GOE 288 AIRFOIL (goe288-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 288 AIRFOIL (goe288-il) Reynolds number: 500,000 Max Cl/Cd: 96.46 at α=5.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe288-il-500000.txt Download as CSV file: xf-goe288-il-500000.csv |
XFOIL Version 6.96
Calculated polar for: GOE 288 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
------ -------- --------- --------- -------- -------- --------
-13.250 -0.6391 0.05939 0.05616 -0.0882 1.0000 0.0369
-13.000 -0.6945 0.05164 0.04824 -0.0919 1.0000 0.0366
-12.750 -0.7202 0.04472 0.04111 -0.0995 0.9959 0.0366
-12.500 -0.7086 0.03775 0.03384 -0.1141 0.9862 0.0368
-12.250 -0.6837 0.03429 0.03014 -0.1212 0.9816 0.0372
-12.000 -0.6620 0.03176 0.02740 -0.1249 0.9743 0.0375
-11.750 -0.6366 0.02958 0.02502 -0.1279 0.9684 0.0377
-11.500 -0.6145 0.02787 0.02314 -0.1293 0.9591 0.0380
-11.250 -0.5893 0.02636 0.02145 -0.1307 0.9513 0.0383
-11.000 -0.5675 0.02513 0.02006 -0.1309 0.9395 0.0385
-10.750 -0.5448 0.02407 0.01885 -0.1310 0.9274 0.0388
-10.500 -0.5214 0.02317 0.01778 -0.1309 0.9148 0.0390
-10.250 -0.4998 0.02179 0.01628 -0.1305 0.9013 0.0393
-10.000 -0.4774 0.02070 0.01513 -0.1302 0.8861 0.0398
-9.750 -0.4535 0.01989 0.01425 -0.1299 0.8706 0.0402
-9.500 -0.4289 0.01922 0.01350 -0.1297 0.8540 0.0407
-9.250 -0.4037 0.01863 0.01281 -0.1294 0.8362 0.0413
-9.000 -0.3783 0.01807 0.01212 -0.1292 0.8172 0.0419
-8.750 -0.3526 0.01753 0.01144 -0.1291 0.7971 0.0424
-8.500 -0.3266 0.01703 0.01079 -0.1289 0.7765 0.0429
-8.250 -0.3003 0.01658 0.01019 -0.1287 0.7563 0.0434
-8.000 -0.2735 0.01620 0.00965 -0.1286 0.7374 0.0439
-7.750 -0.2471 0.01562 0.00896 -0.1286 0.7207 0.0445
-7.500 -0.2203 0.01507 0.00834 -0.1287 0.7063 0.0454
-7.250 -0.1929 0.01470 0.00787 -0.1288 0.6936 0.0463
-7.000 -0.1647 0.01436 0.00745 -0.1290 0.6821 0.0473
-6.750 -0.1364 0.01406 0.00706 -0.1291 0.6724 0.0484
-6.500 -0.1077 0.01382 0.00671 -0.1293 0.6632 0.0496
-6.250 -0.0795 0.01338 0.00622 -0.1296 0.6551 0.0514
-6.000 -0.0504 0.01308 0.00588 -0.1298 0.6470 0.0535
-5.750 -0.0216 0.01289 0.00558 -0.1300 0.6393 0.0557
-5.500 0.0076 0.01252 0.00521 -0.1303 0.6321 0.0596
-5.250 0.0367 0.01222 0.00489 -0.1306 0.6249 0.0663
-5.000 0.0656 0.01192 0.00462 -0.1309 0.6185 0.0861
-4.750 0.0952 0.01165 0.00446 -0.1313 0.6131 0.1101
-4.500 0.1246 0.01151 0.00433 -0.1315 0.6071 0.1243
-4.250 0.1538 0.01146 0.00422 -0.1317 0.6013 0.1352
-4.000 0.1833 0.01134 0.00411 -0.1320 0.5961 0.1458
-3.750 0.2129 0.01120 0.00398 -0.1322 0.5906 0.1559
-3.500 0.2423 0.01112 0.00387 -0.1325 0.5851 0.1669
-3.250 0.2715 0.01106 0.00378 -0.1327 0.5802 0.1807
-3.000 0.3012 0.01087 0.00370 -0.1330 0.5762 0.2008
-2.750 0.3308 0.01073 0.00364 -0.1333 0.5716 0.2301
-2.500 0.3602 0.01065 0.00363 -0.1336 0.5671 0.2634
-2.250 0.3894 0.01068 0.00367 -0.1338 0.5626 0.2876
-2.000 0.4191 0.01069 0.00371 -0.1340 0.5588 0.3058
-1.750 0.4487 0.01073 0.00375 -0.1342 0.5548 0.3211
-1.500 0.4782 0.01077 0.00380 -0.1344 0.5506 0.3334
-1.250 0.5074 0.01083 0.00381 -0.1345 0.5463 0.3422
-1.000 0.5366 0.01092 0.00386 -0.1346 0.5420 0.3504
-0.750 0.5662 0.01096 0.00388 -0.1348 0.5377 0.3579
-0.500 0.5954 0.01094 0.00390 -0.1350 0.5331 0.3656
-0.250 0.6244 0.01101 0.00392 -0.1351 0.5286 0.3726
0.000 0.6534 0.01112 0.00395 -0.1352 0.5241 0.3785
0.250 0.6826 0.01108 0.00399 -0.1353 0.5200 0.3850
0.500 0.7117 0.01112 0.00402 -0.1355 0.5151 0.3918
0.750 0.7404 0.01118 0.00403 -0.1355 0.5101 0.3977
1.000 0.7688 0.01123 0.00408 -0.1356 0.5049 0.4044
1.250 0.7978 0.01126 0.00413 -0.1357 0.4994 0.4131
1.500 0.8262 0.01128 0.00417 -0.1357 0.4933 0.4220
1.750 0.8541 0.01138 0.00423 -0.1357 0.4875 0.4294
2.000 0.8830 0.01140 0.00427 -0.1358 0.4812 0.4354
2.250 0.9109 0.01141 0.00431 -0.1358 0.4742 0.4419
2.500 0.9388 0.01148 0.00437 -0.1358 0.4672 0.4485
2.750 0.9668 0.01154 0.00442 -0.1358 0.4586 0.4553
3.000 0.9940 0.01161 0.00450 -0.1356 0.4498 0.4634
3.250 1.0211 0.01171 0.00458 -0.1355 0.4386 0.4719
3.500 1.0480 0.01180 0.00469 -0.1353 0.4263 0.4809
3.750 1.0740 0.01197 0.00482 -0.1350 0.4129 0.4918
4.000 1.0993 0.01216 0.00499 -0.1346 0.3991 0.5055
4.250 1.1243 0.01238 0.00519 -0.1342 0.3859 0.5234
4.500 1.1496 0.01257 0.00542 -0.1338 0.3749 0.5495
4.750 1.1739 0.01276 0.00570 -0.1334 0.3657 0.5963
5.000 1.1921 0.01236 0.00600 -0.1314 0.3585 0.8711
5.250 1.2151 0.01260 0.00622 -0.1305 0.3515 1.0000
5.500 1.2405 0.01286 0.00645 -0.1301 0.3461 1.0000
5.750 1.2648 0.01317 0.00672 -0.1296 0.3407 1.0000
6.000 1.2876 0.01356 0.00704 -0.1288 0.3356 1.0000
6.250 1.3118 0.01386 0.00733 -0.1282 0.3318 1.0000
6.500 1.3362 0.01413 0.00760 -0.1277 0.3283 1.0000
6.750 1.3595 0.01445 0.00791 -0.1270 0.3248 1.0000
7.000 1.3815 0.01482 0.00825 -0.1262 0.3215 1.0000
7.250 1.4021 0.01528 0.00866 -0.1250 0.3180 1.0000
7.500 1.4246 0.01559 0.00900 -0.1242 0.3156 1.0000
7.750 1.4469 0.01588 0.00933 -0.1234 0.3133 1.0000
8.000 1.4672 0.01620 0.00967 -0.1222 0.3108 1.0000
8.250 1.4868 0.01657 0.01005 -0.1209 0.3083 1.0000
8.500 1.5057 0.01699 0.01047 -0.1196 0.3057 1.0000
8.750 1.5240 0.01750 0.01096 -0.1182 0.3031 1.0000
9.000 1.5430 0.01805 0.01149 -0.1170 0.3000 1.0000
9.250 1.5625 0.01840 0.01192 -0.1158 0.2981 1.0000
9.500 1.5816 0.01880 0.01237 -0.1147 0.2957 1.0000
9.750 1.6004 0.01925 0.01286 -0.1135 0.2935 1.0000
10.000 1.6190 0.01974 0.01339 -0.1123 0.2915 1.0000
10.250 1.6368 0.02028 0.01395 -0.1111 0.2895 1.0000
10.500 1.6539 0.02088 0.01455 -0.1099 0.2872 1.0000
10.750 1.6716 0.02158 0.01523 -0.1087 0.2842 1.0000
11.000 1.6886 0.02214 0.01586 -0.1075 0.2825 1.0000
11.250 1.7049 0.02273 0.01654 -0.1063 0.2805 1.0000
11.500 1.7206 0.02337 0.01724 -0.1051 0.2779 1.0000
11.750 1.7355 0.02407 0.01800 -0.1039 0.2752 1.0000
12.000 1.7495 0.02486 0.01883 -0.1026 0.2725 1.0000
12.250 1.7630 0.02576 0.01971 -0.1013 0.2696 1.0000
12.500 1.7775 0.02662 0.02060 -0.1001 0.2669 1.0000
12.750 1.7909 0.02750 0.02160 -0.0990 0.2650 1.0000
13.000 1.8034 0.02848 0.02267 -0.0979 0.2622 1.0000
13.250 1.8155 0.02954 0.02380 -0.0969 0.2594 1.0000
13.500 1.8266 0.03069 0.02500 -0.0958 0.2566 1.0000
13.750 1.8361 0.03198 0.02630 -0.0946 0.2537 1.0000
14.000 1.8461 0.03327 0.02765 -0.0935 0.2508 1.0000
14.250 1.8559 0.03468 0.02918 -0.0927 0.2478 1.0000
14.500 1.8641 0.03625 0.03084 -0.0920 0.2438 1.0000
14.750 1.8690 0.03815 0.03276 -0.0910 0.2395 1.0000
15.000 1.8737 0.04008 0.03474 -0.0901 0.2358 1.0000
15.250 1.8829 0.04173 0.03651 -0.0896 0.2325 1.0000
15.500 1.8888 0.04371 0.03857 -0.0890 0.2283 1.0000
15.750 1.8898 0.04621 0.04110 -0.0883 0.2238 1.0000
16.000 1.8929 0.04854 0.04351 -0.0878 0.2194 1.0000
16.250 1.8957 0.05097 0.04603 -0.0873 0.2139 1.0000
16.500 1.8917 0.05413 0.04922 -0.0868 0.2086 1.0000
16.750 1.8929 0.05678 0.05195 -0.0864 0.2023 1.0000
17.000 1.8848 0.06051 0.05571 -0.0860 0.1950 1.0000
17.250 1.8785 0.06405 0.05931 -0.0856 0.1861 1.0000
17.500 1.8638 0.06865 0.06392 -0.0854 0.1758 1.0000
17.750 1.8434 0.07402 0.06929 -0.0853 0.1634 1.0000
18.000 1.8152 0.08042 0.07568 -0.0853 0.1486 1.0000
18.250 1.7811 0.08777 0.08300 -0.0857 0.1336 1.0000
18.500 1.7462 0.09540 0.09063 -0.0864 0.1208 1.0000
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