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GOE 241 (MVA PR.1) AIRFOIL (goe241-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: GOE 241 (MVA PR.1) AIRFOIL (goe241-il)
Reynolds number: 500,000
Max Cl/Cd: 94.51 at α=3.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe241-il-500000.txt
Download as CSV file: xf-goe241-il-500000.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 =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.750   0.0981   0.10017   0.09706  -0.1048   0.8256   0.0380
 -10.500   0.1074   0.09759   0.09448  -0.1061   0.8193   0.0387
 -10.250   0.0837   0.08843   0.08528  -0.1156   0.8136   0.0414
 -10.000   0.0975   0.08652   0.08333  -0.1148   0.8080   0.0417
  -9.750   0.1118   0.08487   0.08169  -0.1148   0.8020   0.0419
  -9.500   0.1252   0.08319   0.07997  -0.1150   0.7957   0.0422
  -9.250   0.1378   0.08140   0.07813  -0.1155   0.7897   0.0427
  -9.000   0.1490   0.07919   0.07594  -0.1167   0.7835   0.0433
  -8.750   0.1116   0.06476   0.06151  -0.1309   0.7782   0.0472
  -8.500   0.1282   0.06424   0.06093  -0.1299   0.7720   0.0474
  -8.250   0.1433   0.06309   0.05980  -0.1299   0.7656   0.0476
  -8.000   0.1562   0.06140   0.05810  -0.1306   0.7589   0.0480
  -7.750   0.1671   0.05927   0.05592  -0.1318   0.7527   0.0485
  -7.500   0.1702   0.03333   0.02898  -0.1897   0.7455   0.0536
  -7.250   0.1938   0.03153   0.02723  -0.1901   0.7390   0.0542
  -7.000   0.2203   0.03013   0.02577  -0.1914   0.7327   0.0550
  -6.750   0.2648   0.02333   0.01808  -0.2013   0.7261   0.0458
  -6.500   0.2969   0.02120   0.01572  -0.2036   0.7188   0.0446
  -6.250   0.3294   0.01950   0.01376  -0.2055   0.7118   0.0441
  -6.000   0.3609   0.01841   0.01250  -0.2068   0.7033   0.0444
  -5.750   0.3919   0.01761   0.01151  -0.2077   0.6951   0.0450
  -5.500   0.4227   0.01678   0.01055  -0.2086   0.6856   0.0453
  -5.250   0.4529   0.01612   0.00974  -0.2091   0.6764   0.0456
  -5.000   0.4831   0.01556   0.00908  -0.2097   0.6662   0.0461
  -4.750   0.5129   0.01517   0.00855  -0.2101   0.6563   0.0465
  -4.500   0.5427   0.01474   0.00802  -0.2105   0.6452   0.0470
  -4.250   0.5717   0.01412   0.00739  -0.2109   0.6342   0.0479
  -3.750   0.6299   0.01368   0.00685  -0.2115   0.6093   0.0501
  -3.500   0.6591   0.01351   0.00660  -0.2118   0.5971   0.0513
  -3.250   0.6878   0.01340   0.00638  -0.2120   0.5851   0.0523
  -3.000   0.7173   0.01326   0.00617  -0.2124   0.5736   0.0532
  -2.750   0.7476   0.01298   0.00585  -0.2132   0.5628   0.0549
  -2.500   0.7768   0.01291   0.00570  -0.2136   0.5517   0.0566
  -2.250   0.8061   0.01286   0.00559  -0.2140   0.5421   0.0588
  -2.000   0.8357   0.01277   0.00542  -0.2145   0.5334   0.0613
  -1.750   0.8654   0.01270   0.00530  -0.2150   0.5262   0.0645
  -1.500   0.8946   0.01269   0.00523  -0.2153   0.5192   0.0677
  -1.250   0.9237   0.01266   0.00511  -0.2157   0.5126   0.0734
  -1.000   0.9534   0.01260   0.00505  -0.2162   0.5070   0.0836
  -0.750   0.9880   0.01192   0.00497  -0.2185   0.5011   0.3324
  -0.500   1.0152   0.01208   0.00513  -0.2183   0.4955   0.3721
  -0.250   1.0424   0.01225   0.00529  -0.2182   0.4904   0.3929
   0.000   1.0699   0.01239   0.00545  -0.2181   0.4854   0.4073
   0.250   1.0967   0.01257   0.00560  -0.2179   0.4805   0.4186
   0.500   1.1226   0.01282   0.00577  -0.2175   0.4755   0.4285
   0.750   1.1496   0.01297   0.00594  -0.2173   0.4715   0.4376
   1.000   1.1765   0.01313   0.00610  -0.2171   0.4673   0.4460
   1.250   1.2027   0.01331   0.00624  -0.2168   0.4629   0.4535
   1.500   1.2278   0.01355   0.00646  -0.2163   0.4586   0.4612
   1.750   1.2534   0.01381   0.00667  -0.2159   0.4550   0.4694
   2.000   1.2798   0.01393   0.00684  -0.2157   0.4517   0.4761
   2.250   1.3054   0.01409   0.00701  -0.2153   0.4476   0.4812
   2.500   1.3301   0.01430   0.00719  -0.2148   0.4435   0.4867
   2.750   1.3542   0.01457   0.00738  -0.2142   0.4396   0.4917
   3.000   1.3788   0.01476   0.00760  -0.2137   0.4362   0.4965
   3.250   1.4036   0.01492   0.00781  -0.2132   0.4331   0.5014
   3.500   1.4277   0.01512   0.00801  -0.2126   0.4298   0.5070
   3.750   1.4508   0.01535   0.00821  -0.2118   0.4263   0.5121
   4.000   1.4713   0.01559   0.00846  -0.2106   0.4228   0.5163
   4.250   1.4910   0.01590   0.00875  -0.2092   0.4192   0.5206
   4.500   1.5125   0.01609   0.00899  -0.2081   0.4164   0.5255
   4.750   1.5346   0.01632   0.00924  -0.2073   0.4129   0.5304
   5.000   1.5561   0.01658   0.00953  -0.2063   0.4092   0.5347
   5.250   1.5762   0.01692   0.00987  -0.2052   0.4054   0.5390
   5.500   1.5959   0.01733   0.01026  -0.2040   0.4014   0.5436
   5.750   1.6177   0.01759   0.01056  -0.2032   0.3979   0.5483
   6.000   1.6385   0.01788   0.01091  -0.2023   0.3937   0.5524
   6.250   1.6574   0.01828   0.01132  -0.2010   0.3892   0.5566
   6.500   1.6740   0.01880   0.01182  -0.1995   0.3844   0.5610
   6.750   1.6946   0.01914   0.01221  -0.1986   0.3797   0.5656
   7.000   1.7131   0.01957   0.01268  -0.1974   0.3738   0.5697
   7.250   1.7273   0.02022   0.01331  -0.1957   0.3675   0.5736
   7.500   1.7461   0.02067   0.01382  -0.1947   0.3608   0.5781
   7.750   1.7602   0.02139   0.01452  -0.1930   0.3526   0.5825
   8.000   1.7754   0.02208   0.01523  -0.1916   0.3436   0.5864
   8.250   1.7855   0.02307   0.01620  -0.1896   0.3324   0.5903
   8.500   1.7953   0.02416   0.01726  -0.1876   0.3184   0.5943
   8.750   1.8020   0.02549   0.01855  -0.1854   0.3033   0.5984
   9.000   1.8067   0.02702   0.02002  -0.1831   0.2895   0.6020
   9.250   1.8113   0.02863   0.02158  -0.1809   0.2790   0.6056
   9.500   1.8138   0.03043   0.02336  -0.1786   0.2704   0.6093
   9.750   1.8216   0.03187   0.02482  -0.1769   0.2647   0.6136
  10.000   1.8276   0.03350   0.02646  -0.1751   0.2598   0.6177
  10.250   1.8311   0.03538   0.02833  -0.1732   0.2554   0.6212
  10.500   1.8395   0.03688   0.02990  -0.1718   0.2524   0.6253
  10.750   1.8491   0.03832   0.03141  -0.1706   0.2499   0.6300
  11.000   1.8575   0.03989   0.03303  -0.1693   0.2474   0.6349
  11.250   1.8635   0.04170   0.03488  -0.1679   0.2445   0.6394
  11.500   1.8674   0.04374   0.03695  -0.1664   0.2415   0.6439
  11.750   1.8695   0.04592   0.03914  -0.1648   0.2382   0.6486
  12.000   1.8795   0.04747   0.04079  -0.1639   0.2364   0.6545
  12.250   1.8888   0.04910   0.04253  -0.1630   0.2345   0.6610
  12.500   1.8970   0.05086   0.04438  -0.1621   0.2327   0.6687
  12.750   1.9035   0.05280   0.04640  -0.1611   0.2307   0.6772
  13.000   1.9089   0.05486   0.04854  -0.1602   0.2287   0.6885
  13.250   1.9127   0.05711   0.05087  -0.1592   0.2265   0.7074
  13.500   1.9145   0.05892   0.05296  -0.1576   0.2243   1.0000
  13.750   1.9206   0.06086   0.05492  -0.1566   0.2223   1.0000
  14.000   1.9284   0.06278   0.05692  -0.1560   0.2213   1.0000
  14.250   1.9348   0.06487   0.05910  -0.1553   0.2200   1.0000
  14.500   1.9411   0.06696   0.06127  -0.1547   0.2185   1.0000
  14.750   1.9458   0.06923   0.06361  -0.1541   0.2168   1.0000
  15.000   1.9495   0.07162   0.06605  -0.1534   0.2147   1.0000
  15.250   1.9513   0.07423   0.06870  -0.1528   0.2126   1.0000
  15.500   1.9536   0.07673   0.07122  -0.1521   0.2104   1.0000
  15.750   1.9585   0.07878   0.07327  -0.1513   0.2081   1.0000
  16.000   1.9622   0.08121   0.07578  -0.1509   0.2064   1.0000
  16.250   1.9646   0.08390   0.07859  -0.1506   0.2049   1.0000
  16.500   1.9655   0.08678   0.08157  -0.1503   0.2029   1.0000
  16.750   1.9670   0.08954   0.08442  -0.1501   0.2008   1.0000
  17.000   1.9673   0.09246   0.08740  -0.1499   0.1987   1.0000
  17.250   1.9671   0.09540   0.09038  -0.1497   0.1963   1.0000
  17.500   1.9662   0.09834   0.09332  -0.1494   0.1933   1.0000
  17.750   1.9666   0.10130   0.09639  -0.1494   0.1910   1.0000
  18.000   1.9644   0.10471   0.09992  -0.1496   0.1885   1.0000
  18.250   1.9632   0.10791   0.10322  -0.1498   0.1855   1.0000
  18.500   1.9597   0.11140   0.10676  -0.1500   0.1822   1.0000
  18.750   1.9534   0.11526   0.11062  -0.1503   0.1785   1.0000
  19.000   1.9526   0.11847   0.11396  -0.1508   0.1748   1.0000
  19.250   1.9477   0.12226   0.11784  -0.1514   0.1697   1.0000
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