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GOE 435 AIRFOIL (goe435-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
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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