GOE 601 AIRFOIL (goe601-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 601 AIRFOIL (goe601-il) Reynolds number: 500,000 Max Cl/Cd: 82.81 at α=3.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe601-il-500000.txt Download as CSV file: xf-goe601-il-500000.csv |
XFOIL Version 6.96
Calculated polar for: GOE 601 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
------ -------- --------- --------- -------- -------- --------
-18.750 -0.7391 0.11949 0.11638 -0.0596 1.0000 0.0267
-18.500 -0.7974 0.10438 0.10101 -0.0687 1.0000 0.0266
-18.250 -0.8330 0.09434 0.09078 -0.0749 1.0000 0.0266
-18.000 -0.8600 0.08636 0.08260 -0.0799 1.0000 0.0267
-17.750 -0.8821 0.07972 0.07581 -0.0833 1.0000 0.0267
-17.500 -0.9004 0.07413 0.07010 -0.0858 1.0000 0.0271
-17.250 -0.9121 0.06962 0.06548 -0.0878 1.0000 0.0272
-17.000 -0.9155 0.06647 0.06230 -0.0887 1.0000 0.0275
-16.750 -0.9213 0.06309 0.05886 -0.0899 1.0000 0.0278
-16.500 -0.9274 0.05982 0.05552 -0.0910 1.0000 0.0280
-16.250 -0.9345 0.05657 0.05218 -0.0919 1.0000 0.0283
-16.000 -0.9418 0.05343 0.04895 -0.0925 1.0000 0.0285
-15.750 -0.9483 0.05053 0.04594 -0.0928 1.0000 0.0287
-15.500 -0.9525 0.04809 0.04343 -0.0929 1.0000 0.0291
-15.250 -0.9580 0.04564 0.04088 -0.0926 1.0000 0.0294
-15.000 -0.9639 0.04334 0.03848 -0.0919 1.0000 0.0297
-14.750 -0.9702 0.04121 0.03624 -0.0908 1.0000 0.0300
-14.500 -0.9769 0.03931 0.03423 -0.0894 1.0000 0.0303
-14.250 -0.9833 0.03761 0.03242 -0.0875 1.0000 0.0306
-14.000 -0.9918 0.03611 0.03080 -0.0851 1.0000 0.0309
-13.750 -1.0003 0.03485 0.02942 -0.0822 1.0000 0.0311
-13.500 -1.0009 0.03302 0.02755 -0.0796 1.0000 0.0315
-13.250 -1.0027 0.03176 0.02627 -0.0767 1.0000 0.0319
-13.000 -0.9976 0.03062 0.02511 -0.0750 0.9994 0.0323
-12.750 -0.9729 0.02933 0.02377 -0.0769 0.9968 0.0329
-12.500 -0.9472 0.02820 0.02257 -0.0788 0.9941 0.0337
-12.250 -0.9237 0.02705 0.02133 -0.0800 0.9908 0.0344
-12.000 -0.8986 0.02609 0.02026 -0.0813 0.9872 0.0352
-11.750 -0.8701 0.02526 0.01931 -0.0830 0.9843 0.0358
-11.500 -0.8428 0.02366 0.01768 -0.0847 0.9824 0.0368
-11.250 -0.8222 0.02261 0.01663 -0.0847 0.9767 0.0375
-11.000 -0.7945 0.02175 0.01574 -0.0860 0.9732 0.0385
-10.750 -0.7633 0.02094 0.01488 -0.0877 0.9709 0.0396
-10.500 -0.7305 0.02010 0.01397 -0.0897 0.9693 0.0405
-10.250 -0.7102 0.01944 0.01324 -0.0889 0.9618 0.0412
-10.000 -0.6818 0.01830 0.01207 -0.0902 0.9587 0.0424
-9.750 -0.6493 0.01737 0.01113 -0.0921 0.9566 0.0438
-9.500 -0.6264 0.01675 0.01048 -0.0918 0.9495 0.0449
-9.250 -0.5979 0.01612 0.00980 -0.0924 0.9442 0.0462
-9.000 -0.5660 0.01553 0.00914 -0.0938 0.9406 0.0475
-8.750 -0.5514 0.01490 0.00849 -0.0916 0.9295 0.0490
-8.500 -0.5238 0.01430 0.00786 -0.0920 0.9243 0.0513
-8.250 -0.5070 0.01393 0.00745 -0.0900 0.9130 0.0534
-8.000 -0.4834 0.01344 0.00692 -0.0894 0.9057 0.0565
-7.750 -0.4628 0.01302 0.00650 -0.0881 0.8966 0.0611
-7.500 -0.4398 0.01257 0.00610 -0.0874 0.8894 0.0720
-7.250 -0.4158 0.01232 0.00592 -0.0868 0.8815 0.0913
-7.000 -0.3872 0.01213 0.00571 -0.0870 0.8759 0.1032
-6.750 -0.3658 0.01188 0.00546 -0.0859 0.8681 0.1104
-6.500 -0.3390 0.01172 0.00523 -0.0858 0.8621 0.1164
-6.250 -0.3150 0.01151 0.00497 -0.0851 0.8562 0.1215
-6.000 -0.2923 0.01128 0.00473 -0.0842 0.8498 0.1269
-5.750 -0.2658 0.01112 0.00449 -0.0840 0.8446 0.1319
-5.500 -0.2429 0.01091 0.00429 -0.0831 0.8392 0.1383
-5.250 -0.2198 0.01070 0.00409 -0.0822 0.8336 0.1459
-5.000 -0.1956 0.01045 0.00387 -0.0816 0.8286 0.1605
-4.750 -0.1743 0.01007 0.00367 -0.0806 0.8238 0.2039
-4.500 -0.1536 0.00974 0.00355 -0.0794 0.8186 0.2565
-4.250 -0.1297 0.00953 0.00343 -0.0786 0.8139 0.2890
-4.000 -0.1037 0.00939 0.00332 -0.0783 0.8095 0.3143
-3.750 -0.0814 0.00921 0.00324 -0.0773 0.8040 0.3405
-3.500 -0.0585 0.00901 0.00315 -0.0763 0.7984 0.3700
-3.250 -0.0339 0.00887 0.00309 -0.0756 0.7930 0.4049
-3.000 -0.0099 0.00879 0.00310 -0.0748 0.7878 0.4367
-2.750 0.0146 0.00874 0.00308 -0.0740 0.7822 0.4588
-2.500 0.0409 0.00871 0.00304 -0.0736 0.7773 0.4745
-2.250 0.0684 0.00872 0.00301 -0.0735 0.7728 0.4880
-2.000 0.0929 0.00869 0.00299 -0.0727 0.7674 0.5009
-1.750 0.1183 0.00863 0.00296 -0.0721 0.7621 0.5133
-1.500 0.1453 0.00859 0.00291 -0.0718 0.7571 0.5258
-1.250 0.1706 0.00858 0.00289 -0.0712 0.7518 0.5366
-1.000 0.1956 0.00850 0.00286 -0.0706 0.7463 0.5463
-0.750 0.2223 0.00847 0.00280 -0.0702 0.7411 0.5563
-0.500 0.2478 0.00841 0.00279 -0.0697 0.7356 0.5671
-0.250 0.2722 0.00835 0.00276 -0.0689 0.7292 0.5780
0.000 0.2983 0.00830 0.00272 -0.0684 0.7234 0.5900
0.250 0.3230 0.00825 0.00271 -0.0676 0.7173 0.6024
0.500 0.3468 0.00817 0.00270 -0.0667 0.7099 0.6169
0.750 0.3718 0.00812 0.00267 -0.0660 0.7032 0.6360
1.000 0.3942 0.00804 0.00269 -0.0647 0.6953 0.6566
1.250 0.4185 0.00799 0.00268 -0.0639 0.6888 0.6797
1.500 0.4411 0.00793 0.00272 -0.0627 0.6811 0.7031
1.750 0.4637 0.00786 0.00272 -0.0614 0.6728 0.7298
2.000 0.4854 0.00779 0.00277 -0.0600 0.6638 0.7599
2.250 0.5072 0.00772 0.00281 -0.0585 0.6548 0.7969
2.500 0.5296 0.00767 0.00290 -0.0571 0.6448 0.8346
2.750 0.5549 0.00768 0.00298 -0.0563 0.6339 0.8693
3.000 0.5839 0.00775 0.00309 -0.0564 0.6205 0.9012
3.250 0.6209 0.00791 0.00325 -0.0583 0.6039 0.9240
3.500 0.6591 0.00811 0.00342 -0.0604 0.5846 0.9410
3.750 0.6931 0.00837 0.00360 -0.0617 0.5583 0.9543
4.000 0.7250 0.00880 0.00383 -0.0628 0.5167 0.9638
4.250 0.7530 0.00939 0.00416 -0.0631 0.4616 0.9730
4.500 0.7779 0.01014 0.00458 -0.0630 0.3992 0.9830
4.750 0.8095 0.01081 0.00499 -0.0645 0.3569 0.9898
5.000 0.8432 0.01131 0.00534 -0.0662 0.3351 0.9958
5.500 0.8835 0.01182 0.00575 -0.0639 0.3127 1.0000
5.750 0.8848 0.01198 0.00588 -0.0587 0.3060 1.0000
6.000 0.8900 0.01219 0.00606 -0.0544 0.2999 1.0000
6.250 0.9007 0.01236 0.00623 -0.0511 0.2930 1.0000
6.500 0.9103 0.01263 0.00647 -0.0477 0.2868 1.0000
6.750 0.9234 0.01286 0.00670 -0.0449 0.2810 1.0000
7.000 0.9379 0.01309 0.00693 -0.0425 0.2744 1.0000
7.250 0.9495 0.01345 0.00724 -0.0397 0.2676 1.0000
7.500 0.9672 0.01365 0.00747 -0.0379 0.2602 1.0000
7.750 0.9813 0.01398 0.00778 -0.0356 0.2532 1.0000
8.000 0.9979 0.01426 0.00808 -0.0337 0.2468 1.0000
8.250 1.0136 0.01460 0.00840 -0.0318 0.2381 1.0000
8.500 1.0296 0.01494 0.00874 -0.0299 0.2283 1.0000
8.750 1.0440 0.01538 0.00912 -0.0279 0.2156 1.0000
9.000 1.0567 0.01591 0.00957 -0.0257 0.1955 1.0000
9.250 1.0652 0.01669 0.01018 -0.0230 0.1665 1.0000
9.500 1.0586 0.01832 0.01138 -0.0186 0.1037 1.0000
9.750 1.0507 0.02021 0.01293 -0.0142 0.0553 1.0000
10.000 1.0602 0.02117 0.01385 -0.0121 0.0473 1.0000
10.250 1.0710 0.02210 0.01476 -0.0103 0.0437 1.0000
10.500 1.0837 0.02292 0.01564 -0.0087 0.0420 1.0000
10.750 1.0953 0.02385 0.01660 -0.0071 0.0404 1.0000
11.000 1.1059 0.02486 0.01764 -0.0055 0.0391 1.0000
11.250 1.1138 0.02609 0.01890 -0.0037 0.0379 1.0000
11.500 1.1237 0.02720 0.02007 -0.0022 0.0371 1.0000
11.750 1.1338 0.02833 0.02126 -0.0008 0.0365 1.0000
12.000 1.1429 0.02955 0.02254 0.0006 0.0358 1.0000
12.250 1.1510 0.03087 0.02392 0.0019 0.0353 1.0000
12.500 1.1579 0.03233 0.02544 0.0033 0.0347 1.0000
12.750 1.1634 0.03395 0.02711 0.0046 0.0340 1.0000
13.000 1.1656 0.03586 0.02907 0.0060 0.0333 1.0000
13.250 1.1666 0.03795 0.03122 0.0073 0.0329 1.0000
13.500 1.1633 0.04048 0.03381 0.0086 0.0323 1.0000
13.750 1.1699 0.04221 0.03562 0.0094 0.0320 1.0000
14.000 1.1748 0.04415 0.03764 0.0101 0.0317 1.0000
14.250 1.1791 0.04621 0.03977 0.0108 0.0314 1.0000
14.500 1.1828 0.04838 0.04201 0.0113 0.0310 1.0000
14.750 1.1866 0.05058 0.04429 0.0118 0.0305 1.0000
15.000 1.1899 0.05288 0.04665 0.0121 0.0300 1.0000
15.250 1.1924 0.05530 0.04913 0.0124 0.0297 1.0000
15.500 1.1942 0.05786 0.05174 0.0126 0.0292 1.0000
15.750 1.1963 0.06039 0.05432 0.0127 0.0289 1.0000
16.000 1.1974 0.06298 0.05695 0.0129 0.0285 1.0000
16.250 1.1999 0.06543 0.05943 0.0131 0.0282 1.0000
16.500 1.2029 0.06748 0.06149 0.0141 0.0276 1.0000
16.750 1.2077 0.06980 0.06388 0.0140 0.0275 1.0000
17.000 1.2109 0.07244 0.06662 0.0137 0.0272 1.0000
17.250 1.2132 0.07524 0.06952 0.0133 0.0268 1.0000
17.500 1.2167 0.07779 0.07215 0.0131 0.0265 1.0000
17.750 1.2189 0.08061 0.07505 0.0126 0.0261 1.0000
18.000 1.2217 0.08331 0.07783 0.0122 0.0257 1.0000
18.250 1.2242 0.08605 0.08063 0.0117 0.0254 1.0000
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