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GOE 547 AIRFOIL (goe547-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 547 AIRFOIL (goe547-il)
Reynolds number: 500,000
Max Cl/Cd: 105.79 at α=3.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe547-il-500000-n5.txt
Download as CSV file: xf-goe547-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 547 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
  ------ -------- --------- --------- -------- -------- --------
 -12.250  -0.8004   0.03682   0.03411  -0.0988   0.9895   0.0139
 -12.000  -0.7954   0.03107   0.02788  -0.1046   0.9833   0.0143
 -11.750  -0.7668   0.03110   0.02796  -0.1053   0.9804   0.0149
 -11.500  -0.7367   0.03101   0.02787  -0.1065   0.9781   0.0153
 -11.250  -0.7076   0.03041   0.02721  -0.1081   0.9761   0.0158
 -11.000  -0.6868   0.02930   0.02598  -0.1087   0.9711   0.0165
 -10.750  -0.6651   0.02758   0.02402  -0.1099   0.9669   0.0174
 -10.500  -0.6422   0.02531   0.02140  -0.1117   0.9641   0.0184
 -10.250  -0.6238   0.02403   0.01988  -0.1113   0.9573   0.0190
 -10.000  -0.5971   0.02320   0.01899  -0.1122   0.9539   0.0195
  -9.750  -0.5655   0.02274   0.01847  -0.1137   0.9514   0.0200
  -9.500  -0.5402   0.02236   0.01805  -0.1138   0.9442   0.0206
  -9.250  -0.5078   0.02185   0.01744  -0.1154   0.9404   0.0214
  -9.000  -0.4747   0.02096   0.01638  -0.1175   0.9376   0.0224
  -8.750  -0.4476   0.02021   0.01546  -0.1180   0.9320   0.0233
  -8.500  -0.4173   0.01942   0.01450  -0.1192   0.9275   0.0241
  -8.250  -0.3846   0.01883   0.01375  -0.1208   0.9240   0.0247
  -8.000  -0.3555   0.01816   0.01291  -0.1216   0.9188   0.0251
  -7.750  -0.3307   0.01643   0.01095  -0.1221   0.9127   0.0262
  -7.500  -0.3002   0.01571   0.01012  -0.1231   0.9080   0.0269
  -7.250  -0.2741   0.01512   0.00943  -0.1231   0.9015   0.0275
  -7.000  -0.2459   0.01464   0.00885  -0.1235   0.8960   0.0282
  -6.750  -0.2183   0.01412   0.00822  -0.1237   0.8907   0.0288
  -6.500  -0.1929   0.01358   0.00758  -0.1234   0.8843   0.0292
  -6.250  -0.1657   0.01308   0.00696  -0.1235   0.8787   0.0297
  -6.000  -0.1407   0.01262   0.00641  -0.1230   0.8727   0.0301
  -5.750  -0.1148   0.01220   0.00590  -0.1227   0.8669   0.0306
  -5.500  -0.0881   0.01184   0.00545  -0.1226   0.8618   0.0312
  -5.250  -0.0631   0.01153   0.00507  -0.1221   0.8557   0.0318
  -5.000  -0.0368   0.01121   0.00467  -0.1218   0.8499   0.0322
  -4.750  -0.0111   0.01092   0.00431  -0.1214   0.8443   0.0326
  -4.500   0.0146   0.01066   0.00399  -0.1210   0.8385   0.0328
  -4.250   0.0412   0.01042   0.00368  -0.1208   0.8333   0.0331
  -4.000   0.0662   0.01010   0.00331  -0.1202   0.8273   0.0339
  -3.750   0.0922   0.00986   0.00300  -0.1198   0.8211   0.0348
  -3.500   0.1185   0.00967   0.00277  -0.1195   0.8155   0.0356
  -3.250   0.1445   0.00950   0.00256  -0.1191   0.8092   0.0367
  -3.000   0.1713   0.00937   0.00238  -0.1188   0.8035   0.0378
  -2.750   0.1973   0.00923   0.00223  -0.1184   0.7971   0.0392
  -2.500   0.2237   0.00912   0.00209  -0.1181   0.7904   0.0415
  -2.250   0.2500   0.00900   0.00198  -0.1177   0.7842   0.0478
  -2.000   0.2761   0.00887   0.00190  -0.1174   0.7773   0.0653
  -1.750   0.3025   0.00880   0.00181  -0.1170   0.7707   0.0761
  -1.500   0.3286   0.00871   0.00173  -0.1166   0.7634   0.0853
  -1.250   0.3547   0.00861   0.00165  -0.1163   0.7564   0.0995
  -1.000   0.3793   0.00831   0.00160  -0.1157   0.7487   0.1822
  -0.750   0.4053   0.00824   0.00157  -0.1154   0.7415   0.2099
  -0.500   0.4311   0.00816   0.00155  -0.1149   0.7335   0.2355
  -0.250   0.4563   0.00805   0.00154  -0.1144   0.7245   0.2738
   0.000   0.4806   0.00798   0.00153  -0.1137   0.7112   0.3154
   0.250   0.5046   0.00787   0.00154  -0.1129   0.6990   0.3763
   0.750   0.5502   0.00769   0.00164  -0.1108   0.6682   0.5166
   1.000   0.5735   0.00769   0.00169  -0.1098   0.6533   0.5527
   1.250   0.5972   0.00770   0.00174  -0.1088   0.6402   0.5882
   1.500   0.6205   0.00769   0.00181  -0.1079   0.6277   0.6303
   1.750   0.6431   0.00761   0.00187  -0.1067   0.6172   0.6890
   2.250   0.7439   0.00731   0.00218  -0.1167   0.5979   1.0000
   2.500   0.7671   0.00742   0.00226  -0.1157   0.5892   1.0000
   3.000   0.8113   0.00770   0.00244  -0.1132   0.5632   1.0000
   3.250   0.8326   0.00787   0.00255  -0.1118   0.5442   1.0000
   3.500   0.8523   0.00808   0.00267  -0.1100   0.5197   1.0000
   3.750   0.8723   0.00830   0.00280  -0.1084   0.4950   1.0000
   4.000   0.8907   0.00859   0.00298  -0.1065   0.4649   1.0000
   4.250   0.9075   0.00897   0.00319  -0.1042   0.4286   1.0000
   4.500   0.9217   0.00949   0.00348  -0.1016   0.3807   1.0000
   4.750   0.9353   0.01008   0.00382  -0.0989   0.3319   1.0000
   5.000   0.9508   0.01060   0.00415  -0.0966   0.2950   1.0000
   5.250   0.9670   0.01108   0.00448  -0.0944   0.2621   1.0000
   5.500   0.9832   0.01156   0.00481  -0.0923   0.2319   1.0000
   5.750   0.9991   0.01201   0.00512  -0.0901   0.2052   1.0000
   6.000   1.0144   0.01245   0.00544  -0.0878   0.1768   1.0000
   6.250   1.0239   0.01317   0.00591  -0.0845   0.1294   1.0000
   6.500   1.0385   0.01367   0.00632  -0.0821   0.1124   1.0000
   6.750   1.0556   0.01406   0.00669  -0.0802   0.1029   1.0000
   7.500   1.1011   0.01559   0.00801  -0.0737   0.0547   1.0000
   7.750   1.1163   0.01612   0.00852  -0.0717   0.0455   1.0000
   8.000   1.1300   0.01675   0.00909  -0.0694   0.0301   1.0000
   8.250   1.1414   0.01753   0.00976  -0.0669   0.0186   1.0000
   8.500   1.1557   0.01815   0.01040  -0.0648   0.0155   1.0000
   8.750   1.1714   0.01870   0.01100  -0.0630   0.0144   1.0000
   9.000   1.1857   0.01934   0.01170  -0.0610   0.0131   1.0000
   9.250   1.1993   0.02004   0.01245  -0.0590   0.0123   1.0000
   9.500   1.2109   0.02089   0.01336  -0.0568   0.0113   1.0000
   9.750   1.2242   0.02163   0.01418  -0.0548   0.0109   1.0000
  10.000   1.2374   0.02240   0.01501  -0.0530   0.0105   1.0000
  10.250   1.2503   0.02320   0.01587  -0.0512   0.0099   1.0000
  10.500   1.2620   0.02410   0.01685  -0.0493   0.0096   1.0000
  10.750   1.2731   0.02506   0.01787  -0.0474   0.0091   1.0000
  11.000   1.2836   0.02608   0.01895  -0.0456   0.0086   1.0000
  11.250   1.2917   0.02731   0.02024  -0.0436   0.0083   1.0000
  11.500   1.2963   0.02883   0.02185  -0.0414   0.0080   1.0000
  11.750   1.3046   0.03011   0.02321  -0.0396   0.0078   1.0000
  12.000   1.3129   0.03142   0.02461  -0.0379   0.0076   1.0000
  12.250   1.3197   0.03288   0.02616  -0.0362   0.0075   1.0000
  12.500   1.3267   0.03437   0.02776  -0.0347   0.0072   1.0000
  12.750   1.3324   0.03601   0.02949  -0.0332   0.0071   1.0000
  13.000   1.3372   0.03777   0.03134  -0.0317   0.0069   1.0000
  13.250   1.3417   0.03961   0.03327  -0.0304   0.0067   1.0000
  13.500   1.3448   0.04164   0.03541  -0.0291   0.0066   1.0000
  13.750   1.3497   0.04354   0.03739  -0.0281   0.0064   1.0000
  14.000   1.3515   0.04582   0.03977  -0.0271   0.0063   1.0000
  14.250   1.3550   0.04801   0.04204  -0.0264   0.0061   1.0000
  14.500   1.3574   0.05037   0.04449  -0.0257   0.0060   1.0000
  14.750   1.3575   0.05305   0.04727  -0.0252   0.0059   1.0000
  15.000   1.3545   0.05619   0.05050  -0.0248   0.0057   1.0000
  15.250   1.3512   0.05949   0.05394  -0.0245   0.0057   1.0000
  15.500   1.3463   0.06310   0.05766  -0.0245   0.0056   1.0000
  15.750   1.3453   0.06633   0.06102  -0.0247   0.0055   1.0000
  16.000   1.3424   0.06991   0.06473  -0.0250   0.0054   1.0000
  16.250   1.3388   0.07370   0.06866  -0.0256   0.0054   1.0000
  16.500   1.3340   0.07779   0.07290  -0.0264   0.0053   1.0000
  16.750   1.3269   0.08230   0.07754  -0.0275   0.0053   1.0000
  17.000   1.3209   0.08686   0.08224  -0.0289   0.0052   1.0000
  17.250   1.3127   0.09188   0.08741  -0.0305   0.0051   1.0000
  17.500   1.3053   0.09696   0.09263  -0.0325   0.0051   1.0000
  17.750   1.2946   0.10273   0.09855  -0.0348   0.0051   1.0000
  18.000   1.2860   0.10835   0.10432  -0.0374   0.0050   1.0000
  18.250   1.2753   0.11446   0.11057  -0.0402   0.0050   1.0000
  18.500   1.2636   0.12094   0.11720  -0.0435   0.0049   1.0000
  18.750   1.2525   0.12745   0.12385  -0.0469   0.0049   1.0000
  19.000   1.2411   0.13414   0.13068  -0.0506   0.0049   1.0000
  19.250   1.2292   0.14111   0.13779  -0.0546   0.0049   1.0000
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