GOE 433 AIRFOIL (goe433-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 433 AIRFOIL (goe433-il) Reynolds number: 1,000,000 Max Cl/Cd: 100.28 at α=3.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe433-il-1000000-n5.txt Download as CSV file: xf-goe433-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 433 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
------ -------- --------- --------- -------- -------- --------
-18.250 -0.9891 0.08637 0.08326 -0.0638 1.0000 0.0405
-18.000 -1.0118 0.07961 0.07641 -0.0681 1.0000 0.0410
-17.750 -1.0348 0.07292 0.06962 -0.0724 1.0000 0.0414
-17.500 -1.0579 0.06636 0.06296 -0.0767 1.0000 0.0418
-17.250 -1.0783 0.06029 0.05679 -0.0807 1.0000 0.0422
-17.000 -1.0972 0.05458 0.05097 -0.0846 1.0000 0.0425
-16.750 -1.1150 0.04905 0.04532 -0.0885 1.0000 0.0428
-16.500 -1.1275 0.04424 0.04042 -0.0919 1.0000 0.0431
-16.250 -1.1422 0.03917 0.03526 -0.0958 1.0000 0.0435
-16.000 -1.1446 0.03477 0.03076 -0.1006 0.9796 0.0440
-15.750 -1.1440 0.03109 0.02699 -0.1043 0.9570 0.0446
-15.500 -1.1419 0.02797 0.02374 -0.1072 0.9364 0.0452
-15.250 -1.1278 0.02524 0.02089 -0.1113 0.9192 0.0460
-15.000 -1.1065 0.02285 0.01837 -0.1160 0.9023 0.0469
-14.750 -1.0821 0.02133 0.01671 -0.1190 0.8860 0.0478
-14.500 -1.0588 0.02032 0.01558 -0.1204 0.8709 0.0487
-14.250 -1.0348 0.01944 0.01460 -0.1216 0.8577 0.0498
-14.000 -1.0095 0.01872 0.01382 -0.1224 0.8474 0.0506
-13.750 -0.9838 0.01812 0.01313 -0.1231 0.8378 0.0515
-13.500 -0.9573 0.01759 0.01252 -0.1237 0.8298 0.0524
-13.250 -0.9306 0.01711 0.01196 -0.1242 0.8227 0.0531
-13.000 -0.9033 0.01667 0.01145 -0.1247 0.8171 0.0536
-12.750 -0.8762 0.01612 0.01086 -0.1253 0.8120 0.0546
-12.500 -0.8487 0.01566 0.01036 -0.1257 0.8067 0.0556
-12.250 -0.8210 0.01527 0.00991 -0.1261 0.8015 0.0566
-12.000 -0.7929 0.01489 0.00950 -0.1266 0.7972 0.0576
-11.750 -0.7645 0.01455 0.00911 -0.1269 0.7924 0.0584
-11.500 -0.7361 0.01424 0.00874 -0.1273 0.7871 0.0592
-11.250 -0.7077 0.01394 0.00838 -0.1276 0.7817 0.0599
-11.000 -0.6791 0.01357 0.00798 -0.1280 0.7770 0.0610
-10.750 -0.6504 0.01324 0.00764 -0.1283 0.7707 0.0621
-10.500 -0.6217 0.01298 0.00733 -0.1286 0.7634 0.0633
-10.250 -0.5927 0.01272 0.00703 -0.1289 0.7566 0.0644
-10.000 -0.5636 0.01249 0.00675 -0.1292 0.7482 0.0653
-9.750 -0.5346 0.01229 0.00648 -0.1294 0.7398 0.0661
-9.500 -0.5056 0.01203 0.00618 -0.1297 0.7288 0.0671
-9.250 -0.4766 0.01179 0.00589 -0.1300 0.7163 0.0684
-9.000 -0.4478 0.01161 0.00563 -0.1302 0.6991 0.0698
-8.750 -0.4190 0.01146 0.00539 -0.1303 0.6799 0.0710
-8.500 -0.3901 0.01134 0.00518 -0.1305 0.6640 0.0721
-8.250 -0.3609 0.01121 0.00498 -0.1307 0.6525 0.0730
-8.000 -0.3317 0.01107 0.00478 -0.1309 0.6434 0.0741
-7.750 -0.3024 0.01089 0.00456 -0.1311 0.6338 0.0758
-7.500 -0.2732 0.01075 0.00437 -0.1314 0.6247 0.0774
-7.250 -0.2437 0.01062 0.00419 -0.1316 0.6172 0.0788
-7.000 -0.2143 0.01051 0.00403 -0.1318 0.6106 0.0801
-6.750 -0.1846 0.01041 0.00389 -0.1321 0.6061 0.0813
-6.500 -0.1547 0.01024 0.00371 -0.1323 0.6025 0.0834
-6.250 -0.1249 0.01009 0.00355 -0.1326 0.5989 0.0855
-6.000 -0.0951 0.00997 0.00341 -0.1329 0.5950 0.0875
-5.750 -0.0654 0.00987 0.00329 -0.1331 0.5909 0.0896
-5.500 -0.0357 0.00976 0.00316 -0.1334 0.5870 0.0927
-5.250 -0.0056 0.00962 0.00304 -0.1337 0.5848 0.0964
-5.000 0.0244 0.00951 0.00293 -0.1339 0.5819 0.1000
-4.750 0.0544 0.00938 0.00282 -0.1342 0.5784 0.1056
-4.500 0.0843 0.00929 0.00274 -0.1345 0.5748 0.1117
-4.250 0.1141 0.00919 0.00266 -0.1348 0.5714 0.1190
-4.000 0.1439 0.00913 0.00259 -0.1350 0.5678 0.1245
-3.750 0.1740 0.00905 0.00253 -0.1352 0.5650 0.1304
-3.500 0.2041 0.00900 0.00248 -0.1355 0.5618 0.1342
-3.250 0.2341 0.00891 0.00242 -0.1358 0.5581 0.1400
-3.000 0.2640 0.00887 0.00237 -0.1360 0.5545 0.1448
-2.750 0.2938 0.00885 0.00233 -0.1362 0.5506 0.1477
-2.500 0.3235 0.00882 0.00229 -0.1364 0.5466 0.1520
-2.250 0.3536 0.00875 0.00225 -0.1366 0.5430 0.1566
-2.000 0.3836 0.00872 0.00222 -0.1369 0.5384 0.1610
-1.750 0.4134 0.00870 0.00219 -0.1371 0.5338 0.1653
-1.500 0.4430 0.00868 0.00217 -0.1373 0.5289 0.1713
-1.250 0.4729 0.00865 0.00215 -0.1375 0.5244 0.1769
-1.000 0.5027 0.00862 0.00213 -0.1377 0.5182 0.1844
-0.500 0.5618 0.00855 0.00212 -0.1381 0.5056 0.2152
-0.250 0.5914 0.00851 0.00214 -0.1384 0.4984 0.2339
0.000 0.6205 0.00854 0.00216 -0.1385 0.4897 0.2497
0.250 0.6493 0.00858 0.00220 -0.1386 0.4752 0.2680
0.500 0.6779 0.00865 0.00225 -0.1386 0.4606 0.2834
0.750 0.7066 0.00873 0.00231 -0.1387 0.4507 0.2928
1.000 0.7353 0.00881 0.00237 -0.1388 0.4414 0.3030
1.250 0.7638 0.00891 0.00245 -0.1388 0.4305 0.3121
1.500 0.7917 0.00906 0.00255 -0.1387 0.4169 0.3234
1.750 0.8198 0.00917 0.00265 -0.1387 0.4047 0.3355
2.000 0.8481 0.00927 0.00275 -0.1387 0.3954 0.3526
2.250 0.8762 0.00937 0.00287 -0.1387 0.3854 0.3741
2.500 0.9043 0.00948 0.00299 -0.1387 0.3758 0.3966
2.750 0.9319 0.00963 0.00314 -0.1386 0.3649 0.4184
3.000 0.9598 0.00977 0.00328 -0.1386 0.3543 0.4334
3.250 0.9868 0.00998 0.00344 -0.1384 0.3419 0.4479
3.500 1.0139 0.01017 0.00361 -0.1382 0.3299 0.4601
3.750 1.0409 0.01038 0.00377 -0.1380 0.3176 0.4679
4.000 1.0667 0.01067 0.00399 -0.1376 0.3005 0.4756
4.250 1.0915 0.01103 0.00424 -0.1371 0.2795 0.4827
4.500 1.1151 0.01148 0.00456 -0.1364 0.2546 0.4892
4.750 1.1371 0.01202 0.00495 -0.1355 0.2251 0.4968
5.000 1.1515 0.01310 0.00569 -0.1335 0.1669 0.5025
5.500 1.1958 0.01401 0.00644 -0.1318 0.1367 0.5106
5.750 1.2179 0.01443 0.00680 -0.1308 0.1252 0.5150
6.000 1.2394 0.01487 0.00718 -0.1298 0.1136 0.5198
6.250 1.2596 0.01536 0.00759 -0.1287 0.1011 0.5244
6.750 1.2827 0.01694 0.00896 -0.1236 0.0537 0.5339
7.000 1.3013 0.01741 0.00944 -0.1222 0.0515 0.5398
7.250 1.3202 0.01787 0.00991 -0.1209 0.0499 0.5457
7.500 1.3393 0.01832 0.01040 -0.1197 0.0491 0.5536
7.750 1.3578 0.01881 0.01093 -0.1185 0.0484 0.5610
8.000 1.3756 0.01936 0.01150 -0.1172 0.0478 0.5680
8.250 1.3929 0.01994 0.01213 -0.1160 0.0472 0.5779
8.500 1.4096 0.02058 0.01281 -0.1147 0.0466 0.5876
8.750 1.4256 0.02128 0.01356 -0.1134 0.0461 0.5977
9.000 1.4412 0.02204 0.01436 -0.1121 0.0456 0.6088
9.500 1.4707 0.02374 0.01623 -0.1097 0.0447 0.6502
9.750 1.4863 0.02456 0.01720 -0.1088 0.0445 0.7059
10.000 1.4976 0.02502 0.01819 -0.1069 0.0444 1.0000
10.250 1.5117 0.02604 0.01924 -0.1059 0.0442 1.0000
10.500 1.5249 0.02716 0.02038 -0.1048 0.0440 1.0000
10.750 1.5374 0.02833 0.02159 -0.1037 0.0438 1.0000
11.000 1.5495 0.02957 0.02287 -0.1027 0.0436 1.0000
11.250 1.5606 0.03092 0.02425 -0.1017 0.0434 1.0000
11.500 1.5710 0.03234 0.02571 -0.1006 0.0432 1.0000
11.750 1.5808 0.03383 0.02725 -0.0996 0.0430 1.0000
12.000 1.5895 0.03546 0.02892 -0.0986 0.0428 1.0000
12.250 1.5977 0.03718 0.03068 -0.0977 0.0427 1.0000
12.500 1.6051 0.03898 0.03252 -0.0968 0.0425 1.0000
12.750 1.6120 0.04089 0.03449 -0.0959 0.0423 1.0000
13.000 1.6182 0.04294 0.03659 -0.0952 0.0422 1.0000
13.250 1.6238 0.04510 0.03880 -0.0945 0.0420 1.0000
13.500 1.6288 0.04734 0.04110 -0.0938 0.0419 1.0000
13.750 1.6335 0.04964 0.04345 -0.0932 0.0416 1.0000
14.000 1.6372 0.05210 0.04597 -0.0927 0.0414 1.0000
14.250 1.6402 0.05466 0.04858 -0.0922 0.0411 1.0000
14.500 1.6430 0.05724 0.05121 -0.0917 0.0408 1.0000
14.750 1.6434 0.06014 0.05416 -0.0913 0.0405 1.0000
15.000 1.6435 0.06310 0.05718 -0.0909 0.0402 1.0000
15.250 1.6422 0.06625 0.06039 -0.0906 0.0399 1.0000
15.500 1.6386 0.06972 0.06394 -0.0904 0.0396 1.0000
15.750 1.6416 0.07239 0.06666 -0.0901 0.0395 1.0000
16.000 1.6419 0.07545 0.06979 -0.0900 0.0394 1.0000
16.250 1.6436 0.07835 0.07275 -0.0899 0.0393 1.0000
16.500 1.6437 0.08150 0.07596 -0.0899 0.0391 1.0000
16.750 1.6440 0.08460 0.07913 -0.0899 0.0390 1.0000
17.000 1.6435 0.08784 0.08244 -0.0900 0.0388 1.0000
17.250 1.6423 0.09122 0.08589 -0.0902 0.0387 1.0000
17.500 1.6416 0.09452 0.08925 -0.0905 0.0385 1.0000
17.750 1.6394 0.09809 0.09290 -0.0908 0.0384 1.0000
18.000 1.6392 0.10134 0.09621 -0.0912 0.0382 1.0000
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