GOE 613 AIRFOIL (goe613-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 613 AIRFOIL (goe613-il) Reynolds number: 500,000 Max Cl/Cd: 93.82 at α=3.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe613-il-500000.txt Download as CSV file: xf-goe613-il-500000.csv |
XFOIL Version 6.96
Calculated polar for: GOE 613 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
------ -------- --------- --------- -------- -------- --------
-9.500 -0.3396 0.10336 0.10118 -0.0323 1.0000 0.0240
-9.250 -0.3524 0.10103 0.09890 -0.0318 1.0000 0.0242
-9.000 -0.3609 0.09835 0.09625 -0.0319 0.9997 0.0243
-8.750 -0.3491 0.09287 0.09078 -0.0388 0.9971 0.0244
-8.500 -0.3347 0.08769 0.08559 -0.0454 0.9942 0.0244
-8.250 -0.3271 0.08288 0.08079 -0.0467 0.9915 0.0249
-8.000 -0.3088 0.08002 0.07793 -0.0491 0.9885 0.0254
-7.750 -0.2902 0.07665 0.07455 -0.0537 0.9853 0.0262
-7.500 -0.2747 0.07235 0.07024 -0.0601 0.9793 0.0274
-7.250 -0.2416 0.06248 0.06020 -0.0798 0.9726 0.0302
-7.000 -0.2223 0.05637 0.05392 -0.0861 0.9655 0.0304
-6.750 -0.2103 0.04834 0.04574 -0.0914 0.9611 0.0311
-6.500 -0.1841 0.04606 0.04344 -0.0940 0.9594 0.0318
-6.250 -0.1543 0.04370 0.04102 -0.0973 0.9580 0.0329
-6.000 -0.1350 0.04101 0.03821 -0.0982 0.9506 0.0346
-5.750 -0.0982 0.03751 0.03413 -0.1012 0.9465 0.0382
-5.500 -0.0862 0.03067 0.02700 -0.1024 0.9399 0.0394
-5.250 -0.0604 0.02904 0.02535 -0.1033 0.9344 0.0404
-5.000 -0.0308 0.02745 0.02366 -0.1047 0.9305 0.0418
-4.750 -0.0086 0.02586 0.02191 -0.1042 0.9222 0.0439
-4.500 0.0256 0.02638 0.02204 -0.1041 0.9164 0.0481
-4.250 0.0379 0.02158 0.01683 -0.1026 0.9068 0.0499
-4.000 0.0658 0.02022 0.01546 -0.1032 0.8995 0.0515
-3.750 0.0879 0.01926 0.01439 -0.1021 0.8884 0.0534
-3.500 0.1123 0.01836 0.01331 -0.1013 0.8785 0.0564
-3.250 0.1432 0.01977 0.01448 -0.1008 0.8703 0.0603
-3.000 0.1620 0.01462 0.00888 -0.0987 0.8608 0.0456
-2.750 0.1884 0.01361 0.00769 -0.0981 0.8525 0.0454
-2.500 0.2137 0.01263 0.00656 -0.0973 0.8427 0.0447
-2.250 0.2391 0.01194 0.00577 -0.0966 0.8325 0.0447
-2.000 0.2652 0.01137 0.00510 -0.0959 0.8222 0.0449
-1.750 0.2908 0.01088 0.00454 -0.0953 0.8114 0.0452
-1.500 0.3158 0.01049 0.00409 -0.0945 0.7995 0.0458
-1.250 0.3411 0.01025 0.00379 -0.0937 0.7875 0.0470
-1.000 0.3663 0.01001 0.00349 -0.0930 0.7751 0.0478
-0.750 0.3912 0.00977 0.00319 -0.0922 0.7626 0.0484
-0.500 0.4143 0.00933 0.00267 -0.0911 0.7498 0.0501
-0.250 0.4383 0.00912 0.00240 -0.0902 0.7357 0.0522
0.000 0.4627 0.00902 0.00224 -0.0893 0.7211 0.0546
0.250 0.4870 0.00895 0.00211 -0.0884 0.7057 0.0579
0.500 0.5113 0.00888 0.00199 -0.0875 0.6892 0.0628
0.750 0.5350 0.00880 0.00189 -0.0865 0.6703 0.0770
1.000 0.5339 0.00679 0.00204 -0.0809 0.6523 0.8224
1.250 0.6560 0.00700 0.00218 -0.1013 0.6010 1.0000
1.500 0.6736 0.00723 0.00220 -0.0991 0.5688 1.0000
1.750 0.6920 0.00746 0.00227 -0.0971 0.5438 1.0000
2.000 0.7115 0.00768 0.00235 -0.0954 0.5235 1.0000
2.250 0.7317 0.00788 0.00244 -0.0938 0.5053 1.0000
2.500 0.7523 0.00808 0.00254 -0.0923 0.4882 1.0000
2.750 0.7729 0.00828 0.00265 -0.0908 0.4707 1.0000
3.000 0.7935 0.00848 0.00276 -0.0893 0.4530 1.0000
3.250 0.8142 0.00869 0.00288 -0.0879 0.4346 1.0000
3.500 0.8350 0.00890 0.00300 -0.0864 0.4158 1.0000
3.750 0.8556 0.00913 0.00315 -0.0850 0.3980 1.0000
4.000 0.8763 0.00937 0.00330 -0.0836 0.3819 1.0000
4.250 0.8970 0.00961 0.00347 -0.0822 0.3677 1.0000
4.500 0.9178 0.00986 0.00365 -0.0808 0.3546 1.0000
4.750 0.9384 0.01011 0.00385 -0.0794 0.3419 1.0000
5.000 0.9589 0.01038 0.00404 -0.0780 0.3293 1.0000
5.250 0.9793 0.01065 0.00424 -0.0766 0.3154 1.0000
5.500 1.0005 0.01089 0.00444 -0.0753 0.3046 1.0000
5.750 1.0223 0.01110 0.00465 -0.0742 0.2955 1.0000
6.000 1.0429 0.01138 0.00487 -0.0729 0.2864 1.0000
6.250 1.0650 0.01158 0.00508 -0.0718 0.2778 1.0000
6.500 1.0861 0.01182 0.00532 -0.0706 0.2685 1.0000
6.750 1.1064 0.01210 0.00555 -0.0693 0.2569 1.0000
7.000 1.1272 0.01236 0.00577 -0.0681 0.2449 1.0000
7.250 1.1474 0.01264 0.00602 -0.0668 0.2311 1.0000
7.500 1.1664 0.01299 0.00631 -0.0652 0.2147 1.0000
7.750 1.1838 0.01342 0.00662 -0.0635 0.1893 1.0000
8.000 1.1912 0.01436 0.00719 -0.0601 0.1337 1.0000
8.750 1.2045 0.01787 0.01001 -0.0487 0.0201 1.0000
9.000 1.2191 0.01845 0.01068 -0.0466 0.0190 1.0000
9.250 1.2320 0.01914 0.01146 -0.0443 0.0179 1.0000
9.500 1.2422 0.02002 0.01243 -0.0417 0.0167 1.0000
9.750 1.2521 0.02090 0.01341 -0.0392 0.0160 1.0000
10.000 1.2629 0.02173 0.01433 -0.0369 0.0156 1.0000
10.250 1.2723 0.02267 0.01536 -0.0345 0.0151 1.0000
10.500 1.2798 0.02373 0.01651 -0.0321 0.0148 1.0000
10.750 1.2853 0.02496 0.01783 -0.0295 0.0144 1.0000
11.000 1.2896 0.02631 0.01927 -0.0271 0.0140 1.0000
11.250 1.2911 0.02791 0.02096 -0.0246 0.0137 1.0000
11.500 1.2929 0.02957 0.02271 -0.0224 0.0135 1.0000
11.750 1.2931 0.03146 0.02469 -0.0203 0.0134 1.0000
12.000 1.2905 0.03369 0.02701 -0.0183 0.0132 1.0000
12.250 1.2860 0.03623 0.02965 -0.0166 0.0130 1.0000
12.500 1.2791 0.03916 0.03267 -0.0151 0.0128 1.0000
12.750 1.2693 0.04250 0.03609 -0.0137 0.0125 1.0000
13.000 1.2634 0.04558 0.03923 -0.0124 0.0123 1.0000
13.250 1.2684 0.04772 0.04149 -0.0121 0.0122 1.0000
13.500 1.2714 0.05015 0.04402 -0.0119 0.0119 1.0000
13.750 1.2732 0.05273 0.04670 -0.0116 0.0118 1.0000
14.000 1.2743 0.05543 0.04948 -0.0113 0.0117 1.0000
14.250 1.2755 0.05814 0.05227 -0.0109 0.0116 1.0000
14.500 1.2773 0.06087 0.05511 -0.0108 0.0114 1.0000
14.750 1.2794 0.06358 0.05790 -0.0106 0.0113 1.0000
15.000 1.2820 0.06627 0.06068 -0.0105 0.0112 1.0000
15.250 1.2841 0.06905 0.06356 -0.0104 0.0111 1.0000
15.500 1.2867 0.07181 0.06641 -0.0103 0.0111 1.0000
15.750 1.2878 0.07487 0.06958 -0.0105 0.0109 1.0000
16.000 1.2898 0.07783 0.07265 -0.0104 0.0110 1.0000
16.250 1.2903 0.08107 0.07602 -0.0106 0.0110 1.0000
16.500 1.2905 0.08442 0.07950 -0.0108 0.0112 1.0000
16.750 1.2862 0.08858 0.08381 -0.0119 0.0111 1.0000
17.000 1.2815 0.09286 0.08824 -0.0133 0.0110 1.0000
17.250 1.2769 0.09720 0.09274 -0.0143 0.0113 1.0000
17.500 1.2688 0.10222 0.09790 -0.0165 0.0112 1.0000
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