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GOE 225 (MVA H.35) AIRFOIL (goe225-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 225 (MVA H.35) AIRFOIL (goe225-il)
Reynolds number: 500,000
Max Cl/Cd: 107.48 at α=4.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe225-il-500000-n5.txt
Download as CSV file: xf-goe225-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 225 (MVA H.35) 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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.250  -0.1254   0.10454   0.10135  -0.0860   0.8534   0.0220
 -10.250  -0.3075   0.03786   0.03393  -0.1483   0.8374   0.0258
 -10.000  -0.2703   0.02937   0.02508  -0.1683   0.8341   0.0261
  -9.750  -0.2296   0.02528   0.02075  -0.1791   0.8315   0.0263
  -9.500  -0.1929   0.02298   0.01825  -0.1853   0.8291   0.0266
  -9.250  -0.1596   0.02151   0.01662  -0.1889   0.8266   0.0269
  -9.000  -0.1271   0.02035   0.01531  -0.1916   0.8246   0.0272
  -8.750  -0.0950   0.01936   0.01416  -0.1939   0.8225   0.0276
  -8.500  -0.0630   0.01840   0.01308  -0.1960   0.8201   0.0280
  -8.250  -0.0312   0.01754   0.01210  -0.1977   0.8174   0.0283
  -8.000   0.0004   0.01678   0.01122  -0.1993   0.8151   0.0286
  -7.750   0.0318   0.01611   0.01043  -0.2006   0.8128   0.0289
  -7.500   0.0631   0.01551   0.00972  -0.2018   0.8103   0.0291
  -7.250   0.0941   0.01498   0.00908  -0.2028   0.8076   0.0294
  -7.000   0.1251   0.01452   0.00850  -0.2037   0.8048   0.0297
  -6.750   0.1561   0.01408   0.00799  -0.2046   0.8022   0.0299
  -6.500   0.1875   0.01353   0.00741  -0.2057   0.7992   0.0303
  -6.250   0.2187   0.01304   0.00688  -0.2067   0.7956   0.0308
  -6.000   0.2497   0.01266   0.00644  -0.2075   0.7921   0.0313
  -5.750   0.2805   0.01234   0.00607  -0.2082   0.7891   0.0319
  -5.500   0.3114   0.01206   0.00573  -0.2089   0.7865   0.0326
  -5.250   0.3423   0.01177   0.00541  -0.2096   0.7836   0.0332
  -5.000   0.3731   0.01151   0.00512  -0.2103   0.7801   0.0337
  -4.750   0.4037   0.01128   0.00484  -0.2108   0.7763   0.0343
  -4.500   0.4341   0.01107   0.00457  -0.2113   0.7725   0.0349
  -4.250   0.4649   0.01084   0.00428  -0.2119   0.7690   0.0359
  -4.000   0.4954   0.01063   0.00407  -0.2125   0.7646   0.0371
  -3.750   0.5257   0.01045   0.00387  -0.2129   0.7594   0.0386
  -3.500   0.5557   0.01031   0.00367  -0.2133   0.7541   0.0405
  -3.250   0.5861   0.01011   0.00349  -0.2138   0.7483   0.0455
  -3.000   0.6164   0.00990   0.00337  -0.2143   0.7413   0.0644
  -2.750   0.6458   0.00983   0.00329  -0.2145   0.7336   0.0777
  -2.500   0.6751   0.00977   0.00322  -0.2147   0.7226   0.0854
  -2.250   0.7041   0.00973   0.00314  -0.2148   0.7087   0.0908
  -2.000   0.7325   0.00971   0.00305  -0.2148   0.6894   0.0955
  -1.750   0.7596   0.00980   0.00298  -0.2145   0.6616   0.0996
  -1.500   0.7858   0.00998   0.00297  -0.2141   0.6304   0.1031
  -1.250   0.8120   0.01017   0.00301  -0.2138   0.6048   0.1088
  -1.000   0.8388   0.01035   0.00307  -0.2135   0.5861   0.1136
  -0.750   0.8658   0.01049   0.00313  -0.2133   0.5718   0.1185
  -0.500   0.8935   0.01058   0.00318  -0.2133   0.5597   0.1271
  -0.250   0.9211   0.01066   0.00325  -0.2133   0.5496   0.1432
   0.000   0.9491   0.01065   0.00336  -0.2135   0.5406   0.2049
   0.250   0.9767   0.01074   0.00348  -0.2134   0.5336   0.2402
   0.500   1.0042   0.01085   0.00359  -0.2133   0.5266   0.2604
   0.750   1.0311   0.01100   0.00373  -0.2131   0.5199   0.2763
   1.000   1.0586   0.01110   0.00384  -0.2130   0.5144   0.2876
   1.250   1.0859   0.01123   0.00395  -0.2129   0.5087   0.2975
   1.500   1.1126   0.01138   0.00409  -0.2127   0.5031   0.3075
   1.750   1.1396   0.01151   0.00422  -0.2125   0.4981   0.3168
   2.000   1.1667   0.01161   0.00436  -0.2123   0.4923   0.3274
   2.250   1.1924   0.01180   0.00453  -0.2119   0.4846   0.3387
   2.500   1.2188   0.01194   0.00467  -0.2116   0.4765   0.3512
   2.750   1.2445   0.01211   0.00486  -0.2112   0.4684   0.3666
   3.000   1.2705   0.01226   0.00503  -0.2109   0.4626   0.3836
   3.250   1.2967   0.01239   0.00521  -0.2106   0.4566   0.4042
   3.500   1.3220   0.01257   0.00542  -0.2101   0.4507   0.4255
   3.750   1.3474   0.01273   0.00563  -0.2097   0.4455   0.4477
   4.000   1.3731   0.01288   0.00583  -0.2093   0.4402   0.4689
   4.250   1.3977   0.01308   0.00605  -0.2087   0.4342   0.4846
   4.500   1.4220   0.01329   0.00627  -0.2081   0.4284   0.4979
   4.750   1.4467   0.01346   0.00649  -0.2075   0.4221   0.5103
   5.000   1.4700   0.01370   0.00674  -0.2067   0.4160   0.5218
   5.250   1.4937   0.01391   0.00699  -0.2060   0.4103   0.5341
   5.500   1.5167   0.01413   0.00724  -0.2051   0.4033   0.5474
   5.750   1.5379   0.01442   0.00755  -0.2039   0.3954   0.5602
   6.000   1.5586   0.01471   0.00785  -0.2027   0.3849   0.5729
   6.250   1.5775   0.01505   0.00819  -0.2011   0.3738   0.5863
   6.500   1.5925   0.01544   0.00859  -0.1987   0.3630   0.6019
   6.750   1.6094   0.01585   0.00903  -0.1969   0.3504   0.6244
   7.000   1.6269   0.01627   0.00953  -0.1952   0.3368   0.6743
   7.250   1.6388   0.01645   0.00999  -0.1923   0.3238   1.0000
   7.500   1.6533   0.01712   0.01060  -0.1902   0.3085   1.0000
   7.750   1.6672   0.01784   0.01125  -0.1881   0.2931   1.0000
   8.000   1.6807   0.01862   0.01196  -0.1859   0.2785   1.0000
   8.250   1.6935   0.01946   0.01274  -0.1838   0.2638   1.0000
   8.500   1.7059   0.02035   0.01358  -0.1816   0.2503   1.0000
   8.750   1.7184   0.02126   0.01444  -0.1795   0.2380   1.0000
   9.000   1.7322   0.02210   0.01527  -0.1777   0.2283   1.0000
   9.250   1.7446   0.02305   0.01620  -0.1757   0.2196   1.0000
   9.500   1.7573   0.02400   0.01713  -0.1738   0.2101   1.0000
   9.750   1.7682   0.02508   0.01819  -0.1718   0.2002   1.0000
  10.000   1.7773   0.02632   0.01939  -0.1696   0.1892   1.0000
  10.250   1.7866   0.02757   0.02060  -0.1675   0.1775   1.0000
  10.500   1.7964   0.02878   0.02181  -0.1655   0.1683   1.0000
  10.750   1.8048   0.03013   0.02314  -0.1634   0.1594   1.0000
  11.000   1.8134   0.03149   0.02449  -0.1614   0.1501   1.0000
  11.250   1.8210   0.03295   0.02594  -0.1594   0.1408   1.0000
  11.500   1.8257   0.03464   0.02760  -0.1571   0.1293   1.0000
  11.750   1.8265   0.03671   0.02961  -0.1546   0.1135   1.0000
  12.000   1.8099   0.04038   0.03305  -0.1508   0.0766   1.0000
  12.250   1.7990   0.04371   0.03630  -0.1477   0.0598   1.0000
  12.500   1.7993   0.04614   0.03876  -0.1457   0.0545   1.0000
  12.750   1.8003   0.04856   0.04122  -0.1439   0.0508   1.0000
  13.000   1.8030   0.05086   0.04360  -0.1423   0.0482   1.0000
  13.250   1.8058   0.05323   0.04603  -0.1409   0.0458   1.0000
  13.500   1.8066   0.05588   0.04875  -0.1395   0.0436   1.0000
  13.750   1.8069   0.05867   0.05161  -0.1382   0.0417   1.0000
  14.000   1.8097   0.06122   0.05425  -0.1371   0.0400   1.0000
  14.250   1.8103   0.06410   0.05721  -0.1361   0.0381   1.0000
  14.500   1.8086   0.06731   0.06048  -0.1352   0.0363   1.0000
  14.750   1.8077   0.07050   0.06376  -0.1344   0.0347   1.0000
  15.000   1.8072   0.07370   0.06704  -0.1337   0.0330   1.0000
  15.250   1.8046   0.07721   0.07063  -0.1332   0.0313   1.0000
  15.500   1.8010   0.08089   0.07439  -0.1327   0.0298   1.0000
  15.750   1.7986   0.08444   0.07803  -0.1324   0.0284   1.0000
  16.000   1.7947   0.08824   0.08191  -0.1322   0.0268   1.0000
  16.250   1.7892   0.09229   0.08603  -0.1320   0.0255   1.0000
  16.500   1.7855   0.09612   0.08995  -0.1320   0.0242   1.0000
  16.750   1.7804   0.10016   0.09408  -0.1321   0.0229   1.0000
  17.000   1.7737   0.10444   0.09844  -0.1323   0.0218   1.0000
  17.250   1.7680   0.10861   0.10270  -0.1327   0.0209   1.0000
  17.500   1.7626   0.11278   0.10696  -0.1331   0.0199   1.0000
  17.750   1.7567   0.11705   0.11131  -0.1337   0.0189   1.0000
  18.000   1.7496   0.12156   0.11589  -0.1345   0.0182   1.0000
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