GOE 435 AIRFOIL (goe435-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 435 AIRFOIL (goe435-il) Reynolds number: 1,000,000 Max Cl/Cd: 79.58 at α=4.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe435-il-1000000-n5.txt Download as CSV file: xf-goe435-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 435 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
------ -------- --------- --------- -------- -------- --------
-16.750 -0.6862 0.08968 0.08485 -0.0687 0.7350 0.0554
-16.500 -0.6958 0.08499 0.08009 -0.0710 0.7316 0.0556
-16.250 -0.7059 0.08033 0.07533 -0.0733 0.7281 0.0557
-16.000 -0.7154 0.07582 0.07072 -0.0754 0.7244 0.0558
-15.750 -0.7226 0.07165 0.06646 -0.0775 0.7200 0.0559
-15.500 -0.7269 0.06794 0.06267 -0.0793 0.7161 0.0561
-15.250 -0.7309 0.06425 0.05892 -0.0811 0.7132 0.0562
-15.000 -0.7337 0.06079 0.05538 -0.0828 0.7101 0.0563
-14.750 -0.7327 0.05781 0.05235 -0.0842 0.7072 0.0564
-14.500 -0.7335 0.05465 0.04911 -0.0858 0.7042 0.0565
-14.250 -0.7302 0.05204 0.04644 -0.0871 0.7006 0.0566
-14.000 -0.7288 0.04920 0.04352 -0.0886 0.6962 0.0567
-13.750 -0.7244 0.04678 0.04103 -0.0898 0.6912 0.0568
-13.500 -0.7212 0.04422 0.03842 -0.0911 0.6890 0.0569
-13.250 -0.7181 0.04175 0.03590 -0.0924 0.6867 0.0570
-13.000 -0.7183 0.03896 0.03306 -0.0938 0.6842 0.0573
-12.750 -0.7151 0.03653 0.03058 -0.0951 0.6814 0.0575
-12.500 -0.7111 0.03410 0.02809 -0.0965 0.6784 0.0578
-12.250 -0.7055 0.03179 0.02573 -0.0978 0.6752 0.0580
-12.000 -0.6975 0.02969 0.02358 -0.0992 0.6717 0.0583
-11.750 -0.6876 0.02772 0.02155 -0.1005 0.6680 0.0586
-11.500 -0.6760 0.02586 0.01965 -0.1019 0.6652 0.0589
-11.250 -0.6625 0.02413 0.01788 -0.1033 0.6628 0.0592
-11.000 -0.6494 0.02252 0.01624 -0.1046 0.6598 0.0595
-10.750 -0.6334 0.02108 0.01476 -0.1061 0.6561 0.0599
-10.500 -0.6115 0.01983 0.01345 -0.1082 0.6519 0.0603
-10.250 -0.5869 0.01875 0.01232 -0.1104 0.6473 0.0608
-10.000 -0.5603 0.01785 0.01136 -0.1124 0.6426 0.0612
-9.750 -0.5323 0.01711 0.01059 -0.1142 0.6387 0.0617
-9.500 -0.5045 0.01657 0.01002 -0.1153 0.6329 0.0621
-9.250 -0.4768 0.01614 0.00953 -0.1162 0.6257 0.0625
-9.000 -0.4487 0.01576 0.00910 -0.1169 0.6192 0.0628
-8.750 -0.4205 0.01534 0.00865 -0.1177 0.6119 0.0636
-8.500 -0.3925 0.01497 0.00823 -0.1183 0.6020 0.0645
-8.250 -0.3640 0.01463 0.00786 -0.1190 0.5920 0.0654
-8.000 -0.3357 0.01436 0.00752 -0.1195 0.5789 0.0664
-7.750 -0.3071 0.01411 0.00722 -0.1200 0.5657 0.0675
-7.500 -0.2784 0.01390 0.00694 -0.1204 0.5542 0.0686
-7.250 -0.2497 0.01368 0.00667 -0.1209 0.5436 0.0703
-7.000 -0.2209 0.01341 0.00637 -0.1214 0.5355 0.0732
-6.750 -0.1918 0.01309 0.00604 -0.1220 0.5288 0.0783
-6.500 -0.1650 0.01217 0.00534 -0.1231 0.5225 0.1310
-6.250 -0.1350 0.01211 0.00526 -0.1235 0.5166 0.1356
-6.000 -0.1047 0.01201 0.00517 -0.1240 0.5127 0.1389
-5.750 -0.0744 0.01194 0.00510 -0.1244 0.5084 0.1415
-5.500 -0.0441 0.01190 0.00504 -0.1248 0.5043 0.1435
-5.250 -0.0140 0.01187 0.00499 -0.1251 0.5002 0.1448
-4.750 0.0466 0.01176 0.00484 -0.1259 0.4927 0.1472
-4.500 0.0771 0.01168 0.00477 -0.1263 0.4895 0.1485
-4.250 0.1075 0.01162 0.00471 -0.1268 0.4862 0.1496
-4.000 0.1377 0.01158 0.00466 -0.1271 0.4823 0.1506
-3.750 0.1676 0.01156 0.00461 -0.1275 0.4782 0.1515
-3.500 0.1975 0.01155 0.00458 -0.1278 0.4740 0.1523
-3.250 0.2280 0.01151 0.00454 -0.1282 0.4718 0.1532
-3.000 0.2587 0.01147 0.00449 -0.1286 0.4695 0.1541
-2.750 0.2892 0.01143 0.00445 -0.1290 0.4664 0.1547
-2.500 0.3194 0.01141 0.00442 -0.1294 0.4630 0.1554
-2.250 0.3496 0.01141 0.00440 -0.1297 0.4601 0.1559
-2.000 0.3796 0.01141 0.00439 -0.1300 0.4574 0.1563
-1.750 0.4093 0.01142 0.00438 -0.1303 0.4541 0.1566
-1.500 0.4391 0.01140 0.00434 -0.1306 0.4510 0.1574
-1.250 0.4697 0.01134 0.00429 -0.1311 0.4491 0.1584
-1.000 0.5001 0.01129 0.00426 -0.1315 0.4471 0.1598
-0.750 0.5302 0.01126 0.00425 -0.1318 0.4444 0.1612
-0.500 0.5602 0.01125 0.00424 -0.1322 0.4411 0.1621
-0.250 0.5897 0.01127 0.00424 -0.1324 0.4373 0.1631
0.000 0.6188 0.01130 0.00426 -0.1326 0.4334 0.1642
0.250 0.6482 0.01133 0.00428 -0.1328 0.4303 0.1652
0.500 0.6781 0.01132 0.00429 -0.1332 0.4275 0.1659
0.750 0.7076 0.01134 0.00431 -0.1334 0.4233 0.1666
1.000 0.7365 0.01139 0.00434 -0.1335 0.4181 0.1672
1.250 0.7645 0.01148 0.00439 -0.1336 0.4127 0.1679
1.500 0.7936 0.01152 0.00443 -0.1337 0.4086 0.1685
1.750 0.8220 0.01158 0.00449 -0.1338 0.4019 0.1691
2.000 0.8487 0.01171 0.00457 -0.1336 0.3935 0.1704
2.250 0.8762 0.01180 0.00464 -0.1336 0.3841 0.1724
2.500 0.9017 0.01196 0.00475 -0.1332 0.3731 0.1744
2.750 0.9262 0.01216 0.00490 -0.1327 0.3604 0.1763
3.000 0.9499 0.01239 0.00508 -0.1321 0.3473 0.1783
3.250 0.9724 0.01265 0.00528 -0.1312 0.3349 0.1804
3.500 0.9930 0.01294 0.00552 -0.1301 0.3237 0.1826
4.000 1.0317 0.01341 0.00595 -0.1273 0.3078 0.1941
4.250 1.0543 0.01357 0.00616 -0.1266 0.3019 0.2141
4.500 1.0799 0.01357 0.00647 -0.1270 0.2942 0.3324
4.750 1.1014 0.01392 0.00683 -0.1262 0.2878 0.3465
5.000 1.1237 0.01425 0.00717 -0.1255 0.2821 0.3552
5.250 1.1443 0.01467 0.00757 -0.1246 0.2767 0.3606
5.500 1.1648 0.01509 0.00798 -0.1237 0.2720 0.3638
5.750 1.1875 0.01542 0.00833 -0.1231 0.2689 0.3686
6.000 1.2088 0.01582 0.00874 -0.1225 0.2652 0.3728
6.250 1.2291 0.01628 0.00920 -0.1217 0.2614 0.3765
6.500 1.2479 0.01683 0.00975 -0.1207 0.2576 0.3797
6.750 1.2683 0.01731 0.01024 -0.1200 0.2546 0.3824
7.000 1.2889 0.01780 0.01074 -0.1194 0.2517 0.3849
7.250 1.3082 0.01836 0.01132 -0.1186 0.2481 0.3895
7.500 1.3262 0.01902 0.01199 -0.1178 0.2442 0.3936
7.750 1.3425 0.01981 0.01277 -0.1169 0.2403 0.3963
8.000 1.3620 0.02042 0.01341 -0.1163 0.2381 0.3988
8.250 1.3804 0.02111 0.01412 -0.1156 0.2358 0.4010
8.500 1.3984 0.02184 0.01487 -0.1149 0.2332 0.4029
8.750 1.4146 0.02271 0.01575 -0.1142 0.2303 0.4044
9.000 1.4298 0.02367 0.01670 -0.1133 0.2274 0.4057
9.250 1.4439 0.02471 0.01776 -0.1125 0.2245 0.4077
9.500 1.4610 0.02556 0.01865 -0.1119 0.2227 0.4110
9.750 1.4774 0.02647 0.01959 -0.1113 0.2205 0.4146
10.000 1.4915 0.02757 0.02072 -0.1106 0.2179 0.4180
10.250 1.5048 0.02872 0.02189 -0.1098 0.2149 0.4213
10.500 1.5144 0.03017 0.02335 -0.1089 0.2116 0.4242
10.750 1.5273 0.03138 0.02458 -0.1081 0.2089 0.4272
11.000 1.5407 0.03257 0.02580 -0.1074 0.2066 0.4298
11.250 1.5523 0.03394 0.02721 -0.1067 0.2043 0.4341
11.500 1.5639 0.03529 0.02860 -0.1060 0.2017 0.4388
11.750 1.5723 0.03694 0.03028 -0.1052 0.1992 0.4441
12.000 1.5808 0.03860 0.03198 -0.1044 0.1967 0.4500
12.500 1.6031 0.04156 0.03506 -0.1033 0.1933 0.4677
12.750 1.6133 0.04314 0.03668 -0.1027 0.1911 0.4769
13.000 1.6217 0.04487 0.03847 -0.1021 0.1888 0.4880
13.250 1.6275 0.04691 0.04057 -0.1014 0.1865 0.5036
13.500 1.6342 0.04886 0.04259 -0.1009 0.1841 0.5244
13.750 1.6417 0.05082 0.04465 -0.1004 0.1825 0.5492
14.000 1.6510 0.05258 0.04650 -0.1000 0.1806 0.5752
14.250 1.6575 0.05462 0.04864 -0.0996 0.1785 0.5989
14.500 1.6626 0.05683 0.05093 -0.0991 0.1762 0.6213
14.750 1.6657 0.05925 0.05342 -0.0987 0.1738 0.6434
15.000 1.6675 0.06184 0.05609 -0.0982 0.1715 0.6656
15.250 1.6747 0.06387 0.05822 -0.0979 0.1699 0.6890
15.500 1.6785 0.06626 0.06070 -0.0975 0.1680 0.7086
15.750 1.6834 0.06853 0.06303 -0.0972 0.1657 0.7245
16.000 1.6833 0.07138 0.06594 -0.0969 0.1635 0.7379
16.250 1.6847 0.07406 0.06867 -0.0966 0.1612 0.7488
16.500 1.6850 0.07688 0.07154 -0.0963 0.1594 0.7594
16.750 1.6897 0.07919 0.07393 -0.0961 0.1579 0.7694
17.000 1.6944 0.08151 0.07630 -0.0960 0.1559 0.7809
17.250 1.6931 0.08454 0.07940 -0.0959 0.1533 0.7921
17.500 1.6927 0.08746 0.08237 -0.0958 0.1507 0.8055
18.000 1.6931 0.09277 0.08803 -0.0953 0.1467 0.9119
18.250 1.6943 0.09532 0.09063 -0.0952 0.1441 1.0000
18.500 1.6940 0.09825 0.09358 -0.0953 0.1410 1.0000
18.750 1.6875 0.10200 0.09736 -0.0955 0.1382 1.0000
19.000 1.6902 0.10462 0.10000 -0.0957 0.1353 1.0000
19.250 1.6880 0.10781 0.10321 -0.0960 0.1316 1.0000
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