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GOE 633 AIRFOIL (goe633-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 633 AIRFOIL (goe633-il)
Reynolds number: 1,000,000
Max Cl/Cd: 102.63 at α=7.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe633-il-1000000-n5.txt
Download as CSV file: xf-goe633-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 633 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
  ------ -------- --------- --------- -------- -------- --------
 -16.000  -0.7889   0.09551   0.09316  -0.0320   1.0000   0.0211
 -15.750  -0.8573   0.08029   0.07772  -0.0420   1.0000   0.0212
 -15.500  -0.8998   0.07040   0.06770  -0.0487   1.0000   0.0212
 -15.250  -0.9461   0.06005   0.05720  -0.0562   1.0000   0.0212
 -15.000  -0.9878   0.04940   0.04639  -0.0650   1.0000   0.0212
 -14.750  -1.0175   0.03701   0.03366  -0.0797   1.0000   0.0212
 -14.500  -1.0262   0.03395   0.03046  -0.0800   1.0000   0.0212
 -14.250  -0.9775   0.03064   0.02684  -0.0902   0.9039   0.0214
 -14.000  -0.9831   0.02963   0.02539  -0.0866   0.8127   0.0215
 -13.750  -0.9827   0.02862   0.02422  -0.0834   0.7918   0.0216
 -13.500  -0.9810   0.02766   0.02311  -0.0801   0.7782   0.0217
 -13.250  -0.9793   0.02672   0.02205  -0.0766   0.7666   0.0217
 -13.000  -0.9705   0.02589   0.02109  -0.0741   0.7580   0.0218
 -12.750  -0.9588   0.02507   0.02015  -0.0719   0.7492   0.0218
 -12.500  -0.9451   0.02429   0.01927  -0.0700   0.7420   0.0219
 -12.250  -0.9302   0.02353   0.01840  -0.0682   0.7348   0.0220
 -12.000  -0.9155   0.02272   0.01748  -0.0664   0.7284   0.0220
 -11.750  -0.9019   0.02171   0.01636  -0.0644   0.7227   0.0222
 -11.500  -0.8859   0.02087   0.01542  -0.0627   0.7163   0.0223
 -11.250  -0.8681   0.02016   0.01463  -0.0612   0.7105   0.0225
 -11.000  -0.8487   0.01951   0.01392  -0.0598   0.7053   0.0226
 -10.750  -0.8282   0.01894   0.01329  -0.0586   0.6999   0.0227
 -10.500  -0.8069   0.01844   0.01271  -0.0575   0.6947   0.0229
 -10.250  -0.7851   0.01794   0.01215  -0.0564   0.6899   0.0230
 -10.000  -0.7629   0.01745   0.01160  -0.0554   0.6845   0.0231
  -9.750  -0.7403   0.01700   0.01109  -0.0544   0.6791   0.0233
  -9.500  -0.7173   0.01659   0.01060  -0.0535   0.6744   0.0234
  -9.250  -0.6933   0.01620   0.01017  -0.0527   0.6703   0.0237
  -9.000  -0.6694   0.01581   0.00972  -0.0518   0.6654   0.0239
  -8.750  -0.6454   0.01543   0.00929  -0.0510   0.6601   0.0241
  -8.500  -0.6213   0.01505   0.00884  -0.0502   0.6554   0.0242
  -8.250  -0.5968   0.01467   0.00840  -0.0494   0.6509   0.0244
  -8.000  -0.5722   0.01430   0.00798  -0.0487   0.6462   0.0246
  -7.750  -0.5474   0.01395   0.00757  -0.0480   0.6416   0.0247
  -7.500  -0.5222   0.01364   0.00720  -0.0473   0.6373   0.0249
  -7.250  -0.4968   0.01331   0.00684  -0.0467   0.6327   0.0251
  -7.000  -0.4712   0.01302   0.00648  -0.0460   0.6275   0.0253
  -6.750  -0.4456   0.01274   0.00615  -0.0454   0.6226   0.0254
  -6.500  -0.4195   0.01248   0.00585  -0.0449   0.6186   0.0256
  -6.250  -0.3932   0.01222   0.00556  -0.0444   0.6138   0.0257
  -6.000  -0.3669   0.01199   0.00528  -0.0439   0.6075   0.0258
  -5.750  -0.3412   0.01168   0.00491  -0.0432   0.6010   0.0261
  -5.500  -0.3151   0.01138   0.00457  -0.0427   0.5943   0.0264
  -5.250  -0.2888   0.01115   0.00429  -0.0422   0.5879   0.0267
  -5.000  -0.2621   0.01094   0.00405  -0.0417   0.5819   0.0271
  -4.750  -0.2352   0.01075   0.00383  -0.0413   0.5741   0.0274
  -4.500  -0.2083   0.01059   0.00363  -0.0409   0.5671   0.0278
  -4.250  -0.1811   0.01043   0.00344  -0.0405   0.5609   0.0282
  -4.000  -0.1539   0.01029   0.00327  -0.0402   0.5548   0.0286
  -3.750  -0.1267   0.01015   0.00310  -0.0398   0.5494   0.0291
  -3.500  -0.0992   0.01002   0.00294  -0.0395   0.5437   0.0294
  -3.250  -0.0719   0.00990   0.00280  -0.0392   0.5383   0.0298
  -3.000  -0.0445   0.00980   0.00267  -0.0388   0.5335   0.0301
  -2.750  -0.0170   0.00965   0.00251  -0.0385   0.5286   0.0307
  -2.500   0.0103   0.00953   0.00237  -0.0382   0.5224   0.0315
  -2.250   0.0376   0.00944   0.00226  -0.0378   0.5164   0.0324
  -2.000   0.0652   0.00935   0.00216  -0.0375   0.5104   0.0334
  -1.750   0.0926   0.00928   0.00207  -0.0372   0.5043   0.0344
  -1.500   0.1200   0.00921   0.00199  -0.0369   0.4988   0.0364
  -1.250   0.1475   0.00912   0.00191  -0.0366   0.4930   0.0394
  -1.000   0.1740   0.00896   0.00180  -0.0362   0.4862   0.0584
  -0.750   0.1999   0.00873   0.00172  -0.0357   0.4798   0.1026
  -0.500   0.2269   0.00866   0.00168  -0.0353   0.4714   0.1152
  -0.250   0.2536   0.00861   0.00165  -0.0349   0.4632   0.1292
   0.000   0.2797   0.00852   0.00164  -0.0344   0.4526   0.1600
   0.250   0.3064   0.00851   0.00166  -0.0341   0.4409   0.1789
   0.500   0.3331   0.00857   0.00168  -0.0337   0.4266   0.1878
   0.750   0.3595   0.00861   0.00171  -0.0332   0.4134   0.1981
   1.000   0.3861   0.00870   0.00174  -0.0328   0.3998   0.2047
   1.250   0.4125   0.00876   0.00179  -0.0324   0.3864   0.2124
   1.500   0.4388   0.00885   0.00184  -0.0320   0.3731   0.2194
   1.750   0.4650   0.00895   0.00190  -0.0316   0.3607   0.2246
   2.000   0.4908   0.00905   0.00198  -0.0311   0.3486   0.2338
   2.250   0.5170   0.00914   0.00204  -0.0306   0.3383   0.2413
   2.500   0.5431   0.00922   0.00212  -0.0302   0.3305   0.2501
   2.750   0.5694   0.00929   0.00219  -0.0298   0.3235   0.2586
   3.000   0.5952   0.00938   0.00228  -0.0293   0.3162   0.2686
   3.250   0.6216   0.00942   0.00235  -0.0289   0.3116   0.2824
   3.750   0.6727   0.00955   0.00254  -0.0279   0.3007   0.3201
   4.000   0.6980   0.00954   0.00263  -0.0273   0.2967   0.3564
   4.250   0.7154   0.00911   0.00275  -0.0254   0.2924   0.5692
   4.500   0.7267   0.00827   0.00294  -0.0216   0.2886   0.9323
   4.750   0.7601   0.00848   0.00313  -0.0228   0.2831   0.9518
   5.000   0.7951   0.00863   0.00328  -0.0242   0.2793   0.9582
   5.250   0.8266   0.00879   0.00343  -0.0250   0.2743   0.9631
   5.500   0.8502   0.00896   0.00357  -0.0241   0.2687   0.9685
   5.750   0.8870   0.00916   0.00375  -0.0261   0.2634   0.9706
   6.000   0.9219   0.00936   0.00393  -0.0277   0.2569   0.9729
   6.250   0.9528   0.00959   0.00412  -0.0284   0.2509   0.9751
   6.500   0.9819   0.00975   0.00428  -0.0288   0.2464   0.9773
   6.750   1.0074   0.00994   0.00445  -0.0284   0.2404   0.9801
   7.000   1.0345   0.01018   0.00465  -0.0284   0.2336   0.9819
   7.250   1.0663   0.01041   0.00486  -0.0294   0.2252   0.9829
   7.500   1.0981   0.01070   0.00511  -0.0306   0.2157   0.9843
   7.750   1.1303   0.01108   0.00541  -0.0319   0.2020   0.9864
   8.000   1.1585   0.01155   0.00578  -0.0324   0.1833   0.9887
   8.250   1.1832   0.01212   0.00623  -0.0324   0.1637   0.9913
   8.500   1.2053   0.01267   0.00669  -0.0319   0.1479   0.9932
   8.750   1.2343   0.01315   0.00711  -0.0327   0.1370   0.9946
   9.000   1.2610   0.01359   0.00751  -0.0331   0.1291   0.9960
   9.250   1.2854   0.01404   0.00793  -0.0330   0.1231   0.9973
   9.500   1.3106   0.01439   0.00829  -0.0331   0.1198   0.9984
   9.750   1.3357   0.01476   0.00866  -0.0331   0.1174   0.9993
  10.000   1.3570   0.01518   0.00908  -0.0324   0.1142   1.0000
  10.250   1.3615   0.01554   0.00945  -0.0283   0.1121   1.0000
  10.500   1.3590   0.01589   0.00982  -0.0230   0.1099   1.0000
  10.750   1.3627   0.01628   0.01025  -0.0190   0.1086   1.0000
  11.000   1.3710   0.01670   0.01071  -0.0161   0.1077   1.0000
  11.250   1.3804   0.01720   0.01125  -0.0136   0.1067   1.0000
  11.500   1.3901   0.01781   0.01189  -0.0114   0.1051   1.0000
  11.750   1.4004   0.01852   0.01263  -0.0096   0.1036   1.0000
  12.000   1.4104   0.01936   0.01350  -0.0080   0.1016   1.0000
  12.250   1.4202   0.02033   0.01448  -0.0066   0.0995   1.0000
  12.500   1.4303   0.02134   0.01553  -0.0053   0.0976   1.0000
  12.750   1.4416   0.02234   0.01656  -0.0043   0.0958   1.0000
  13.000   1.4545   0.02326   0.01753  -0.0035   0.0945   1.0000
  13.250   1.4659   0.02430   0.01861  -0.0026   0.0920   1.0000
  13.500   1.4753   0.02554   0.01986  -0.0017   0.0890   1.0000
  14.000   1.4910   0.02834   0.02271   0.0000   0.0821   1.0000
  14.250   1.4932   0.03025   0.02459   0.0009   0.0739   1.0000
  14.500   1.4872   0.03290   0.02716   0.0019   0.0618   1.0000
  14.750   1.4810   0.03565   0.02990   0.0028   0.0542   1.0000
  15.000   1.4752   0.03847   0.03273   0.0035   0.0483   1.0000
  15.250   1.4690   0.04143   0.03571   0.0040   0.0430   1.0000
  15.500   1.4631   0.04451   0.03882   0.0043   0.0381   1.0000
  15.750   1.4517   0.04830   0.04262   0.0044   0.0307   1.0000
  16.250   1.4233   0.05692   0.05127   0.0039   0.0178   1.0000
  16.500   1.4196   0.06023   0.05463   0.0036   0.0166   1.0000
  16.750   1.4160   0.06356   0.05803   0.0031   0.0158   1.0000
  17.000   1.4102   0.06724   0.06177   0.0026   0.0148   1.0000
  17.250   1.4055   0.07084   0.06544   0.0020   0.0141   1.0000
  17.500   1.4016   0.07439   0.06907   0.0013   0.0138   1.0000
  17.750   1.3951   0.07831   0.07306   0.0004   0.0133   1.0000
  18.000   1.3884   0.08234   0.07717  -0.0005   0.0128   1.0000
  18.250   1.3819   0.08642   0.08133  -0.0015   0.0126   1.0000
  18.500   1.3764   0.09040   0.08539  -0.0026   0.0123   1.0000
  18.750   1.3704   0.09447   0.08953  -0.0037   0.0121   1.0000
  19.000   1.3642   0.09860   0.09374  -0.0049   0.0117   1.0000
  19.250   1.3571   0.10293   0.09815  -0.0063   0.0117   1.0000
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