GOE 433 AIRFOIL (goe433-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 433 AIRFOIL (goe433-il) Reynolds number: 1,000,000 Max Cl/Cd: 115.92 at α=5.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe433-il-1000000.txt Download as CSV file: xf-goe433-il-1000000.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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.250 -0.9639 0.10400 0.10120 -0.0533 1.0000 0.0437
-19.000 -0.9781 0.09819 0.09532 -0.0569 1.0000 0.0443
-18.750 -0.9917 0.09254 0.08959 -0.0603 1.0000 0.0449
-18.500 -1.0064 0.08680 0.08375 -0.0639 1.0000 0.0453
-18.250 -1.0207 0.08115 0.07799 -0.0674 1.0000 0.0457
-18.000 -1.0330 0.07613 0.07295 -0.0706 1.0000 0.0465
-17.750 -1.0462 0.07093 0.06770 -0.0740 1.0000 0.0471
-17.500 -1.0600 0.06567 0.06237 -0.0774 1.0000 0.0476
-17.250 -1.0726 0.06061 0.05725 -0.0808 1.0000 0.0481
-17.000 -1.0837 0.05581 0.05237 -0.0841 1.0000 0.0486
-16.750 -1.0944 0.05120 0.04769 -0.0873 1.0000 0.0491
-16.500 -1.1025 0.04696 0.04336 -0.0903 1.0000 0.0496
-16.250 -1.1075 0.04312 0.03944 -0.0930 1.0000 0.0501
-16.000 -1.1101 0.03960 0.03583 -0.0957 1.0000 0.0505
-15.750 -1.1093 0.03651 0.03265 -0.0981 1.0000 0.0508
-15.500 -1.1174 0.03267 0.02876 -0.1009 1.0000 0.0515
-15.250 -1.1245 0.02922 0.02526 -0.1035 0.9970 0.0521
-15.000 -1.0966 0.02637 0.02236 -0.1102 0.9901 0.0531
-14.750 -1.0668 0.02423 0.02017 -0.1155 0.9816 0.0541
-14.500 -1.0376 0.02234 0.01819 -0.1203 0.9720 0.0550
-14.250 -1.0109 0.02114 0.01689 -0.1229 0.9623 0.0559
-14.000 -0.9874 0.02045 0.01609 -0.1236 0.9508 0.0565
-13.750 -0.9668 0.01918 0.01477 -0.1248 0.9380 0.0578
-13.500 -0.9430 0.01846 0.01400 -0.1253 0.9272 0.0588
-13.250 -0.9180 0.01792 0.01339 -0.1256 0.9156 0.0597
-13.000 -0.8921 0.01744 0.01285 -0.1260 0.9041 0.0607
-12.750 -0.8660 0.01702 0.01234 -0.1262 0.8929 0.0616
-12.500 -0.8390 0.01665 0.01188 -0.1264 0.8821 0.0623
-12.250 -0.8128 0.01609 0.01123 -0.1268 0.8729 0.0633
-12.000 -0.7862 0.01548 0.01058 -0.1274 0.8643 0.0646
-11.750 -0.7589 0.01511 0.01015 -0.1276 0.8564 0.0657
-11.500 -0.7307 0.01477 0.00977 -0.1280 0.8500 0.0667
-11.250 -0.7026 0.01446 0.00940 -0.1283 0.8432 0.0677
-11.000 -0.6744 0.01420 0.00905 -0.1285 0.8366 0.0687
-10.750 -0.6454 0.01397 0.00877 -0.1288 0.8312 0.0693
-10.500 -0.6178 0.01338 0.00815 -0.1293 0.8249 0.0711
-10.250 -0.5895 0.01306 0.00778 -0.1296 0.8182 0.0724
-10.000 -0.5606 0.01278 0.00748 -0.1299 0.8127 0.0735
-9.750 -0.5316 0.01252 0.00718 -0.1302 0.8065 0.0747
-9.500 -0.5026 0.01232 0.00691 -0.1303 0.8002 0.0758
-9.250 -0.4733 0.01216 0.00669 -0.1306 0.7944 0.0766
-9.000 -0.4446 0.01169 0.00621 -0.1310 0.7879 0.0787
-8.750 -0.4156 0.01142 0.00590 -0.1313 0.7804 0.0802
-8.500 -0.3863 0.01119 0.00564 -0.1315 0.7730 0.0816
-8.250 -0.3570 0.01100 0.00540 -0.1318 0.7642 0.0831
-8.000 -0.3277 0.01086 0.00519 -0.1319 0.7551 0.0843
-7.750 -0.2984 0.01057 0.00487 -0.1322 0.7429 0.0863
-7.500 -0.2693 0.01034 0.00459 -0.1324 0.7276 0.0884
-7.250 -0.2403 0.01018 0.00436 -0.1326 0.7092 0.0903
-7.000 -0.2113 0.01008 0.00416 -0.1327 0.6908 0.0922
-6.750 -0.1822 0.00998 0.00397 -0.1328 0.6760 0.0941
-6.500 -0.1530 0.00981 0.00375 -0.1330 0.6638 0.0974
-6.250 -0.1235 0.00968 0.00359 -0.1333 0.6549 0.1003
-6.000 -0.0940 0.00960 0.00346 -0.1335 0.6471 0.1029
-5.750 -0.0645 0.00945 0.00330 -0.1337 0.6400 0.1083
-5.500 -0.0346 0.00935 0.00319 -0.1340 0.6348 0.1128
-5.250 -0.0049 0.00922 0.00307 -0.1342 0.6296 0.1194
-5.000 0.0247 0.00917 0.00299 -0.1344 0.6244 0.1252
-4.750 0.0545 0.00907 0.00291 -0.1347 0.6200 0.1329
-4.500 0.0846 0.00901 0.00284 -0.1349 0.6162 0.1381
-4.250 0.1145 0.00890 0.00276 -0.1352 0.6122 0.1446
-4.000 0.1443 0.00888 0.00271 -0.1354 0.6082 0.1492
-3.750 0.1739 0.00885 0.00265 -0.1356 0.6037 0.1543
-3.500 0.2039 0.00877 0.00259 -0.1358 0.6002 0.1600
-3.250 0.2341 0.00871 0.00254 -0.1361 0.5970 0.1641
-3.000 0.2641 0.00864 0.00247 -0.1363 0.5935 0.1693
-2.750 0.2940 0.00858 0.00242 -0.1366 0.5898 0.1754
-2.500 0.3236 0.00857 0.00239 -0.1368 0.5857 0.1804
-2.250 0.3534 0.00853 0.00236 -0.1370 0.5814 0.1893
-1.750 0.4137 0.00835 0.00228 -0.1376 0.5748 0.2116
-1.500 0.4436 0.00828 0.00225 -0.1378 0.5709 0.2291
-1.250 0.4732 0.00824 0.00225 -0.1381 0.5666 0.2483
-1.000 0.5027 0.00823 0.00227 -0.1383 0.5618 0.2657
-0.750 0.5329 0.00815 0.00226 -0.1385 0.5582 0.2806
-0.500 0.5628 0.00811 0.00225 -0.1388 0.5539 0.2951
0.000 0.6217 0.00812 0.00228 -0.1391 0.5436 0.3247
0.250 0.6517 0.00806 0.00229 -0.1394 0.5392 0.3409
0.500 0.6814 0.00803 0.00231 -0.1396 0.5325 0.3586
0.750 0.7104 0.00805 0.00234 -0.1397 0.5249 0.3799
1.000 0.7401 0.00802 0.00239 -0.1399 0.5182 0.4035
1.250 0.7692 0.00806 0.00244 -0.1400 0.5095 0.4238
1.500 0.7982 0.00812 0.00250 -0.1401 0.4997 0.4402
1.750 0.8265 0.00824 0.00257 -0.1400 0.4866 0.4527
2.000 0.8551 0.00835 0.00265 -0.1400 0.4738 0.4639
2.250 0.8834 0.00847 0.00275 -0.1400 0.4629 0.4733
2.500 0.9111 0.00865 0.00287 -0.1398 0.4506 0.4826
2.750 0.9394 0.00877 0.00297 -0.1398 0.4401 0.4903
3.000 0.9671 0.00893 0.00310 -0.1397 0.4305 0.4981
3.250 0.9951 0.00909 0.00323 -0.1396 0.4208 0.5053
3.500 1.0227 0.00925 0.00336 -0.1395 0.4122 0.5120
3.750 1.0506 0.00939 0.00350 -0.1394 0.4037 0.5189
4.000 1.0777 0.00959 0.00365 -0.1392 0.3942 0.5254
4.250 1.1053 0.00974 0.00379 -0.1391 0.3849 0.5316
4.500 1.1322 0.00993 0.00396 -0.1389 0.3757 0.5384
4.750 1.1595 0.01010 0.00411 -0.1387 0.3667 0.5446
5.000 1.1861 0.01031 0.00428 -0.1384 0.3573 0.5496
5.250 1.2129 0.01049 0.00445 -0.1382 0.3477 0.5551
5.500 1.2392 0.01069 0.00463 -0.1379 0.3383 0.5606
5.750 1.2648 0.01096 0.00484 -0.1375 0.3266 0.5657
6.000 1.2906 0.01118 0.00505 -0.1372 0.3146 0.5723
6.250 1.3150 0.01149 0.00531 -0.1366 0.2995 0.5793
6.500 1.3375 0.01194 0.00564 -0.1358 0.2781 0.5859
6.750 1.3580 0.01247 0.00605 -0.1347 0.2529 0.5947
7.000 1.3742 0.01326 0.00664 -0.1329 0.2164 0.6046
7.250 1.3864 0.01424 0.00740 -0.1306 0.1784 0.6166
7.500 1.4018 0.01495 0.00802 -0.1288 0.1570 0.6323
7.750 1.4161 0.01549 0.00857 -0.1266 0.1435 0.6580
8.000 1.4319 0.01599 0.00917 -0.1248 0.1318 0.7215
8.250 1.4427 0.01619 0.00978 -0.1220 0.1208 1.0000
8.500 1.4550 0.01701 0.01049 -0.1199 0.1068 1.0000
8.750 1.4537 0.01863 0.01187 -0.1162 0.0700 1.0000
9.000 1.4610 0.01984 0.01302 -0.1138 0.0597 1.0000
9.250 1.4738 0.02078 0.01395 -0.1122 0.0572 1.0000
9.500 1.4875 0.02169 0.01487 -0.1108 0.0555 1.0000
9.750 1.5023 0.02257 0.01577 -0.1095 0.0548 1.0000
10.000 1.5164 0.02351 0.01674 -0.1083 0.0542 1.0000
10.250 1.5298 0.02454 0.01780 -0.1071 0.0537 1.0000
10.500 1.5423 0.02567 0.01896 -0.1058 0.0531 1.0000
10.750 1.5539 0.02689 0.02022 -0.1046 0.0527 1.0000
11.000 1.5645 0.02821 0.02157 -0.1034 0.0522 1.0000
11.250 1.5743 0.02964 0.02304 -0.1022 0.0518 1.0000
11.500 1.5830 0.03119 0.02463 -0.1010 0.0514 1.0000
11.750 1.5908 0.03284 0.02632 -0.0998 0.0510 1.0000
12.000 1.5977 0.03460 0.02813 -0.0986 0.0506 1.0000
12.250 1.6031 0.03655 0.03014 -0.0975 0.0502 1.0000
12.500 1.6073 0.03865 0.03230 -0.0964 0.0499 1.0000
12.750 1.6104 0.04094 0.03465 -0.0955 0.0496 1.0000
13.000 1.6132 0.04335 0.03713 -0.0946 0.0493 1.0000
13.250 1.6183 0.04557 0.03941 -0.0939 0.0493 1.0000
13.500 1.6226 0.04789 0.04179 -0.0932 0.0491 1.0000
13.750 1.6264 0.05031 0.04428 -0.0926 0.0490 1.0000
14.000 1.6296 0.05285 0.04688 -0.0921 0.0489 1.0000
14.250 1.6325 0.05545 0.04955 -0.0916 0.0487 1.0000
14.500 1.6354 0.05803 0.05218 -0.0912 0.0484 1.0000
14.750 1.6362 0.06090 0.05512 -0.0908 0.0482 1.0000
15.000 1.6372 0.06375 0.05804 -0.0904 0.0479 1.0000
15.250 1.6373 0.06676 0.06111 -0.0901 0.0477 1.0000
15.500 1.6363 0.06993 0.06434 -0.0899 0.0474 1.0000
15.750 1.6358 0.07302 0.06750 -0.0896 0.0472 1.0000
16.000 1.6333 0.07645 0.07100 -0.0896 0.0470 1.0000
16.250 1.6316 0.07980 0.07442 -0.0895 0.0467 1.0000
16.500 1.6294 0.08325 0.07793 -0.0895 0.0465 1.0000
16.750 1.6260 0.08687 0.08162 -0.0897 0.0464 1.0000
17.000 1.6239 0.09033 0.08515 -0.0898 0.0462 1.0000
17.250 1.6202 0.09408 0.08897 -0.0901 0.0460 1.0000
17.500 1.6174 0.09772 0.09267 -0.0904 0.0458 1.0000
17.750 1.6143 0.10139 0.09640 -0.0908 0.0456 1.0000
18.000 1.6103 0.10519 0.10026 -0.0913 0.0454 1.0000
18.250 1.6075 0.10884 0.10397 -0.0919 0.0451 1.0000
18.500 1.6026 0.11280 0.10799 -0.0926 0.0448 1.0000
18.750 1.5998 0.11645 0.11169 -0.0932 0.0445 1.0000
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