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GOE 241 (MVA PR.1) AIRFOIL (goe241-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: GOE 241 (MVA PR.1) AIRFOIL (goe241-il)
Reynolds number: 200,000
Max Cl/Cd: 68.14 at α=6.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe241-il-200000.txt
Download as CSV file: xf-goe241-il-200000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 241 (MVA PR.1) AIRFOIL                      
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.750   0.1380   0.10540   0.10158  -0.1159   0.9069   0.0635
 -10.500   0.1441   0.10272   0.09886  -0.1171   0.9009   0.0658
 -10.250   0.1249   0.09865   0.09481  -0.1229   0.8908   0.0682
 -10.000   0.1442   0.09632   0.09246  -0.1210   0.8853   0.0688
  -9.750   0.1589   0.09430   0.09041  -0.1202   0.8783   0.0698
  -9.500   0.1699   0.09215   0.08824  -0.1202   0.8707   0.0712
  -9.250   0.1778   0.08965   0.08569  -0.1209   0.8648   0.0733
  -9.000   0.1548   0.08441   0.08049  -0.1289   0.8545   0.0772
  -8.750   0.1758   0.08262   0.07865  -0.1264   0.8487   0.0779
  -8.500   0.1919   0.08102   0.07703  -0.1253   0.8413   0.0791
  -8.250   0.2045   0.07917   0.07515  -0.1252   0.8336   0.0813
  -8.000   0.1790   0.07286   0.06885  -0.1350   0.8251   0.0875
  -7.750   0.2028   0.07201   0.06799  -0.1315   0.8178   0.0885
  -7.500   0.2213   0.07069   0.06661  -0.1302   0.8114   0.0901
  -7.250   0.1951   0.06262   0.05859  -0.1453   0.8014   0.0991
  -7.000   0.2160   0.06268   0.05861  -0.1398   0.7946   0.0999
  -6.750   0.2359   0.06204   0.05792  -0.1370   0.7880   0.1013
  -6.500   0.2512   0.06080   0.05668  -0.1363   0.7790   0.1039
  -6.250   0.2667   0.04545   0.04106  -0.1738   0.7715   0.1270
  -6.000   0.2776   0.04667   0.04244  -0.1644   0.7625   0.1279
  -5.750   0.2956   0.04813   0.04390  -0.1570   0.7550   0.1292
  -5.500   0.4009   0.02702   0.02014  -0.2062   0.7480   0.0770
  -5.250   0.4291   0.02486   0.01796  -0.2068   0.7392   0.0750
  -5.000   0.4627   0.02334   0.01618  -0.2082   0.7324   0.0737
  -4.750   0.4921   0.02226   0.01496  -0.2087   0.7221   0.0732
  -4.500   0.5250   0.02139   0.01383  -0.2096   0.7147   0.0741
  -4.250   0.5536   0.02068   0.01302  -0.2098   0.7037   0.0748
  -4.000   0.5854   0.01994   0.01207  -0.2103   0.6957   0.0751
  -3.750   0.6132   0.01939   0.01147  -0.2102   0.6842   0.0757
  -3.500   0.6437   0.01893   0.01084  -0.2105   0.6753   0.0765
  -3.250   0.6715   0.01829   0.01024  -0.2105   0.6646   0.0779
  -3.000   0.7012   0.01784   0.00979  -0.2109   0.6555   0.0808
  -2.750   0.7303   0.01756   0.00949  -0.2111   0.6453   0.0837
  -2.500   0.7605   0.01736   0.00921  -0.2115   0.6364   0.0862
  -2.250   0.7914   0.01703   0.00889  -0.2123   0.6268   0.0897
  -2.000   0.8229   0.01687   0.00864  -0.2132   0.6181   0.0953
  -1.750   0.8541   0.01667   0.00836  -0.2141   0.6087   0.1042
  -1.500   0.8866   0.01646   0.00807  -0.2152   0.6005   0.1244
  -1.250   0.9195   0.01602   0.00837  -0.2169   0.5914   0.3819
  -1.000   0.9469   0.01651   0.00873  -0.2164   0.5842   0.4167
  -0.750   0.9718   0.01694   0.00917  -0.2156   0.5762   0.4356
  -0.500   0.9988   0.01736   0.00946  -0.2151   0.5696   0.4508
  -0.250   1.0239   0.01779   0.00993  -0.2143   0.5634   0.4600
   0.000   1.0507   0.01811   0.01016  -0.2140   0.5569   0.4720
   0.250   1.0761   0.01848   0.01053  -0.2132   0.5514   0.4789
   0.500   1.1035   0.01886   0.01081  -0.2131   0.5460   0.4897
   0.750   1.1273   0.01917   0.01118  -0.2121   0.5399   0.4969
   1.000   1.1533   0.01946   0.01143  -0.2117   0.5346   0.5046
   1.250   1.1845   0.01969   0.01145  -0.2125   0.5302   0.5125
   1.500   1.2089   0.01990   0.01175  -0.2119   0.5255   0.5167
   1.750   1.2346   0.02011   0.01196  -0.2116   0.5206   0.5221
   2.000   1.2630   0.02029   0.01203  -0.2119   0.5158   0.5294
   2.250   1.2926   0.02054   0.01215  -0.2124   0.5115   0.5343
   2.500   1.3155   0.02075   0.01245  -0.2116   0.5067   0.5394
   2.750   1.3407   0.02096   0.01264  -0.2113   0.5015   0.5467
   3.000   1.3672   0.02114   0.01277  -0.2112   0.4969   0.5526
   3.250   1.3967   0.02144   0.01296  -0.2116   0.4927   0.5583
   3.500   1.4189   0.02168   0.01327  -0.2109   0.4884   0.5650
   3.750   1.4428   0.02189   0.01351  -0.2104   0.4838   0.5707
   4.000   1.4676   0.02210   0.01372  -0.2100   0.4795   0.5766
   4.250   1.4962   0.02239   0.01389  -0.2104   0.4756   0.5845
   4.500   1.5194   0.02267   0.01423  -0.2098   0.4716   0.5898
   4.750   1.5402   0.02293   0.01458  -0.2088   0.4671   0.5957
   5.000   1.5638   0.02320   0.01482  -0.2083   0.4627   0.6029
   5.250   1.5887   0.02340   0.01501  -0.2079   0.4586   0.6086
   5.500   1.6140   0.02373   0.01532  -0.2078   0.4544   0.6156
   5.750   1.6310   0.02406   0.01574  -0.2062   0.4497   0.6218
   6.000   1.6503   0.02431   0.01606  -0.2050   0.4449   0.6274
   6.250   1.6734   0.02456   0.01627  -0.2044   0.4403   0.6346
   6.500   1.6953   0.02491   0.01662  -0.2037   0.4357   0.6410
   6.750   1.7066   0.02528   0.01713  -0.2011   0.4304   0.6468
   7.000   1.7201   0.02560   0.01748  -0.1989   0.4252   0.6533
   7.250   1.7436   0.02586   0.01766  -0.1984   0.4202   0.6600
   7.500   1.7483   0.02643   0.01839  -0.1949   0.4146   0.6661
   7.750   1.7578   0.02699   0.01900  -0.1923   0.4084   0.6727
   8.000   1.7765   0.02735   0.01931  -0.1912   0.4027   0.6792
   8.250   1.7797   0.02818   0.02030  -0.1879   0.3959   0.6858
   8.500   1.7868   0.02893   0.02109  -0.1853   0.3887   0.6928
   8.750   1.7970   0.02967   0.02183  -0.1831   0.3815   0.7002
   9.000   1.7980   0.03082   0.02310  -0.1800   0.3730   0.7073
   9.250   1.8068   0.03172   0.02396  -0.1779   0.3653   0.7151
   9.500   1.8070   0.03315   0.02551  -0.1750   0.3560   0.7238
   9.750   1.8147   0.03425   0.02658  -0.1730   0.3486   0.7341
  10.000   1.8166   0.03583   0.02828  -0.1706   0.3399   0.7458
  10.250   1.8258   0.03695   0.02935  -0.1690   0.3335   0.7625
  10.500   1.8284   0.03858   0.03119  -0.1669   0.3262   0.7933
  10.750   1.8315   0.03979   0.03248  -0.1645   0.3206   1.0000
  11.000   1.8425   0.04107   0.03368  -0.1633   0.3158   1.0000
  11.250   1.8481   0.04281   0.03550  -0.1618   0.3108   1.0000
  11.500   1.8568   0.04430   0.03701  -0.1606   0.3066   1.0000
  11.750   1.8697   0.04545   0.03809  -0.1595   0.3031   1.0000
  12.000   1.8826   0.04665   0.03926  -0.1585   0.2997   1.0000
  12.250   1.8881   0.04849   0.04121  -0.1572   0.2964   1.0000
  12.500   1.8957   0.05015   0.04294  -0.1560   0.2932   1.0000
  12.750   1.9053   0.05162   0.04443  -0.1550   0.2904   1.0000
  13.000   1.9202   0.05262   0.04539  -0.1542   0.2877   1.0000
  13.250   1.9376   0.05341   0.04611  -0.1535   0.2846   1.0000
  13.500   1.9356   0.05598   0.04886  -0.1520   0.2817   1.0000
  13.750   1.9369   0.05828   0.05127  -0.1508   0.2785   1.0000
  14.000   1.9416   0.06024   0.05327  -0.1498   0.2753   1.0000
  14.250   1.9536   0.06145   0.05445  -0.1490   0.2721   1.0000
  14.500   1.9713   0.06213   0.05507  -0.1483   0.2689   1.0000
  14.750   1.9652   0.06529   0.05842  -0.1471   0.2666   1.0000
  15.000   1.9631   0.06810   0.06137  -0.1461   0.2641   1.0000
  15.250   1.9644   0.07057   0.06394  -0.1452   0.2615   1.0000
  15.500   1.9702   0.07251   0.06594  -0.1445   0.2590   1.0000
  15.750   1.9834   0.07357   0.06698  -0.1439   0.2563   1.0000
  16.000   2.0036   0.07387   0.06723  -0.1433   0.2533   1.0000
  16.250   1.9881   0.07829   0.07189  -0.1424   0.2513   1.0000
  16.500   1.9758   0.08250   0.07629  -0.1418   0.2488   1.0000
  16.750   1.9691   0.08606   0.07998  -0.1414   0.2461   1.0000
  17.000   1.9718   0.08843   0.08243  -0.1410   0.2435   1.0000
  17.250   1.9852   0.08940   0.08338  -0.1406   0.2408   1.0000
  17.500   2.0070   0.08926   0.08318  -0.1400   0.2376   1.0000
  17.750   1.9801   0.09553   0.08973  -0.1401   0.2356   1.0000
  18.000   1.9543   0.10188   0.09632  -0.1405   0.2331   1.0000
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