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GOE 417A (GEW. PLATTE) AIRFOIL (goe417a-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 417A (GEW. PLATTE) AIRFOIL (goe417a-il)
Reynolds number: 1,000,000
Max Cl/Cd: 116.87 at α=1.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe417a-il-1000000-n5.txt
Download as CSV file: xf-goe417a-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 417A (GEW. PLATTE) 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
  ------ -------- --------- --------- -------- -------- --------
 -10.000  -0.3186   0.10804   0.10629  -0.0360   0.9927   0.0083
  -9.750  -0.3094   0.10481   0.10307  -0.0381   0.9913   0.0085
  -9.500  -0.3024   0.10034   0.09859  -0.0410   0.9896   0.0093
  -9.250  -0.2897   0.09736   0.09561  -0.0437   0.9881   0.0095
  -9.000  -0.2744   0.09480   0.09305  -0.0465   0.9867   0.0096
  -8.750  -0.2577   0.09208   0.09033  -0.0497   0.9853   0.0098
  -8.500  -0.2430   0.08984   0.08808  -0.0521   0.9830   0.0103
  -8.250  -0.2321   0.08694   0.08519  -0.0545   0.9794   0.0106
  -8.000  -0.2199   0.08257   0.08081  -0.0590   0.9764   0.0119
  -7.750  -0.1995   0.08009   0.07831  -0.0626   0.9751   0.0121
  -7.500  -0.1821   0.07785   0.07606  -0.0653   0.9724   0.0123
  -7.250  -0.1642   0.07554   0.07375  -0.0680   0.9693   0.0128
  -7.000  -0.1408   0.07162   0.06980  -0.0736   0.9666   0.0146
  -6.750  -0.1164   0.06918   0.06735  -0.0776   0.9651   0.0149
  -6.500  -0.0891   0.06690   0.06506  -0.0820   0.9640   0.0156
  -6.250  -0.0663   0.06434   0.06247  -0.0856   0.9603   0.0171
  -6.000  -0.0274   0.06086   0.05890  -0.0948   0.9558   0.0175
  -5.750  -0.0074   0.05768   0.05571  -0.0968   0.9535   0.0177
  -5.500   0.0156   0.05536   0.05338  -0.0995   0.9501   0.0179
  -5.250   0.0373   0.05319   0.05118  -0.1017   0.9453   0.0180
  -5.000   0.0642   0.05092   0.04887  -0.1050   0.9414   0.0183
  -4.750   0.0885   0.04883   0.04674  -0.1074   0.9362   0.0188
  -4.500   0.1134   0.04668   0.04454  -0.1097   0.9295   0.0192
  -4.250   0.1386   0.04456   0.04236  -0.1118   0.9220   0.0197
  -4.000   0.1644   0.04247   0.04021  -0.1138   0.9140   0.0199
  -3.750   0.1891   0.04049   0.03816  -0.1153   0.9069   0.0200
  -3.500   0.2162   0.03854   0.03612  -0.1170   0.8986   0.0202
  -3.250   0.2415   0.03678   0.03429  -0.1180   0.8903   0.0202
  -3.000   0.2671   0.03506   0.03248  -0.1189   0.8813   0.0202
  -2.750   0.2917   0.03346   0.03081  -0.1194   0.8699   0.0203
  -2.500   0.3156   0.03193   0.02915  -0.1196   0.8500   0.0203
  -2.250   0.3364   0.03073   0.02769  -0.1187   0.7988   0.0203
  -2.000   0.3527   0.02972   0.02636  -0.1168   0.7431   0.0203
  -1.500   0.3938   0.02732   0.02361  -0.1149   0.6909   0.0203
  -1.250   0.4158   0.02607   0.02221  -0.1140   0.6704   0.0203
  -1.000   0.4375   0.02491   0.02090  -0.1130   0.6472   0.0203
  -0.750   0.4590   0.02378   0.01960  -0.1119   0.6209   0.0203
  -0.500   0.4797   0.02275   0.01837  -0.1105   0.5878   0.0203
  -0.250   0.5015   0.02171   0.01712  -0.1091   0.5611   0.0203
   0.000   0.5059   0.00684   0.00223  -0.1027   0.5281   0.0206
   0.250   0.5272   0.00635   0.00167  -0.1020   0.5153   0.0207
   0.500   0.5490   0.00600   0.00122  -0.1013   0.5014   0.0210
   0.750   0.5719   0.00571   0.00083  -0.1006   0.4880   0.0216
   1.000   0.5957   0.00547   0.00047  -0.0997   0.4743   0.0228
   1.250   0.6206   0.00531   0.00018  -0.0987   0.4610   0.0233
   1.500   0.6578   0.01628   0.01083  -0.1011   0.4547   0.0233
   1.750   0.6811   0.01587   0.01025  -0.0998   0.4341   0.0234
   2.000   0.7014   0.01556   0.00967  -0.0980   0.3862   0.0235
   2.250   0.7167   0.01572   0.00931  -0.0955   0.2828   0.0235
   2.500   0.7350   0.01569   0.00892  -0.0934   0.2165   0.0235
   2.750   0.7571   0.01535   0.00841  -0.0921   0.1958   0.0235
   3.000   0.7801   0.01494   0.00790  -0.0909   0.1856   0.0235
   3.250   0.8033   0.01456   0.00741  -0.0898   0.1774   0.0235
   3.500   0.8268   0.01415   0.00691  -0.0887   0.1709   0.0235
   3.750   0.8498   0.01378   0.00643  -0.0875   0.1618   0.0235
   4.000   0.8727   0.01324   0.00581  -0.0865   0.1533   0.0227
   4.250   0.8966   0.01296   0.00541  -0.0855   0.1452   0.0227
   5.250   0.9806   0.01382   0.00565  -0.0799   0.0360   0.0279
   5.500   1.0031   0.01390   0.00568  -0.0788   0.0315   0.0279
   5.750   1.0265   0.01366   0.00544  -0.0778   0.0283   0.0285
   6.000   1.0493   0.01361   0.00541  -0.0768   0.0276   0.0288
   6.250   1.0714   0.01368   0.00552  -0.0756   0.0267   0.0286
   6.500   1.0926   0.01371   0.00560  -0.0743   0.0256   0.0264
   6.750   1.1132   0.01382   0.00571  -0.0728   0.0243   0.0255
   7.000   1.1336   0.01399   0.00588  -0.0713   0.0232   0.0249
   7.250   1.1533   0.01422   0.00612  -0.0697   0.0217   0.0246
   7.500   1.1722   0.01453   0.00647  -0.0679   0.0203   0.0245
   7.750   1.1924   0.01471   0.00669  -0.0664   0.0199   0.0248
   8.000   1.2121   0.01494   0.00695  -0.0648   0.0195   0.0252
   8.250   1.2307   0.01519   0.00724  -0.0631   0.0190   0.0266
   8.500   1.2484   0.01546   0.00755  -0.0611   0.0183   0.0275
   8.750   1.2656   0.01573   0.00787  -0.0591   0.0177   0.0294
   9.000   1.2827   0.01606   0.00821  -0.0570   0.0171   0.0304
   9.250   1.2997   0.01638   0.00852  -0.0551   0.0161   0.0304
   9.500   1.3149   0.01685   0.00902  -0.0527   0.0153   0.0311
   9.750   1.3323   0.01715   0.00934  -0.0509   0.0146   0.0327
  10.000   1.3485   0.01752   0.00980  -0.0489   0.0142   0.0719
  10.250   1.5418   0.01859   0.01208  -0.0881   0.0114   1.0000
  10.500   1.5554   0.01915   0.01269  -0.0855   0.0107   1.0000
  10.750   1.5688   0.01959   0.01318  -0.0829   0.0105   1.0000
  11.000   1.5801   0.01997   0.01361  -0.0798   0.0101   1.0000
  11.250   1.5901   0.02039   0.01409  -0.0766   0.0097   1.0000
  11.500   1.6006   0.02083   0.01458  -0.0735   0.0091   1.0000
  11.750   1.6110   0.02131   0.01508  -0.0705   0.0085   1.0000
  12.000   1.6214   0.02184   0.01564  -0.0676   0.0077   1.0000
  12.250   1.6302   0.02249   0.01634  -0.0645   0.0072   1.0000
  12.500   1.6398   0.02311   0.01704  -0.0616   0.0069   1.0000
  12.750   1.6486   0.02381   0.01779  -0.0587   0.0064   1.0000
  13.000   1.6570   0.02456   0.01860  -0.0558   0.0058   1.0000
  13.250   1.6645   0.02539   0.01949  -0.0529   0.0055   1.0000
  13.500   1.6705   0.02636   0.02052  -0.0499   0.0049   1.0000
  13.750   1.6760   0.02739   0.02163  -0.0470   0.0047   1.0000
  14.000   1.6815   0.02845   0.02277  -0.0443   0.0045   1.0000
  14.250   1.6860   0.02962   0.02404  -0.0415   0.0044   1.0000
  14.500   1.6900   0.03088   0.02539  -0.0389   0.0043   1.0000
  14.750   1.6931   0.03226   0.02686  -0.0364   0.0041   1.0000
  15.000   1.6952   0.03380   0.02851  -0.0340   0.0040   1.0000
  15.250   1.6962   0.03549   0.03030  -0.0317   0.0039   1.0000
  15.500   1.6961   0.03738   0.03229  -0.0296   0.0038   1.0000
  15.750   1.6947   0.03951   0.03453  -0.0277   0.0037   1.0000
  16.000   1.6927   0.04182   0.03694  -0.0261   0.0036   1.0000
  16.250   1.6911   0.04423   0.03946  -0.0249   0.0035   1.0000
  16.500   1.6867   0.04710   0.04243  -0.0239   0.0034   1.0000
  16.750   1.6809   0.05029   0.04574  -0.0233   0.0033   1.0000
  17.000   1.6728   0.05396   0.04954  -0.0230   0.0032   1.0000
  17.250   1.6631   0.05806   0.05378  -0.0232   0.0031   1.0000
  17.500   1.6549   0.06215   0.05799  -0.0237   0.0032   1.0000
  17.750   1.6412   0.06727   0.06325  -0.0247   0.0031   1.0000
  18.000   1.6250   0.07302   0.06915  -0.0263   0.0030   1.0000
  18.250   1.6078   0.07910   0.07537  -0.0282   0.0030   1.0000
  18.500   1.5919   0.08512   0.08153  -0.0303   0.0029   1.0000
  18.750   1.5748   0.09159   0.08814  -0.0328   0.0030   1.0000
  19.000   1.5489   0.09988   0.09658  -0.0363   0.0029   1.0000
  19.250   1.5277   0.10760   0.10445  -0.0397   0.0030   1.0000
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