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GOE 344 (PFALZ 71) AIRFOIL (goe344-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 344 (PFALZ 71) AIRFOIL (goe344-il)
Reynolds number: 1,000,000
Max Cl/Cd: 95.3 at α=5.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe344-il-1000000.txt
Download as CSV file: xf-goe344-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 344 (PFALZ 71) 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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.000  -0.5548   0.13597   0.13417   0.0054   1.0000   0.0142
 -11.750  -0.5476   0.13341   0.13162   0.0046   1.0000   0.0146
 -11.500  -0.9849   0.03001   0.02722  -0.0482   1.0000   0.0129
 -11.250  -0.9721   0.02724   0.02418  -0.0474   1.0000   0.0133
 -11.000  -0.9553   0.02547   0.02220  -0.0464   1.0000   0.0135
 -10.750  -0.9424   0.02293   0.01934  -0.0452   1.0000   0.0140
 -10.500  -0.9230   0.02178   0.01811  -0.0442   1.0000   0.0145
 -10.250  -0.9001   0.02139   0.01768  -0.0434   1.0000   0.0149
 -10.000  -0.8768   0.02107   0.01733  -0.0426   1.0000   0.0154
  -9.750  -0.8540   0.02063   0.01684  -0.0418   1.0000   0.0159
  -9.500  -0.8317   0.02006   0.01617  -0.0409   1.0000   0.0165
  -9.250  -0.8088   0.01961   0.01562  -0.0400   1.0000   0.0170
  -9.000  -0.7850   0.01940   0.01533  -0.0392   1.0000   0.0173
  -8.750  -0.7671   0.01764   0.01337  -0.0379   1.0000   0.0182
  -8.500  -0.7436   0.01743   0.01315  -0.0371   1.0000   0.0187
  -8.250  -0.7201   0.01723   0.01294  -0.0362   1.0000   0.0193
  -8.000  -0.6969   0.01691   0.01256  -0.0353   1.0000   0.0199
  -7.750  -0.6741   0.01648   0.01205  -0.0343   1.0000   0.0206
  -7.500  -0.6509   0.01621   0.01170  -0.0333   1.0000   0.0212
  -7.250  -0.6272   0.01617   0.01162  -0.0324   1.0000   0.0216
  -7.000  -0.6074   0.01455   0.00978  -0.0312   1.0000   0.0227
  -6.750  -0.5846   0.01419   0.00941  -0.0302   1.0000   0.0234
  -6.500  -0.5617   0.01391   0.00909  -0.0292   1.0000   0.0241
  -6.250  -0.5387   0.01362   0.00876  -0.0282   1.0000   0.0248
  -6.000  -0.5078   0.01333   0.00842  -0.0289   0.9993   0.0257
  -5.750  -0.4740   0.01300   0.00802  -0.0302   0.9982   0.0265
  -5.500  -0.4407   0.01275   0.00770  -0.0313   0.9971   0.0270
  -5.250  -0.4101   0.01156   0.00636  -0.0320   0.9963   0.0283
  -5.000  -0.3774   0.01106   0.00584  -0.0331   0.9954   0.0294
  -4.750  -0.3438   0.01070   0.00545  -0.0344   0.9946   0.0303
  -4.500  -0.3099   0.01033   0.00505  -0.0356   0.9933   0.0311
  -4.250  -0.2755   0.00999   0.00468  -0.0370   0.9910   0.0322
  -4.000  -0.2404   0.00964   0.00430  -0.0385   0.9889   0.0330
  -3.750  -0.2052   0.00933   0.00397  -0.0400   0.9871   0.0336
  -3.500  -0.1696   0.00900   0.00361  -0.0416   0.9856   0.0343
  -3.250  -0.1338   0.00851   0.00307  -0.0432   0.9843   0.0362
  -3.000  -0.1017   0.00821   0.00278  -0.0440   0.9805   0.0380
  -2.750  -0.0676   0.00794   0.00252  -0.0452   0.9766   0.0396
  -2.500  -0.0314   0.00770   0.00227  -0.0469   0.9737   0.0414
  -2.250   0.0002   0.00744   0.00202  -0.0476   0.9685   0.0453
  -2.000   0.0309   0.00718   0.00183  -0.0480   0.9611   0.0562
  -1.750   0.0625   0.00691   0.00168  -0.0487   0.9515   0.0818
  -1.500   0.0958   0.00672   0.00156  -0.0497   0.9394   0.1003
  -1.250   0.1277   0.00660   0.00146  -0.0504   0.9217   0.1146
  -1.000   0.1566   0.00656   0.00138  -0.0503   0.8987   0.1257
  -0.750   0.1837   0.00659   0.00133  -0.0499   0.8714   0.1340
  -0.500   0.2097   0.00664   0.00128  -0.0492   0.8270   0.1436
  -0.250   0.2329   0.00693   0.00123  -0.0479   0.7403   0.1508
   0.000   0.2583   0.00712   0.00125  -0.0473   0.6909   0.1606
   0.250   0.2848   0.00721   0.00125  -0.0469   0.6546   0.1734
   0.500   0.3113   0.00729   0.00125  -0.0465   0.6163   0.1895
   0.750   0.3375   0.00730   0.00130  -0.0462   0.5770   0.2491
   1.000   0.3638   0.00728   0.00135  -0.0459   0.5428   0.3217
   1.250   0.3898   0.00714   0.00141  -0.0456   0.5115   0.4360
   1.500   0.4008   0.00589   0.00153  -0.0417   0.4847   0.9574
   1.750   0.4305   0.00611   0.00161  -0.0418   0.4456   0.9799
   2.000   0.4672   0.00642   0.00171  -0.0438   0.3964   0.9898
   2.250   0.5111   0.00678   0.00187  -0.0475   0.3534   0.9953
   2.500   0.5578   0.00709   0.00202  -0.0518   0.3220   0.9990
   2.750   0.5894   0.00729   0.00211  -0.0527   0.2999   1.0000
   3.000   0.6142   0.00743   0.00218  -0.0520   0.2852   1.0000
   3.250   0.6389   0.00756   0.00225  -0.0512   0.2727   1.0000
   3.500   0.6636   0.00768   0.00233  -0.0505   0.2616   1.0000
   3.750   0.6883   0.00780   0.00242  -0.0498   0.2507   1.0000
   4.000   0.7128   0.00793   0.00251  -0.0490   0.2398   1.0000
   4.250   0.7372   0.00809   0.00262  -0.0482   0.2289   1.0000
   4.500   0.7618   0.00822   0.00273  -0.0475   0.2185   1.0000
   4.750   0.7862   0.00837   0.00285  -0.0467   0.2074   1.0000
   5.000   0.8105   0.00856   0.00298  -0.0459   0.1935   1.0000
   5.250   0.8348   0.00876   0.00313  -0.0452   0.1782   1.0000
   5.500   0.8588   0.00902   0.00331  -0.0444   0.1596   1.0000
   5.750   0.8823   0.00936   0.00353  -0.0435   0.1349   1.0000
   6.000   0.9047   0.00988   0.00385  -0.0426   0.0999   1.0000
   6.250   0.9278   0.01036   0.00420  -0.0417   0.0762   1.0000
   6.500   0.9520   0.01074   0.00451  -0.0410   0.0646   1.0000
   6.750   0.9769   0.01102   0.00479  -0.0405   0.0592   1.0000
   7.000   1.0015   0.01139   0.00513  -0.0399   0.0527   1.0000
   7.250   1.0269   0.01164   0.00541  -0.0394   0.0496   1.0000
   7.500   1.0515   0.01200   0.00575  -0.0389   0.0453   1.0000
   7.750   1.0765   0.01232   0.00609  -0.0384   0.0420   1.0000
   8.000   1.1017   0.01259   0.00638  -0.0380   0.0391   1.0000
   8.250   1.1257   0.01305   0.00681  -0.0373   0.0346   1.0000
   8.500   1.1510   0.01330   0.00710  -0.0369   0.0324   1.0000
   8.750   1.1750   0.01372   0.00750  -0.0364   0.0285   1.0000
   9.000   1.1993   0.01410   0.00790  -0.0358   0.0254   1.0000
   9.250   1.2220   0.01467   0.00845  -0.0350   0.0215   1.0000
   9.500   1.2462   0.01504   0.00886  -0.0345   0.0197   1.0000
   9.750   1.2686   0.01562   0.00944  -0.0337   0.0175   1.0000
  10.000   1.2910   0.01618   0.01006  -0.0329   0.0163   1.0000
  10.250   1.3136   0.01668   0.01061  -0.0321   0.0153   1.0000
  10.500   1.3351   0.01728   0.01125  -0.0312   0.0143   1.0000
  10.750   1.3531   0.01827   0.01233  -0.0297   0.0131   1.0000
  11.000   1.3749   0.01878   0.01290  -0.0289   0.0127   1.0000
  11.250   1.3958   0.01935   0.01354  -0.0279   0.0121   1.0000
  11.500   1.4158   0.01999   0.01424  -0.0268   0.0115   1.0000
  11.750   1.4343   0.02074   0.01506  -0.0256   0.0110   1.0000
  12.000   1.4491   0.02179   0.01620  -0.0238   0.0104   1.0000
  12.250   1.4593   0.02318   0.01772  -0.0214   0.0100   1.0000
  12.500   1.4760   0.02391   0.01854  -0.0199   0.0098   1.0000
  12.750   1.4907   0.02475   0.01948  -0.0181   0.0096   1.0000
  13.000   1.5029   0.02568   0.02051  -0.0161   0.0093   1.0000
  13.250   1.5119   0.02665   0.02159  -0.0135   0.0091   1.0000
  13.500   1.5176   0.02771   0.02273  -0.0105   0.0088   1.0000
  13.750   1.5224   0.02889   0.02401  -0.0076   0.0086   1.0000
  14.000   1.5260   0.03024   0.02546  -0.0050   0.0084   1.0000
  14.250   1.5278   0.03183   0.02715  -0.0025   0.0083   1.0000
  14.500   1.5268   0.03378   0.02921  -0.0004   0.0081   1.0000
  14.750   1.5220   0.03629   0.03184   0.0013   0.0080   1.0000
  15.000   1.5131   0.03956   0.03525   0.0023   0.0078   1.0000
  15.250   1.4986   0.04413   0.03999   0.0018   0.0077   1.0000
  15.500   1.4826   0.04976   0.04580  -0.0004   0.0076   1.0000
  15.750   1.4629   0.05664   0.05287  -0.0039   0.0076   1.0000
  16.000   1.4431   0.06393   0.06033  -0.0078   0.0075   1.0000
  16.250   1.4210   0.07173   0.06830  -0.0119   0.0075   1.0000
  16.500   1.3992   0.07953   0.07624  -0.0158   0.0075   1.0000
  16.750   1.3782   0.08720   0.08404  -0.0196   0.0075   1.0000
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