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GOE 390 AIRFOIL (goe390-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: GOE 390 AIRFOIL (goe390-il)
Reynolds number: 500,000
Max Cl/Cd: 85.22 at α=3°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe390-il-500000.txt
Download as CSV file: xf-goe390-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 390 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
  ------ -------- --------- --------- -------- -------- --------
 -13.500  -0.4920   0.04151   0.03750  -0.1437   0.8712   0.0401
 -13.250  -0.5089   0.03582   0.03147  -0.1501   0.8572   0.0402
 -13.000  -0.5126   0.03282   0.02826  -0.1526   0.8454   0.0403
 -12.750  -0.5106   0.03092   0.02617  -0.1527   0.8359   0.0405
 -12.500  -0.5067   0.02952   0.02462  -0.1517   0.8269   0.0407
 -12.250  -0.4961   0.02825   0.02316  -0.1511   0.8190   0.0410
 -12.000  -0.4826   0.02707   0.02185  -0.1505   0.8118   0.0413
 -11.750  -0.4669   0.02604   0.02067  -0.1499   0.8044   0.0417
 -11.500  -0.4499   0.02509   0.01954  -0.1493   0.7973   0.0422
 -11.250  -0.4319   0.02411   0.01843  -0.1487   0.7904   0.0426
 -11.000  -0.4128   0.02321   0.01735  -0.1480   0.7835   0.0430
 -10.750  -0.3923   0.02244   0.01638  -0.1474   0.7770   0.0433
 -10.500  -0.3724   0.02138   0.01524  -0.1468   0.7710   0.0437
 -10.250  -0.3502   0.02065   0.01448  -0.1463   0.7645   0.0442
 -10.000  -0.3267   0.02013   0.01389  -0.1458   0.7582   0.0447
  -9.750  -0.3028   0.01964   0.01335  -0.1454   0.7517   0.0452
  -9.500  -0.2788   0.01913   0.01279  -0.1449   0.7445   0.0458
  -9.250  -0.2546   0.01865   0.01218  -0.1444   0.7376   0.0465
  -9.000  -0.2302   0.01816   0.01159  -0.1440   0.7307   0.0472
  -8.750  -0.2055   0.01769   0.01101  -0.1435   0.7234   0.0478
  -8.500  -0.1814   0.01712   0.01035  -0.1430   0.7170   0.0486
  -8.250  -0.1560   0.01675   0.00997  -0.1426   0.7114   0.0494
  -8.000  -0.1300   0.01644   0.00965  -0.1423   0.7055   0.0503
  -7.750  -0.1038   0.01615   0.00929  -0.1420   0.6997   0.0514
  -7.500  -0.0773   0.01591   0.00890  -0.1417   0.6943   0.0527
  -7.250  -0.0516   0.01550   0.00851  -0.1413   0.6896   0.0540
  -7.000  -0.0249   0.01529   0.00829  -0.1411   0.6843   0.0553
  -6.750   0.0019   0.01508   0.00802  -0.1408   0.6791   0.0569
  -6.500   0.0289   0.01489   0.00769  -0.1405   0.6739   0.0586
  -6.250   0.0552   0.01459   0.00745  -0.1403   0.6693   0.0603
  -6.000   0.0825   0.01443   0.00726  -0.1401   0.6644   0.0625
  -5.750   0.1094   0.01421   0.00696  -0.1398   0.6597   0.0649
  -5.500   0.1365   0.01405   0.00677  -0.1396   0.6551   0.0671
  -5.250   0.1642   0.01395   0.00662  -0.1395   0.6508   0.0700
  -5.000   0.1904   0.01364   0.00634  -0.1392   0.6461   0.0726
  -4.750   0.2176   0.01350   0.00617  -0.1389   0.6411   0.0756
  -4.500   0.2442   0.01329   0.00589  -0.1387   0.6363   0.0785
  -4.250   0.2712   0.01311   0.00571  -0.1385   0.6319   0.0814
  -4.000   0.2984   0.01298   0.00555  -0.1383   0.6275   0.0841
  -3.750   0.3244   0.01268   0.00529  -0.1379   0.6228   0.0872
  -3.500   0.3515   0.01255   0.00513  -0.1377   0.6181   0.0903
  -3.250   0.3788   0.01245   0.00497  -0.1375   0.6132   0.0936
  -3.000   0.4052   0.01227   0.00484  -0.1372   0.6085   0.0974
  -2.750   0.4320   0.01215   0.00472  -0.1369   0.6032   0.1011
  -2.500   0.4588   0.01205   0.00463  -0.1366   0.5979   0.1063
  -2.250   0.4860   0.01202   0.00459  -0.1365   0.5928   0.1132
  -2.000   0.5128   0.01193   0.00458  -0.1362   0.5878   0.1233
  -1.750   0.5396   0.01188   0.00457  -0.1359   0.5821   0.1366
  -1.500   0.5663   0.01188   0.00455  -0.1356   0.5764   0.1511
  -1.250   0.5928   0.01185   0.00455  -0.1353   0.5706   0.1633
  -1.000   0.6191   0.01182   0.00452  -0.1349   0.5640   0.1729
  -0.750   0.6447   0.01180   0.00449  -0.1345   0.5574   0.1825
  -0.500   0.6707   0.01181   0.00449  -0.1341   0.5511   0.1903
  -0.250   0.6964   0.01178   0.00448  -0.1336   0.5438   0.1987
   0.000   0.7211   0.01183   0.00448  -0.1330   0.5365   0.2068
   0.250   0.7464   0.01180   0.00452  -0.1325   0.5289   0.2189
   0.500   0.7705   0.01182   0.00454  -0.1319   0.5206   0.2340
   0.750   0.7946   0.01184   0.00461  -0.1312   0.5130   0.2587
   1.000   0.8185   0.01181   0.00468  -0.1305   0.5049   0.3001
   1.250   0.8408   0.01181   0.00478  -0.1296   0.4972   0.3569
   1.500   0.8643   0.01166   0.00493  -0.1290   0.4897   0.4572
   1.750   0.8858   0.01163   0.00510  -0.1280   0.4823   0.5539
   2.000   0.9075   0.01160   0.00527  -0.1269   0.4759   0.6298
   2.250   0.9249   0.01133   0.00550  -0.1248   0.4698   0.7966
   2.500   0.9639   0.01139   0.00578  -0.1269   0.4628   1.0000
   2.750   0.9840   0.01159   0.00593  -0.1255   0.4575   1.0000
   3.000   1.0048   0.01179   0.00608  -0.1242   0.4522   1.0000
   3.250   1.0246   0.01205   0.00626  -0.1229   0.4470   1.0000
   3.500   1.0447   0.01236   0.00648  -0.1216   0.4418   1.0000
   3.750   1.0671   0.01256   0.00667  -0.1208   0.4375   1.0000
   4.000   1.0886   0.01281   0.00688  -0.1198   0.4328   1.0000
   4.250   1.1093   0.01312   0.00712  -0.1188   0.4284   1.0000
   4.500   1.1302   0.01349   0.00740  -0.1178   0.4237   1.0000
   4.750   1.1523   0.01372   0.00765  -0.1170   0.4204   1.0000
   5.000   1.1742   0.01399   0.00791  -0.1162   0.4166   1.0000
   5.250   1.1953   0.01431   0.00819  -0.1154   0.4128   1.0000
   5.500   1.2156   0.01469   0.00851  -0.1144   0.4089   1.0000
   5.750   1.2369   0.01508   0.00884  -0.1136   0.4049   1.0000
   6.000   1.2581   0.01538   0.00917  -0.1128   0.4019   1.0000
   6.250   1.2789   0.01572   0.00952  -0.1120   0.3986   1.0000
   6.500   1.2991   0.01610   0.00988  -0.1111   0.3951   1.0000
   6.750   1.3186   0.01653   0.01028  -0.1102   0.3915   1.0000
   7.000   1.3391   0.01701   0.01067  -0.1094   0.3872   1.0000
   7.250   1.3583   0.01741   0.01113  -0.1085   0.3846   1.0000
   7.500   1.3779   0.01783   0.01158  -0.1077   0.3815   1.0000
   7.750   1.3968   0.01829   0.01205  -0.1068   0.3781   1.0000
   8.000   1.4147   0.01882   0.01256  -0.1058   0.3745   1.0000
   8.250   1.4325   0.01940   0.01309  -0.1048   0.3706   1.0000
   8.500   1.4507   0.01994   0.01366  -0.1040   0.3674   1.0000
   8.750   1.4684   0.02050   0.01427  -0.1031   0.3643   1.0000
   9.000   1.4857   0.02111   0.01489  -0.1022   0.3608   1.0000
   9.250   1.5017   0.02179   0.01557  -0.1012   0.3572   1.0000
   9.500   1.5171   0.02252   0.01626  -0.1001   0.3533   1.0000
   9.750   1.5330   0.02325   0.01702  -0.0992   0.3498   1.0000
  10.000   1.5487   0.02400   0.01782  -0.0983   0.3462   1.0000
  10.250   1.5634   0.02482   0.01867  -0.0974   0.3424   1.0000
  10.500   1.5770   0.02571   0.01956  -0.0964   0.3386   1.0000
  10.750   1.5901   0.02664   0.02043  -0.0952   0.3345   1.0000
  11.000   1.6040   0.02759   0.02147  -0.0944   0.3311   1.0000
  11.250   1.6176   0.02857   0.02249  -0.0935   0.3270   1.0000
  11.500   1.6286   0.02972   0.02366  -0.0925   0.3227   1.0000
  11.750   1.6385   0.03094   0.02483  -0.0913   0.3182   1.0000
  12.000   1.6505   0.03212   0.02609  -0.0905   0.3144   1.0000
  12.250   1.6622   0.03332   0.02734  -0.0897   0.3101   1.0000
  12.500   1.6708   0.03475   0.02877  -0.0886   0.3057   1.0000
  12.750   1.6783   0.03624   0.03022  -0.0875   0.3012   1.0000
  13.000   1.6891   0.03762   0.03168  -0.0868   0.2973   1.0000
  13.250   1.6978   0.03914   0.03325  -0.0860   0.2927   1.0000
  13.500   1.7033   0.04092   0.03501  -0.0849   0.2882   1.0000
  13.750   1.7098   0.04263   0.03674  -0.0840   0.2838   1.0000
  14.000   1.7178   0.04430   0.03848  -0.0833   0.2795   1.0000
  14.250   1.7232   0.04620   0.04039  -0.0825   0.2750   1.0000
  14.500   1.7265   0.04823   0.04239  -0.0815   0.2706   1.0000
  14.750   1.7332   0.05005   0.04429  -0.0808   0.2670   1.0000
  15.000   1.7397   0.05191   0.04620  -0.0802   0.2631   1.0000
  15.250   1.7428   0.05408   0.04837  -0.0794   0.2592   1.0000
  15.500   1.7463   0.05612   0.05038  -0.0786   0.2552   1.0000
  15.750   1.7510   0.05822   0.05257  -0.0780   0.2520   1.0000
  16.000   1.7555   0.06036   0.05478  -0.0775   0.2484   1.0000
  16.250   1.7581   0.06263   0.05706  -0.0769   0.2448   1.0000
  16.500   1.7603   0.06489   0.05930  -0.0763   0.2412   1.0000
  16.750   1.7652   0.06691   0.06137  -0.0758   0.2381   1.0000
  17.000   1.7669   0.06943   0.06399  -0.0754   0.2351   1.0000
  17.250   1.7687   0.07190   0.06650  -0.0751   0.2317   1.0000
  17.500   1.7698   0.07439   0.06898  -0.0747   0.2283   1.0000
  17.750   1.7732   0.07651   0.07108  -0.0742   0.2246   1.0000
  18.000   1.7724   0.07940   0.07409  -0.0741   0.2218   1.0000
  18.250   1.7703   0.08242   0.07719  -0.0739   0.2185   1.0000
  18.500   1.7706   0.08509   0.07988  -0.0738   0.2152   1.0000
  18.750   1.7740   0.08727   0.08202  -0.0735   0.2117   1.0000
  19.000   1.7728   0.09020   0.08504  -0.0735   0.2091   1.0000
  19.250   1.7717   0.09314   0.08808  -0.0736   0.2065   1.0000
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