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GOE 225 (MVA H.35) AIRFOIL (goe225-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 225 (MVA H.35) AIRFOIL (goe225-il)
Reynolds number: 1,000,000
Max Cl/Cd: 128.99 at α=4.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe225-il-1000000-n5.txt
Download as CSV file: xf-goe225-il-1000000-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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.000  -0.4472   0.05510   0.05203  -0.1160   0.8243   0.0217
 -11.750  -0.4638   0.04501   0.04175  -0.1301   0.8208   0.0218
 -11.500  -0.4504   0.03695   0.03350  -0.1454   0.8179   0.0218
 -11.250  -0.4193   0.02923   0.02553  -0.1628   0.8148   0.0220
 -11.000  -0.3803   0.02428   0.02036  -0.1749   0.8120   0.0223
 -10.750  -0.3412   0.02117   0.01708  -0.1830   0.8097   0.0225
 -10.500  -0.3053   0.01932   0.01507  -0.1879   0.8076   0.0227
 -10.250  -0.2725   0.01821   0.01384  -0.1908   0.8054   0.0228
 -10.000  -0.2403   0.01729   0.01283  -0.1930   0.8036   0.0230
  -9.750  -0.2084   0.01650   0.01196  -0.1949   0.8020   0.0232
  -9.500  -0.1767   0.01579   0.01118  -0.1965   0.8003   0.0234
  -9.250  -0.1454   0.01519   0.01051  -0.1979   0.7983   0.0237
  -9.000  -0.1141   0.01465   0.00989  -0.1992   0.7962   0.0240
  -8.750  -0.0829   0.01412   0.00928  -0.2003   0.7941   0.0242
  -8.500  -0.0518   0.01361   0.00869  -0.2014   0.7918   0.0244
  -8.250  -0.0208   0.01316   0.00815  -0.2024   0.7892   0.0246
  -8.000   0.0102   0.01275   0.00765  -0.2033   0.7869   0.0248
  -7.750   0.0414   0.01234   0.00720  -0.2043   0.7853   0.0250
  -7.500   0.0724   0.01197   0.00677  -0.2051   0.7832   0.0252
  -7.250   0.1034   0.01163   0.00639  -0.2059   0.7804   0.0254
  -7.000   0.1342   0.01133   0.00603  -0.2066   0.7772   0.0255
  -6.750   0.1649   0.01106   0.00569  -0.2072   0.7739   0.0257
  -6.500   0.1961   0.01067   0.00523  -0.2081   0.7707   0.0260
  -6.250   0.2274   0.01032   0.00484  -0.2089   0.7679   0.0264
  -6.000   0.2584   0.01004   0.00454  -0.2096   0.7649   0.0268
  -5.750   0.2892   0.00981   0.00427  -0.2103   0.7614   0.0272
  -5.500   0.3198   0.00960   0.00403  -0.2108   0.7577   0.0276
  -5.250   0.3503   0.00943   0.00381  -0.2113   0.7542   0.0280
  -5.000   0.3808   0.00926   0.00361  -0.2118   0.7506   0.0285
  -4.750   0.4114   0.00909   0.00342  -0.2123   0.7456   0.0290
  -4.500   0.4417   0.00895   0.00324  -0.2127   0.7396   0.0294
  -4.250   0.4719   0.00883   0.00307  -0.2131   0.7338   0.0298
  -4.000   0.5021   0.00871   0.00291  -0.2136   0.7259   0.0302
  -3.750   0.5322   0.00858   0.00273  -0.2139   0.7154   0.0310
  -3.500   0.5617   0.00851   0.00259  -0.2142   0.6980   0.0320
  -3.250   0.5901   0.00855   0.00249  -0.2142   0.6685   0.0330
  -3.000   0.6176   0.00871   0.00246  -0.2141   0.6329   0.0342
  -2.750   0.6451   0.00887   0.00246  -0.2140   0.6025   0.0364
  -2.500   0.6733   0.00896   0.00245  -0.2141   0.5795   0.0417
  -2.250   0.7021   0.00894   0.00246  -0.2144   0.5625   0.0704
  -2.000   0.7306   0.00902   0.00249  -0.2145   0.5502   0.0787
  -1.750   0.7592   0.00908   0.00253  -0.2146   0.5401   0.0851
  -1.500   0.7878   0.00915   0.00256  -0.2147   0.5318   0.0880
  -1.250   0.8164   0.00921   0.00258  -0.2148   0.5237   0.0918
  -1.000   0.8449   0.00927   0.00262  -0.2149   0.5170   0.0960
  -0.750   0.8737   0.00931   0.00264  -0.2150   0.5117   0.0993
  -0.500   0.9022   0.00937   0.00268  -0.2151   0.5059   0.1024
  -0.250   0.9305   0.00943   0.00272  -0.2151   0.5003   0.1082
   0.000   0.9593   0.00946   0.00276  -0.2153   0.4958   0.1137
   0.250   0.9878   0.00950   0.00280  -0.2154   0.4910   0.1213
   0.500   1.0161   0.00953   0.00286  -0.2155   0.4859   0.1402
   0.750   1.0452   0.00945   0.00295  -0.2159   0.4814   0.2209
   1.000   1.0736   0.00949   0.00303  -0.2160   0.4770   0.2434
   1.250   1.1013   0.00958   0.00313  -0.2159   0.4704   0.2585
   1.500   1.1286   0.00970   0.00324  -0.2158   0.4626   0.2710
   1.750   1.1560   0.00982   0.00334  -0.2157   0.4537   0.2812
   2.000   1.1830   0.00995   0.00346  -0.2155   0.4464   0.2895
   2.250   1.2105   0.01005   0.00355  -0.2155   0.4405   0.2966
   2.500   1.2375   0.01018   0.00368  -0.2153   0.4343   0.3043
   2.750   1.2644   0.01030   0.00380  -0.2151   0.4293   0.3142
   3.000   1.2917   0.01038   0.00392  -0.2150   0.4246   0.3274
   3.250   1.3183   0.01051   0.00406  -0.2148   0.4183   0.3388
   3.500   1.3445   0.01066   0.00421  -0.2145   0.4121   0.3507
   3.750   1.3712   0.01078   0.00436  -0.2143   0.4063   0.3666
   4.000   1.3971   0.01093   0.00454  -0.2140   0.4001   0.3895
   4.250   1.4229   0.01107   0.00472  -0.2137   0.3944   0.4137
   4.500   1.4485   0.01123   0.00492  -0.2133   0.3870   0.4408
   4.750   1.4730   0.01144   0.00514  -0.2127   0.3788   0.4602
   5.000   1.4970   0.01168   0.00536  -0.2120   0.3679   0.4734
   5.250   1.5201   0.01196   0.00561  -0.2112   0.3553   0.4841
   5.500   1.5424   0.01228   0.00589  -0.2102   0.3428   0.4949
   5.750   1.5638   0.01261   0.00619  -0.2091   0.3301   0.5044
   6.000   1.5835   0.01303   0.00653  -0.2077   0.3134   0.5141
   6.250   1.6012   0.01351   0.00694  -0.2059   0.2935   0.5245
   6.500   1.6176   0.01402   0.00737  -0.2038   0.2754   0.5344
   6.750   1.6309   0.01451   0.00781  -0.2012   0.2610   0.5444
   7.000   1.6462   0.01503   0.00829  -0.1990   0.2481   0.5536
   7.250   1.6616   0.01560   0.00882  -0.1969   0.2351   0.5641
   7.500   1.6772   0.01618   0.00938  -0.1949   0.2228   0.5760
   7.750   1.6942   0.01670   0.00990  -0.1932   0.2136   0.5915
   8.000   1.7102   0.01729   0.01049  -0.1914   0.2050   0.6122
   8.250   1.7282   0.01777   0.01104  -0.1899   0.1981   0.6486
   8.500   1.7409   0.01804   0.01173  -0.1876   0.1891   1.0000
   8.750   1.7548   0.01881   0.01245  -0.1856   0.1781   1.0000
   9.000   1.7687   0.01959   0.01319  -0.1837   0.1681   1.0000
   9.250   1.7817   0.02043   0.01399  -0.1816   0.1591   1.0000
   9.500   1.7932   0.02140   0.01491  -0.1795   0.1479   1.0000
   9.750   1.8039   0.02245   0.01590  -0.1773   0.1358   1.0000
  10.000   1.8130   0.02362   0.01701  -0.1749   0.1231   1.0000
  10.250   1.8186   0.02507   0.01836  -0.1722   0.1073   1.0000
  10.500   1.8036   0.02808   0.02111  -0.1672   0.0655   1.0000
  10.750   1.8068   0.02982   0.02282  -0.1645   0.0551   1.0000
  11.000   1.8139   0.03129   0.02431  -0.1624   0.0504   1.0000
  11.250   1.8235   0.03259   0.02564  -0.1605   0.0474   1.0000
  11.500   1.8323   0.03396   0.02704  -0.1587   0.0450   1.0000
  11.750   1.8395   0.03549   0.02860  -0.1567   0.0426   1.0000
  12.000   1.8486   0.03690   0.03004  -0.1550   0.0408   1.0000
  12.250   1.8567   0.03841   0.03160  -0.1534   0.0389   1.0000
  12.500   1.8631   0.04012   0.03333  -0.1516   0.0366   1.0000
  12.750   1.8694   0.04186   0.03511  -0.1499   0.0348   1.0000
  13.000   1.8767   0.04355   0.03685  -0.1483   0.0331   1.0000
  13.250   1.8814   0.04554   0.03887  -0.1467   0.0311   1.0000
  13.500   1.8866   0.04752   0.04089  -0.1451   0.0295   1.0000
  13.750   1.8912   0.04961   0.04303  -0.1437   0.0276   1.0000
  14.000   1.8932   0.05200   0.04545  -0.1422   0.0255   1.0000
  14.250   1.8965   0.05432   0.04783  -0.1408   0.0236   1.0000
  14.500   1.8975   0.05697   0.05051  -0.1395   0.0217   1.0000
  14.750   1.8987   0.05965   0.05325  -0.1384   0.0202   1.0000
  15.000   1.8984   0.06258   0.05623  -0.1373   0.0187   1.0000
  15.250   1.8976   0.06561   0.05932  -0.1363   0.0176   1.0000
  15.500   1.8966   0.06872   0.06250  -0.1354   0.0166   1.0000
  15.750   1.8945   0.07204   0.06589  -0.1347   0.0158   1.0000
  16.000   1.8911   0.07560   0.06952  -0.1340   0.0150   1.0000
  16.250   1.8889   0.07903   0.07303  -0.1335   0.0145   1.0000
  16.500   1.8854   0.08264   0.07672  -0.1331   0.0140   1.0000
  16.750   1.8809   0.08642   0.08058  -0.1327   0.0134   1.0000
  17.000   1.8754   0.09038   0.08462  -0.1325   0.0130   1.0000
  17.250   1.8688   0.09453   0.08885  -0.1324   0.0125   1.0000
  17.500   1.8631   0.09859   0.09299  -0.1325   0.0121   1.0000
  17.750   1.8577   0.10260   0.09709  -0.1326   0.0118   1.0000
  18.000   1.8522   0.10661   0.10119  -0.1328   0.0115   1.0000
  18.250   1.8464   0.11071   0.10538  -0.1331   0.0112   1.0000
  18.500   1.8395   0.11503   0.10978  -0.1336   0.0109   1.0000
  18.750   1.8330   0.11932   0.11415  -0.1343   0.0106   1.0000
  19.000   1.8270   0.12354   0.11845  -0.1350   0.0104   1.0000
  19.250   1.8194   0.12806   0.12305  -0.1359   0.0101   1.0000
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