648 -0.1008 0.7757 0.0395
-7.250 -0.2897 0.01228 0.00621 -0.1006 0.7707 0.0399
-6.750 -0.2391 0.01154 0.00541 -0.0997 0.7586 0.0417
-6.500 -0.2122 0.01136 0.00520 -0.0995 0.7530 0.0426
-6.250 -0.1851 0.01122 0.00501 -0.0993 0.7482 0.0436
-6.000 -0.1576 0.01108 0.00483 -0.0992 0.7446 0.0446
-5.750 -0.1297 0.01094 0.00467 -0.0992 0.7412 0.0452
-5.500 -0.1039 0.01057 0.00430 -0.0988 0.7376 0.0468
-5.250 -0.0765 0.01044 0.00416 -0.0987 0.7339 0.0481
-5.000 -0.0489 0.01035 0.00403 -0.0986 0.7299 0.0494
-4.750 -0.0210 0.01023 0.00390 -0.0986 0.7268 0.0506
-4.500 0.0060 0.01000 0.00366 -0.0984 0.7234 0.0523
-4.250 0.0337 0.00986 0.00354 -0.0984 0.7198 0.0540
-4.000 0.0616 0.00979 0.00345 -0.0983 0.7161 0.0558
-3.750 0.0896 0.00976 0.00338 -0.0983 0.7121 0.0574
-3.500 0.1167 0.00955 0.00319 -0.0982 0.7090 0.0596
-3.250 0.1446 0.00944 0.00310 -0.0982 0.7054 0.0615
-3.000 0.1726 0.00936 0.00302 -0.0981 0.7013 0.0635
-2.750 0.2005 0.00932 0.00295 -0.0981 0.6973 0.0650
-2.500 0.2275 0.00917 0.00278 -0.0979 0.6932 0.0678
-2.250 0.2554 0.00907 0.00272 -0.0979 0.6896 0.0702
-2.000 0.2834 0.00899 0.00264 -0.0979 0.6850 0.0724
-1.750 0.3111 0.00896 0.00258 -0.0979 0.6800 0.0738
-1.500 0.3378 0.00881 0.00243 -0.0976 0.6751 0.0777
-1.250 0.3658 0.00871 0.00237 -0.0976 0.6704 0.0806
-1.000 0.3934 0.00866 0.00231 -0.0976 0.6647 0.0831
-0.750 0.4201 0.00860 0.00221 -0.0973 0.6586 0.0871
-0.500 0.4478 0.00849 0.00215 -0.0972 0.6520 0.0915
-0.250 0.4746 0.00847 0.00210 -0.0970 0.6438 0.0954
0.000 0.5014 0.00838 0.00205 -0.0968 0.6352 0.1049
0.250 0.5271 0.00831 0.00201 -0.0964 0.6246 0.1251
0.500 0.5506 0.00795 0.00199 -0.0957 0.6122 0.2427
0.750 0.5727 0.00763 0.00201 -0.0947 0.5970 0.3765
1.000 0.5929 0.00734 0.00205 -0.0934 0.5785 0.5166
1.250 0.6049 0.00671 0.00211 -0.0903 0.5592 0.7631
1.500 0.6188 0.00671 0.00246 -0.0867 0.5400 0.9288
1.750 0.6398 0.00696 0.00262 -0.0851 0.5216 0.9463
2.000 0.6616 0.00721 0.00279 -0.0837 0.5053 0.9577
2.250 0.6834 0.00743 0.00294 -0.0823 0.4916 0.9677
2.500 0.7190 0.00771 0.00314 -0.0840 0.4788 0.9744
2.750 0.7530 0.00799 0.00334 -0.0853 0.4673 0.9813
3.000 0.8219 0.00840 0.00364 -0.0945 0.4538 0.9846
3.250 0.8697 0.00862 0.00380 -0.0989 0.4441 0.9879
3.500 0.9129 0.00889 0.00400 -0.1024 0.4348 0.9928
3.750 0.9787 0.00907 0.00410 -0.1109 0.4245 0.9966
4.000 1.0293 0.00924 0.00419 -0.1161 0.4131 1.0000
4.250 1.0490 0.00943 0.00433 -0.1147 0.4045 1.0000
4.500 1.0697 0.00956 0.00444 -0.1134 0.3985 1.0000
4.750 1.0899 0.00969 0.00456 -0.1120 0.3927 1.0000
5.000 1.1079 0.00989 0.00471 -0.1102 0.3866 1.0000
5.250 1.1272 0.01001 0.00484 -0.1086 0.3820 1.0000
5.500 1.1457 0.01015 0.00497 -0.1068 0.3770 1.0000
5.750 1.1616 0.01032 0.00512 -0.1046 0.3720 1.0000
6.000 1.1758 0.01051 0.00529 -0.1020 0.3671 1.0000
6.250 1.1917 0.01062 0.00542 -0.0997 0.3632 1.0000
6.500 1.2028 0.01076 0.00556 -0.0964 0.3589 1.0000
6.750 1.2030 0.01090 0.00570 -0.0909 0.3549 1.0000
7.000 1.2037 0.01107 0.00586 -0.0855 0.3507 1.0000
7.250 1.2135 0.01117 0.00599 -0.0821 0.3476 1.0000
7.500 1.2237 0.01132 0.00615 -0.0787 0.3439 1.0000
7.750 1.2354 0.01153 0.00636 -0.0758 0.3400 1.0000
8.000 1.2493 0.01182 0.00664 -0.0735 0.3353 1.0000
8.250 1.2691 0.01204 0.00687 -0.0723 0.3312 1.0000
8.500 1.2889 0.01230 0.00714 -0.0711 0.3262 1.0000
8.750 1.3076 0.01263 0.00746 -0.0699 0.3215 1.0000
9.000 1.3263 0.01299 0.00782 -0.0687 0.3167 1.0000
9.250 1.3475 0.01327 0.00812 -0.0679 0.3111 1.0000
9.500 1.3647 0.01374 0.00856 -0.0666 0.3034 1.0000
9.750 1.3847 0.01410 0.00893 -0.0658 0.2969 1.0000
10.000 1.4026 0.01458 0.00938 -0.0646 0.2890 1.0000
10.250 1.4206 0.01506 0.00986 -0.0635 0.2807 1.0000
10.500 1.4357 0.01570 0.01045 -0.0621 0.2695 1.0000
10.750 1.4516 0.01633 0.01105 -0.0609 0.2573 1.0000
11.000 1.4635 0.01718 0.01182 -0.0591 0.2403 1.0000
11.250 1.4703 0.01835 0.01285 -0.0568 0.2144 1.0000
11.500 1.4699 0.01999 0.01430 -0.0538 0.1842 1.0000
11.750 1.4734 0.02145 0.01565 -0.0514 0.1661 1.0000
12.000 1.4814 0.02268 0.01684 -0.0496 0.1553 1.0000
12.250 1.4926 0.02373 0.01789 -0.0482 0.1480 1.0000
12.500 1.5010 0.02499 0.01913 -0.0467 0.1407 1.0000
12.750 1.5132 0.02601 0.02017 -0.0455 0.1355 1.0000
13.000 1.5229 0.02725 0.02140 -0.0442 0.1301 1.0000
13.250 1.5330 0.02849 0.02265 -0.0430 0.1252 1.0000
13.500 1.5445 0.02965 0.02383 -0.0420 0.1209 1.0000
13.750 1.5523 0.03110 0.02529 -0.0408 0.1160 1.0000
14.000 1.5624 0.03240 0.02661 -0.0398 0.1117 1.0000
14.250 1.5705 0.03391 0.02812 -0.0387 0.1067 1.0000
14.500 1.5766 0.03560 0.02982 -0.0376 0.1015 1.0000
14.750 1.5846 0.03716 0.03141 -0.0366 0.0965 1.0000
15.000 1.5875 0.03919 0.03342 -0.0355 0.0901 1.0000
15.250 1.5874 0.04152 0.03572 -0.0342 0.0812 1.0000
15.500 1.5801 0.04458 0.03872 -0.0327 0.0667 1.0000
15.750 1.5572 0.04928 0.04330 -0.0308 0.0465 1.0000
16.000 1.5365 0.05400 0.04798 -0.0294 0.0340 1.0000
16.250 1.5262 0.05784 0.05186 -0.0286 0.0291 1.0000
16.500 1.5203 0.06130 0.05537 -0.0280 0.0265 1.0000
16.750 1.5158 0.06468 0.05881 -0.0277 0.0247 1.0000
17.000 1.5117 0.06810 0.06230 -0.0276 0.0234 1.0000
17.250 1.5056 0.07183 0.06609 -0.0275 0.0223 1.0000
17.500 1.5018 0.07530 0.06964 -0.0275 0.0215 1.0000
17.750 1.4981 0.07881 0.07323 -0.0277 0.0208 1.0000
18.000 1.4930 0.08254 0.07703 -0.0279 0.0201 1.0000
18.250 1.4866 0.08647 0.08103 -0.0283 0.0196 1.0000
18.500 1.4782 0.09072 0.08536 -0.0288 0.0190 1.0000
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