GOE 284 AIRFOIL (goe284-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 284 AIRFOIL (goe284-il) Reynolds number: 1,000,000 Max Cl/Cd: 126.47 at α=5.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe284-il-1000000.txt Download as CSV file: xf-goe284-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: GOE 284 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
------ -------- --------- --------- -------- -------- --------
-17.000 -0.9089 0.08231 0.07935 -0.0568 1.0000 0.0301
-16.750 -0.9416 0.07401 0.07095 -0.0622 1.0000 0.0301
-16.500 -0.9867 0.06389 0.06069 -0.0691 1.0000 0.0301
-16.250 -1.0397 0.05184 0.04844 -0.0781 1.0000 0.0300
-16.000 -1.0738 0.04033 0.03666 -0.0894 1.0000 0.0299
-15.750 -1.0857 0.03405 0.03020 -0.0964 1.0000 0.0300
-15.500 -1.0886 0.03082 0.02685 -0.0987 1.0000 0.0301
-15.250 -1.0870 0.02874 0.02468 -0.0989 1.0000 0.0303
-15.000 -1.0757 0.02715 0.02298 -0.0992 0.9785 0.0304
-14.750 -1.0702 0.02603 0.02176 -0.0972 0.9630 0.0306
-14.500 -1.0610 0.02505 0.02068 -0.0953 0.9512 0.0308
-14.250 -1.0480 0.02412 0.01966 -0.0938 0.9408 0.0310
-14.000 -1.0328 0.02327 0.01872 -0.0925 0.9318 0.0312
-13.750 -1.0160 0.02247 0.01783 -0.0913 0.9223 0.0314
-13.500 -0.9971 0.02172 0.01699 -0.0904 0.9132 0.0316
-13.250 -0.9776 0.02104 0.01621 -0.0894 0.9031 0.0318
-13.000 -0.9562 0.02039 0.01547 -0.0886 0.8926 0.0320
-12.750 -0.9345 0.01981 0.01479 -0.0878 0.8812 0.0322
-12.500 -0.9121 0.01922 0.01411 -0.0872 0.8680 0.0323
-12.250 -0.8921 0.01833 0.01311 -0.0863 0.8540 0.0328
-12.000 -0.8701 0.01764 0.01232 -0.0856 0.8385 0.0331
-11.750 -0.8467 0.01706 0.01164 -0.0851 0.8207 0.0336
-11.500 -0.8223 0.01658 0.01104 -0.0846 0.8006 0.0340
-11.250 -0.7973 0.01615 0.01049 -0.0842 0.7786 0.0345
-11.000 -0.7718 0.01576 0.00997 -0.0838 0.7557 0.0349
-10.750 -0.7458 0.01541 0.00949 -0.0835 0.7333 0.0353
-10.500 -0.7194 0.01508 0.00904 -0.0833 0.7123 0.0357
-10.250 -0.6926 0.01479 0.00862 -0.0831 0.6927 0.0361
-10.000 -0.6663 0.01439 0.00811 -0.0829 0.6750 0.0368
-9.750 -0.6398 0.01398 0.00762 -0.0827 0.6591 0.0376
-9.500 -0.6127 0.01366 0.00721 -0.0826 0.6443 0.0385
-9.250 -0.5852 0.01336 0.00683 -0.0825 0.6316 0.0394
-9.000 -0.5573 0.01310 0.00650 -0.0824 0.6206 0.0403
-8.750 -0.5299 0.01275 0.00609 -0.0823 0.6105 0.0421
-8.500 -0.5022 0.01243 0.00574 -0.0823 0.6019 0.0446
-8.250 -0.4747 0.01203 0.00535 -0.0822 0.5944 0.0505
-8.000 -0.4470 0.01173 0.00510 -0.0822 0.5867 0.0641
-7.750 -0.4177 0.01164 0.00503 -0.0823 0.5812 0.0719
-7.500 -0.3882 0.01159 0.00498 -0.0825 0.5755 0.0760
-7.250 -0.3585 0.01160 0.00495 -0.0826 0.5699 0.0790
-7.000 -0.3290 0.01158 0.00487 -0.0828 0.5648 0.0810
-6.750 -0.2994 0.01150 0.00481 -0.0829 0.5616 0.0832
-6.500 -0.2697 0.01148 0.00477 -0.0831 0.5579 0.0849
-6.250 -0.2399 0.01146 0.00473 -0.0833 0.5542 0.0866
-6.000 -0.2102 0.01148 0.00468 -0.0834 0.5504 0.0878
-5.750 -0.1812 0.01141 0.00456 -0.0836 0.5462 0.0892
-5.500 -0.1518 0.01126 0.00444 -0.0837 0.5443 0.0910
-5.250 -0.1220 0.01121 0.00440 -0.0839 0.5421 0.0925
-5.000 -0.0922 0.01116 0.00434 -0.0841 0.5397 0.0938
-4.750 -0.0626 0.01112 0.00427 -0.0843 0.5371 0.0952
-4.500 -0.0329 0.01109 0.00421 -0.0845 0.5345 0.0963
-4.250 -0.0032 0.01109 0.00417 -0.0847 0.5316 0.0970
-4.000 0.0254 0.01090 0.00395 -0.0848 0.5284 0.0986
-3.750 0.0546 0.01078 0.00383 -0.0850 0.5262 0.1001
-3.500 0.0843 0.01068 0.00375 -0.0852 0.5249 0.1014
-3.250 0.1141 0.01062 0.00369 -0.0854 0.5233 0.1029
-3.000 0.1438 0.01055 0.00363 -0.0856 0.5212 0.1043
-2.750 0.1736 0.01049 0.00355 -0.0859 0.5186 0.1055
-2.500 0.2033 0.01046 0.00350 -0.0861 0.5156 0.1066
-2.250 0.2325 0.01037 0.00338 -0.0863 0.5124 0.1081
-2.000 0.2614 0.01029 0.00327 -0.0864 0.5086 0.1101
-1.750 0.2910 0.01020 0.00320 -0.0866 0.5066 0.1117
-1.500 0.3209 0.01010 0.00312 -0.0869 0.5043 0.1133
-1.250 0.3507 0.01003 0.00306 -0.0872 0.5013 0.1149
-1.000 0.3804 0.00997 0.00300 -0.0874 0.4984 0.1164
-0.750 0.4100 0.00995 0.00295 -0.0877 0.4958 0.1177
-0.500 0.4394 0.00991 0.00290 -0.0879 0.4933 0.1196
-0.250 0.4686 0.00989 0.00287 -0.0881 0.4905 0.1228
0.000 0.4981 0.00986 0.00286 -0.0883 0.4884 0.1256
0.250 0.5279 0.00981 0.00284 -0.0886 0.4869 0.1284
0.500 0.5577 0.00977 0.00281 -0.0889 0.4848 0.1314
0.750 0.5873 0.00969 0.00279 -0.0892 0.4824 0.1384
1.000 0.6169 0.00965 0.00278 -0.0895 0.4800 0.1462
1.250 0.6461 0.00956 0.00278 -0.0897 0.4775 0.1693
1.500 0.6747 0.00938 0.00281 -0.0900 0.4748 0.2464
1.750 0.7032 0.00929 0.00288 -0.0902 0.4715 0.3095
2.000 0.7321 0.00909 0.00293 -0.0905 0.4695 0.3879
2.250 0.7602 0.00868 0.00299 -0.0908 0.4673 0.5485
2.500 0.7869 0.00825 0.00307 -0.0907 0.4647 0.7249
2.750 0.8108 0.00793 0.00318 -0.0896 0.4617 0.8642
3.000 0.8344 0.00786 0.00326 -0.0883 0.4585 0.9458
3.250 0.8704 0.00795 0.00333 -0.0899 0.4543 0.9819
3.500 0.9130 0.00801 0.00339 -0.0931 0.4508 0.9979
3.750 0.9443 0.00806 0.00343 -0.0938 0.4465 1.0000
4.000 0.9712 0.00813 0.00347 -0.0936 0.4409 1.0000
4.250 0.9979 0.00825 0.00353 -0.0934 0.4349 1.0000
4.500 1.0258 0.00831 0.00359 -0.0934 0.4283 1.0000
4.750 1.0525 0.00845 0.00367 -0.0932 0.4196 1.0000
5.000 1.0801 0.00856 0.00375 -0.0932 0.4104 1.0000
5.250 1.1066 0.00875 0.00387 -0.0931 0.3980 1.0000
5.500 1.1323 0.00899 0.00402 -0.0928 0.3815 1.0000
5.750 1.1570 0.00930 0.00423 -0.0924 0.3639 1.0000
6.000 1.1814 0.00964 0.00447 -0.0920 0.3480 1.0000
6.250 1.2054 0.00999 0.00474 -0.0915 0.3345 1.0000
6.500 1.2297 0.01032 0.00500 -0.0910 0.3234 1.0000
6.750 1.2544 0.01061 0.00525 -0.0907 0.3150 1.0000
7.000 1.2781 0.01094 0.00553 -0.0901 0.3067 1.0000
7.250 1.3026 0.01121 0.00578 -0.0897 0.2999 1.0000
7.500 1.3261 0.01153 0.00606 -0.0892 0.2930 1.0000
7.750 1.3491 0.01185 0.00636 -0.0886 0.2870 1.0000
8.000 1.3735 0.01209 0.00660 -0.0882 0.2829 1.0000
8.250 1.3964 0.01239 0.00689 -0.0875 0.2783 1.0000
8.500 1.4172 0.01277 0.00723 -0.0866 0.2731 1.0000
8.750 1.4397 0.01303 0.00751 -0.0859 0.2695 1.0000
9.000 1.4609 0.01332 0.00780 -0.0850 0.2654 1.0000
9.250 1.4783 0.01370 0.00817 -0.0834 0.2611 1.0000
9.500 1.4938 0.01418 0.00864 -0.0817 0.2564 1.0000
9.750 1.5141 0.01450 0.00899 -0.0807 0.2539 1.0000
10.000 1.5336 0.01488 0.00939 -0.0797 0.2508 1.0000
10.250 1.5514 0.01536 0.00987 -0.0785 0.2472 1.0000
10.500 1.5673 0.01595 0.01046 -0.0772 0.2433 1.0000
10.750 1.5837 0.01654 0.01106 -0.0760 0.2399 1.0000
11.000 1.6030 0.01700 0.01156 -0.0752 0.2374 1.0000
11.250 1.6205 0.01757 0.01216 -0.0742 0.2343 1.0000
11.500 1.6358 0.01828 0.01289 -0.0731 0.2309 1.0000
11.750 1.6488 0.01918 0.01378 -0.0718 0.2270 1.0000
12.000 1.6647 0.01992 0.01456 -0.0709 0.2240 1.0000
12.250 1.6809 0.02067 0.01534 -0.0701 0.2206 1.0000
12.500 1.6934 0.02169 0.01638 -0.0690 0.2163 1.0000
12.750 1.7022 0.02303 0.01771 -0.0677 0.2115 1.0000
13.000 1.7165 0.02400 0.01873 -0.0670 0.2078 1.0000
13.250 1.7267 0.02531 0.02007 -0.0660 0.2024 1.0000
13.500 1.7318 0.02709 0.02185 -0.0649 0.1966 1.0000
13.750 1.7407 0.02861 0.02339 -0.0640 0.1897 1.0000
14.000 1.7401 0.03099 0.02575 -0.0628 0.1791 1.0000
14.250 1.7275 0.03451 0.02920 -0.0612 0.1592 1.0000
14.500 1.6920 0.04035 0.03489 -0.0591 0.1308 1.0000
14.750 1.6730 0.04480 0.03931 -0.0578 0.1192 1.0000
15.000 1.6624 0.04852 0.04304 -0.0569 0.1131 1.0000
15.250 1.6578 0.05168 0.04625 -0.0564 0.1096 1.0000
15.500 1.6520 0.05505 0.04966 -0.0558 0.1065 1.0000
15.750 1.6466 0.05838 0.05303 -0.0554 0.1033 1.0000
16.000 1.6475 0.06106 0.05576 -0.0551 0.1012 1.0000
16.250 1.6448 0.06420 0.05896 -0.0549 0.0991 1.0000
16.500 1.6420 0.06734 0.06214 -0.0546 0.0969 1.0000
16.750 1.6360 0.07091 0.06575 -0.0545 0.0946 1.0000
17.000 1.6374 0.07362 0.06853 -0.0544 0.0930 1.0000
17.250 1.6379 0.07651 0.07148 -0.0544 0.0914 1.0000
17.500 1.6381 0.07940 0.07442 -0.0544 0.0894 1.0000
17.750 1.6331 0.08298 0.07804 -0.0545 0.0873 1.0000
18.000 1.6280 0.08655 0.08166 -0.0547 0.0849 1.0000
18.250 1.6286 0.08949 0.08467 -0.0549 0.0830 1.0000
18.500 1.6278 0.09260 0.08782 -0.0551 0.0801 1.0000
18.750 1.6201 0.09666 0.09190 -0.0555 0.0770 1.0000
19.000 1.6184 0.09991 0.09520 -0.0559 0.0736 1.0000
19.250 1.6082 0.10433 0.09965 -0.0566 0.0690 1.0000
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