GOE 776 AIRFOIL (goe776-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 776 AIRFOIL (goe776-il) Reynolds number: 1,000,000 Max Cl/Cd: 61.39 at α=9.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe776-il-1000000-n5.txt Download as CSV file: xf-goe776-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 776 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 = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -1.2662 0.08140 0.07659 -0.0441 1.0000 0.0743
-19.500 -1.2711 0.07784 0.07298 -0.0449 1.0000 0.0757
-19.250 -1.2722 0.07480 0.06989 -0.0456 1.0000 0.0770
-19.000 -1.2780 0.07126 0.06629 -0.0464 1.0000 0.0784
-18.750 -1.2835 0.06774 0.06273 -0.0470 1.0000 0.0799
-18.500 -1.2842 0.06483 0.05977 -0.0475 1.0000 0.0815
-18.250 -1.2849 0.06191 0.05680 -0.0480 1.0000 0.0829
-18.000 -1.2832 0.05932 0.05415 -0.0483 1.0000 0.0841
-17.750 -1.2848 0.05641 0.05120 -0.0487 1.0000 0.0856
-17.500 -1.2858 0.05356 0.04832 -0.0489 1.0000 0.0872
-17.250 -1.2834 0.05112 0.04584 -0.0490 1.0000 0.0890
-17.000 -1.2795 0.04886 0.04354 -0.0491 1.0000 0.0906
-16.750 -1.2755 0.04664 0.04127 -0.0492 1.0000 0.0919
-16.500 -1.2727 0.04436 0.03896 -0.0491 1.0000 0.0937
-16.250 -1.2690 0.04218 0.03675 -0.0490 1.0000 0.0955
-16.000 -1.2627 0.04028 0.03482 -0.0488 1.0000 0.0972
-15.750 -1.2548 0.03857 0.03307 -0.0485 1.0000 0.0988
-15.500 -1.2483 0.03678 0.03124 -0.0482 1.0000 0.1005
-15.250 -1.2417 0.03504 0.02950 -0.0477 1.0000 0.1024
-15.000 -1.2344 0.03341 0.02784 -0.0472 1.0000 0.1043
-14.750 -1.2251 0.03200 0.02641 -0.0466 1.0000 0.1061
-14.500 -1.2149 0.03073 0.02510 -0.0460 1.0000 0.1077
-14.250 -1.2076 0.02933 0.02369 -0.0450 1.0000 0.1098
-14.000 -1.2002 0.02807 0.02243 -0.0438 1.0000 0.1119
-13.750 -1.1938 0.02693 0.02127 -0.0422 1.0000 0.1140
-13.500 -1.1778 0.02591 0.02023 -0.0421 0.9983 0.1161
-13.250 -1.1582 0.02477 0.01908 -0.0428 0.9953 0.1186
-13.000 -1.1381 0.02369 0.01800 -0.0435 0.9923 0.1215
-12.750 -1.1182 0.02272 0.01702 -0.0440 0.9882 0.1243
-12.500 -1.0976 0.02192 0.01621 -0.0442 0.9822 0.1267
-12.250 -1.0785 0.02096 0.01525 -0.0444 0.9761 0.1301
-12.000 -1.0616 0.02018 0.01447 -0.0437 0.9671 0.1333
-11.750 -1.0434 0.01948 0.01374 -0.0432 0.9582 0.1362
-11.500 -1.0279 0.01879 0.01304 -0.0421 0.9471 0.1393
-11.250 -1.0132 0.01810 0.01233 -0.0407 0.9357 0.1431
-11.000 -0.9969 0.01754 0.01174 -0.0395 0.9229 0.1465
-10.750 -0.9801 0.01699 0.01116 -0.0383 0.9109 0.1500
-10.500 -0.9644 0.01642 0.01056 -0.0369 0.8974 0.1543
-10.250 -0.9460 0.01596 0.01007 -0.0358 0.8835 0.1586
-10.000 -0.9289 0.01547 0.00955 -0.0346 0.8697 0.1632
-9.750 -0.9108 0.01504 0.00908 -0.0333 0.8543 0.1681
-9.250 -0.8726 0.01427 0.00823 -0.0312 0.8236 0.1772
-9.000 -0.8525 0.01396 0.00786 -0.0302 0.8077 0.1819
-8.750 -0.8313 0.01366 0.00753 -0.0293 0.7927 0.1861
-8.500 -0.8119 0.01333 0.00717 -0.0282 0.7785 0.1913
-8.250 -0.7906 0.01307 0.00687 -0.0273 0.7635 0.1963
-8.000 -0.7686 0.01283 0.00659 -0.0265 0.7499 0.2004
-7.750 -0.7482 0.01256 0.00629 -0.0254 0.7360 0.2058
-7.500 -0.7260 0.01234 0.00604 -0.0246 0.7227 0.2111
-7.250 -0.7039 0.01214 0.00580 -0.0237 0.7098 0.2160
-7.000 -0.6823 0.01190 0.00556 -0.0227 0.6968 0.2215
-6.750 -0.6595 0.01173 0.00535 -0.0219 0.6850 0.2265
-6.500 -0.6367 0.01156 0.00515 -0.0211 0.6723 0.2316
-6.250 -0.6149 0.01136 0.00494 -0.0201 0.6614 0.2381
-6.000 -0.5917 0.01121 0.00477 -0.0193 0.6498 0.2435
-5.750 -0.5693 0.01106 0.00460 -0.0183 0.6389 0.2490
-5.500 -0.5470 0.01091 0.00445 -0.0173 0.6284 0.2550
-5.250 -0.5253 0.01083 0.00433 -0.0161 0.6175 0.2605
-5.000 -0.5046 0.01070 0.00421 -0.0147 0.6080 0.2667
-4.750 -0.4838 0.01061 0.00410 -0.0133 0.5977 0.2732
-4.500 -0.4605 0.01054 0.00402 -0.0124 0.5891 0.2784
-4.250 -0.4377 0.01043 0.00391 -0.0114 0.5786 0.2854
-4.000 -0.4141 0.01035 0.00381 -0.0106 0.5688 0.2927
-3.750 -0.3896 0.01026 0.00373 -0.0099 0.5597 0.2995
-3.500 -0.3664 0.01019 0.00364 -0.0090 0.5490 0.3074
-3.250 -0.3412 0.01012 0.00357 -0.0084 0.5397 0.3140
-3.000 -0.3171 0.01006 0.00350 -0.0076 0.5291 0.3208
-2.750 -0.2924 0.01000 0.00344 -0.0070 0.5201 0.3281
-2.500 -0.2670 0.00998 0.00339 -0.0064 0.5092 0.3340
-2.250 -0.2427 0.00992 0.00333 -0.0057 0.4994 0.3413
-2.000 -0.2174 0.00988 0.00329 -0.0051 0.4897 0.3485
-1.750 -0.1921 0.00988 0.00326 -0.0046 0.4792 0.3544
-1.500 -0.1672 0.00982 0.00321 -0.0039 0.4699 0.3623
-1.000 -0.1162 0.00981 0.00317 -0.0029 0.4511 0.3759
-0.750 -0.0916 0.00979 0.00314 -0.0022 0.4413 0.3839
-0.500 -0.0658 0.00979 0.00313 -0.0017 0.4331 0.3914
-0.250 -0.0401 0.00978 0.00312 -0.0012 0.4246 0.3980
0.000 -0.0155 0.00978 0.00312 -0.0005 0.4159 0.4063
0.250 0.0109 0.00978 0.00312 -0.0001 0.4090 0.4138
0.500 0.0361 0.00977 0.00312 0.0005 0.4008 0.4217
0.750 0.0613 0.00979 0.00313 0.0011 0.3934 0.4304
1.000 0.0875 0.00979 0.00314 0.0015 0.3866 0.4383
1.250 0.1121 0.00980 0.00316 0.0021 0.3786 0.4481
1.500 0.1378 0.00983 0.00319 0.0027 0.3718 0.4570
1.750 0.1631 0.00982 0.00320 0.0032 0.3649 0.4667
2.000 0.1880 0.00986 0.00324 0.0039 0.3571 0.4767
2.250 0.2132 0.00988 0.00328 0.0044 0.3508 0.4865
2.500 0.2385 0.00990 0.00332 0.0050 0.3438 0.4968
2.750 0.2631 0.00997 0.00338 0.0057 0.3364 0.5060
3.000 0.2881 0.00999 0.00342 0.0063 0.3305 0.5173
3.250 0.3134 0.01005 0.00348 0.0068 0.3235 0.5264
3.500 0.3369 0.01011 0.00356 0.0077 0.3161 0.5368
3.750 0.3624 0.01017 0.00362 0.0082 0.3101 0.5466
4.000 0.3861 0.01023 0.00370 0.0090 0.3028 0.5569
4.250 0.4100 0.01033 0.00379 0.0098 0.2956 0.5666
4.500 0.4343 0.01040 0.00388 0.0106 0.2888 0.5758
4.750 0.4569 0.01051 0.00399 0.0116 0.2812 0.5867
5.000 0.4803 0.01060 0.00408 0.0125 0.2756 0.5953
5.250 0.5017 0.01066 0.00418 0.0137 0.2697 0.6056
5.500 0.5219 0.01080 0.00430 0.0152 0.2631 0.6155
5.750 0.5437 0.01088 0.00442 0.0164 0.2578 0.6259
6.000 0.5661 0.01101 0.00456 0.0174 0.2515 0.6366
6.250 0.5880 0.01119 0.00474 0.0184 0.2455 0.6470
6.500 0.6115 0.01131 0.00490 0.0192 0.2407 0.6589
6.750 0.6340 0.01150 0.00509 0.0201 0.2344 0.6696
7.000 0.6559 0.01169 0.00531 0.0211 0.2285 0.6826
7.250 0.6792 0.01186 0.00551 0.0218 0.2238 0.6942
7.500 0.7011 0.01207 0.00574 0.0227 0.2183 0.7073
7.750 0.7227 0.01230 0.00599 0.0236 0.2130 0.7199
8.000 0.7453 0.01250 0.00623 0.0244 0.2080 0.7338
8.250 0.7662 0.01275 0.00651 0.0254 0.2026 0.7472
8.500 0.7876 0.01302 0.00681 0.0263 0.1981 0.7609
8.750 0.8094 0.01325 0.00709 0.0272 0.1935 0.7759
9.000 0.8293 0.01358 0.00744 0.0282 0.1881 0.7899
9.250 0.8498 0.01389 0.00779 0.0292 0.1837 0.8052
9.500 0.8705 0.01418 0.00814 0.0301 0.1792 0.8206
9.750 0.8890 0.01459 0.00857 0.0312 0.1740 0.8361
10.000 0.9086 0.01495 0.00898 0.0323 0.1699 0.8521
10.250 0.9275 0.01535 0.00943 0.0334 0.1651 0.8670
10.750 0.9629 0.01630 0.01044 0.0357 0.1563 0.8953
11.000 0.9797 0.01682 0.01099 0.0369 0.1520 0.9084
11.250 0.9955 0.01742 0.01161 0.0382 0.1482 0.9210
11.500 1.0126 0.01794 0.01217 0.0394 0.1450 0.9336
11.750 1.0280 0.01858 0.01284 0.0407 0.1414 0.9451
12.000 1.0426 0.01931 0.01357 0.0419 0.1377 0.9567
12.250 1.0608 0.01999 0.01427 0.0425 0.1351 0.9657
12.500 1.0782 0.02073 0.01502 0.0432 0.1319 0.9750
12.750 1.0975 0.02164 0.01593 0.0430 0.1284 0.9812
13.000 1.1173 0.02251 0.01680 0.0428 0.1257 0.9875
13.250 1.1376 0.02341 0.01772 0.0424 0.1230 0.9920
13.500 1.1583 0.02446 0.01877 0.0417 0.1200 0.9950
13.750 1.1771 0.02564 0.01994 0.0410 0.1172 0.9981
14.000 1.1938 0.02665 0.02097 0.0410 0.1150 1.0000
14.250 1.2011 0.02772 0.02207 0.0426 0.1130 1.0000
14.500 1.2092 0.02893 0.02329 0.0437 0.1108 1.0000
14.750 1.2161 0.03036 0.02472 0.0447 0.1086 1.0000
15.000 1.2265 0.03161 0.02600 0.0454 0.1069 1.0000
15.250 1.2359 0.03302 0.02744 0.0459 0.1051 1.0000
15.500 1.2440 0.03457 0.02901 0.0465 0.1031 1.0000
15.750 1.2509 0.03628 0.03074 0.0469 0.1011 1.0000
16.000 1.2569 0.03813 0.03262 0.0473 0.0993 1.0000
16.250 1.2657 0.03975 0.03427 0.0475 0.0977 1.0000
16.500 1.2717 0.04168 0.03623 0.0477 0.0959 1.0000
16.750 1.2763 0.04376 0.03834 0.0478 0.0941 1.0000
17.000 1.2795 0.04602 0.04062 0.0479 0.0924 1.0000
17.250 1.2831 0.04829 0.04294 0.0478 0.0910 1.0000
17.500 1.2881 0.05042 0.04512 0.0478 0.0893 1.0000
17.750 1.2897 0.05294 0.04768 0.0476 0.0876 1.0000
18.000 1.2893 0.05571 0.05049 0.0474 0.0859 1.0000
18.250 1.2886 0.05853 0.05334 0.0471 0.0843 1.0000
18.500 1.2896 0.06123 0.05609 0.0467 0.0831 1.0000
18.750 1.2901 0.06399 0.05891 0.0463 0.0817 1.0000
19.000 1.2886 0.06701 0.06198 0.0458 0.0802 1.0000
19.250 1.2835 0.07048 0.06549 0.0451 0.0787 1.0000
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