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GOE 546 AIRFOIL (goe546-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 546 AIRFOIL (goe546-il)
Reynolds number: 1,000,000
Max Cl/Cd: 101.67 at α=2.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe546-il-1000000-n5.txt
Download as CSV file: xf-goe546-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 546 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
  ------ -------- --------- --------- -------- -------- --------
 -14.500  -0.9838   0.04190   0.03940  -0.0847   1.0000   0.0069
 -14.250  -1.0306   0.03438   0.03164  -0.0899   1.0000   0.0068
 -14.000  -1.0441   0.03157   0.02867  -0.0880   1.0000   0.0069
 -13.750  -1.0449   0.02921   0.02615  -0.0868   0.9998   0.0070
 -13.500  -1.0249   0.02689   0.02365  -0.0890   0.9979   0.0072
 -13.250  -1.0020   0.02506   0.02166  -0.0908   0.9957   0.0074
 -13.000  -0.9781   0.02357   0.02003  -0.0921   0.9936   0.0077
 -12.750  -0.9545   0.02226   0.01859  -0.0929   0.9907   0.0079
 -12.500  -0.9288   0.02108   0.01727  -0.0940   0.9881   0.0082
 -12.250  -0.9015   0.02001   0.01607  -0.0951   0.9861   0.0084
 -12.000  -0.8776   0.01909   0.01503  -0.0953   0.9823   0.0087
 -11.750  -0.8517   0.01825   0.01407  -0.0958   0.9784   0.0089
 -11.250  -0.8003   0.01653   0.01217  -0.0965   0.9680   0.0098
 -10.750  -0.7398   0.01517   0.01064  -0.0986   0.9571   0.0109
 -10.500  -0.7053   0.01456   0.00994  -0.1006   0.9528   0.0114
 -10.250  -0.6708   0.01394   0.00925  -0.1025   0.9473   0.0123
 -10.000  -0.6358   0.01343   0.00869  -0.1044   0.9406   0.0131
  -9.750  -0.6013   0.01298   0.00815  -0.1061   0.9329   0.0141
  -9.500  -0.5691   0.01257   0.00764  -0.1073   0.9234   0.0148
  -9.250  -0.5403   0.01224   0.00725  -0.1078   0.9144   0.0157
  -9.000  -0.5120   0.01200   0.00696  -0.1080   0.9065   0.0166
  -8.750  -0.4854   0.01179   0.00670  -0.1078   0.8984   0.0176
  -8.500  -0.4587   0.01159   0.00640  -0.1077   0.8910   0.0185
  -8.250  -0.4329   0.01132   0.00607  -0.1073   0.8845   0.0191
  -8.000  -0.4067   0.01109   0.00581  -0.1071   0.8790   0.0200
  -7.750  -0.3800   0.01092   0.00560  -0.1069   0.8744   0.0207
  -7.500  -0.3533   0.01077   0.00542  -0.1067   0.8694   0.0216
  -7.250  -0.3268   0.01058   0.00518  -0.1064   0.8643   0.0224
  -7.000  -0.3001   0.01042   0.00495  -0.1062   0.8599   0.0231
  -6.750  -0.2733   0.01025   0.00475  -0.1060   0.8556   0.0235
  -6.500  -0.2474   0.00994   0.00438  -0.1056   0.8510   0.0242
  -6.250  -0.2213   0.00967   0.00407  -0.1053   0.8463   0.0251
  -6.000  -0.1946   0.00949   0.00387  -0.1051   0.8418   0.0259
  -5.750  -0.1678   0.00931   0.00367  -0.1049   0.8368   0.0267
  -5.500  -0.1411   0.00912   0.00344  -0.1046   0.8322   0.0274
  -5.250  -0.1142   0.00896   0.00323  -0.1044   0.8276   0.0281
  -5.000  -0.0873   0.00879   0.00303  -0.1041   0.8222   0.0287
  -4.750  -0.0606   0.00863   0.00282  -0.1038   0.8162   0.0292
  -4.500  -0.0338   0.00849   0.00264  -0.1036   0.8096   0.0295
  -4.250  -0.0077   0.00830   0.00238  -0.1032   0.8001   0.0303
  -4.000   0.0187   0.00811   0.00216  -0.1028   0.7902   0.0315
  -3.750   0.0452   0.00799   0.00199  -0.1024   0.7811   0.0324
  -3.500   0.0721   0.00787   0.00184  -0.1022   0.7722   0.0334
  -3.250   0.0989   0.00777   0.00171  -0.1019   0.7633   0.0344
  -3.000   0.1256   0.00769   0.00158  -0.1015   0.7530   0.0355
  -2.750   0.1524   0.00762   0.00147  -0.1012   0.7413   0.0366
  -2.500   0.1789   0.00755   0.00136  -0.1008   0.7282   0.0389
  -2.250   0.2051   0.00750   0.00127  -0.1004   0.7137   0.0428
  -2.000   0.2313   0.00746   0.00120  -0.1000   0.6984   0.0476
  -1.750   0.2573   0.00743   0.00114  -0.0995   0.6826   0.0564
  -1.500   0.2832   0.00740   0.00109  -0.0991   0.6676   0.0691
  -1.250   0.3091   0.00735   0.00105  -0.0986   0.6535   0.0894
  -1.000   0.3347   0.00723   0.00101  -0.0982   0.6405   0.1338
  -0.750   0.3598   0.00704   0.00098  -0.0977   0.6285   0.2059
  -0.500   0.3854   0.00692   0.00098  -0.0973   0.6166   0.2667
  -0.250   0.4117   0.00683   0.00099  -0.0970   0.6072   0.3099
   0.250   0.4630   0.00652   0.00107  -0.0962   0.5914   0.4614
   0.500   0.4887   0.00646   0.00112  -0.0957   0.5816   0.5159
   0.750   0.5145   0.00646   0.00117  -0.0953   0.5685   0.5495
   1.000   0.5399   0.00651   0.00121  -0.0947   0.5482   0.5742
   1.250   0.5644   0.00662   0.00127  -0.0940   0.5201   0.5993
   1.500   0.5877   0.00679   0.00135  -0.0931   0.4812   0.6275
   1.750   0.6113   0.00690   0.00145  -0.0922   0.4530   0.6671
   2.000   0.6347   0.00693   0.00156  -0.0913   0.4327   0.7223
   2.250   0.6560   0.00687   0.00168  -0.0898   0.4149   0.8139
   2.500   0.6776   0.00682   0.00181  -0.0883   0.3945   0.9077
   2.750   0.7310   0.00719   0.00203  -0.0943   0.3462   0.9991
   3.000   0.7524   0.00760   0.00222  -0.0931   0.2993   1.0000
   3.250   0.7729   0.00805   0.00244  -0.0918   0.2536   1.0000
   3.500   0.7945   0.00843   0.00265  -0.0906   0.2204   1.0000
   3.750   0.8170   0.00876   0.00285  -0.0896   0.1938   1.0000
   4.000   0.8392   0.00912   0.00306  -0.0885   0.1640   1.0000
   4.250   0.8559   0.00988   0.00347  -0.0866   0.0962   1.0000
   4.500   0.8782   0.01023   0.00373  -0.0856   0.0767   1.0000
   4.750   0.8984   0.01075   0.00406  -0.0842   0.0429   1.0000
   5.000   0.9217   0.01102   0.00429  -0.0834   0.0361   1.0000
   5.250   0.9457   0.01124   0.00451  -0.0826   0.0345   1.0000
   5.500   0.9694   0.01147   0.00474  -0.0819   0.0334   1.0000
   5.750   0.9929   0.01172   0.00499  -0.0811   0.0323   1.0000
   6.000   1.0159   0.01199   0.00525  -0.0802   0.0313   1.0000
   6.250   1.0388   0.01226   0.00553  -0.0793   0.0303   1.0000
   6.500   1.0614   0.01255   0.00584  -0.0784   0.0296   1.0000
   6.750   1.0834   0.01287   0.00618  -0.0774   0.0288   1.0000
   7.000   1.1048   0.01321   0.00655  -0.0762   0.0280   1.0000
   7.250   1.1268   0.01350   0.00685  -0.0752   0.0278   1.0000
   7.500   1.1484   0.01379   0.00718  -0.0742   0.0276   1.0000
   7.750   1.1698   0.01410   0.00751  -0.0731   0.0273   1.0000
   8.000   1.1908   0.01439   0.00783  -0.0720   0.0268   1.0000
   8.250   1.2111   0.01472   0.00817  -0.0707   0.0262   1.0000
   8.500   1.2299   0.01503   0.00853  -0.0691   0.0254   1.0000
   8.750   1.2479   0.01537   0.00889  -0.0674   0.0248   1.0000
   9.000   1.2651   0.01575   0.00929  -0.0656   0.0242   1.0000
   9.250   1.2822   0.01613   0.00969  -0.0639   0.0234   1.0000
   9.500   1.2978   0.01661   0.01019  -0.0619   0.0227   1.0000
   9.750   1.3111   0.01721   0.01084  -0.0596   0.0218   1.0000
  10.000   1.3292   0.01756   0.01122  -0.0581   0.0215   1.0000
  10.250   1.3468   0.01792   0.01162  -0.0566   0.0210   1.0000
  10.500   1.3637   0.01834   0.01208  -0.0551   0.0205   1.0000
  10.750   1.3801   0.01879   0.01256  -0.0535   0.0198   1.0000
  11.000   1.3964   0.01926   0.01306  -0.0519   0.0190   1.0000
  11.250   1.4121   0.01975   0.01357  -0.0504   0.0181   1.0000
  11.500   1.4270   0.02032   0.01414  -0.0487   0.0171   1.0000
  11.750   1.4412   0.02093   0.01479  -0.0471   0.0164   1.0000
  12.000   1.4550   0.02158   0.01550  -0.0454   0.0156   1.0000
  12.250   1.4686   0.02226   0.01620  -0.0439   0.0146   1.0000
  12.500   1.4815   0.02301   0.01697  -0.0423   0.0137   1.0000
  12.750   1.4932   0.02386   0.01785  -0.0406   0.0128   1.0000
  13.000   1.5042   0.02478   0.01882  -0.0390   0.0120   1.0000
  13.250   1.5145   0.02578   0.01986  -0.0374   0.0112   1.0000
  13.500   1.5234   0.02691   0.02102  -0.0358   0.0102   1.0000
  13.750   1.5321   0.02809   0.02226  -0.0342   0.0098   1.0000
  14.000   1.5402   0.02935   0.02359  -0.0327   0.0092   1.0000
  14.250   1.5477   0.03071   0.02502  -0.0313   0.0089   1.0000
  14.500   1.5538   0.03222   0.02659  -0.0299   0.0084   1.0000
  14.750   1.5588   0.03387   0.02831  -0.0286   0.0080   1.0000
  15.000   1.5632   0.03564   0.03015  -0.0274   0.0077   1.0000
  15.250   1.5672   0.03751   0.03210  -0.0264   0.0075   1.0000
  15.500   1.5711   0.03945   0.03413  -0.0255   0.0072   1.0000
  15.750   1.5745   0.04153   0.03629  -0.0247   0.0070   1.0000
  16.000   1.5763   0.04384   0.03870  -0.0241   0.0069   1.0000
  16.250   1.5774   0.04632   0.04126  -0.0236   0.0066   1.0000
  16.500   1.5774   0.04902   0.04404  -0.0234   0.0064   1.0000
  16.750   1.5768   0.05189   0.04701  -0.0233   0.0062   1.0000
  17.000   1.5747   0.05502   0.05023  -0.0234   0.0060   1.0000
  17.250   1.5707   0.05850   0.05381  -0.0237   0.0059   1.0000
  17.500   1.5659   0.06221   0.05762  -0.0242   0.0058   1.0000
  17.750   1.5604   0.06613   0.06165  -0.0249   0.0056   1.0000
  18.000   1.5554   0.07007   0.06570  -0.0259   0.0055   1.0000
  18.250   1.5505   0.07412   0.06985  -0.0270   0.0054   1.0000
  18.500   1.5421   0.07884   0.07469  -0.0284   0.0054   1.0000
  18.750   1.5343   0.08360   0.07957  -0.0301   0.0053   1.0000
  19.000   1.5252   0.08866   0.08475  -0.0320   0.0052   1.0000
  19.250   1.5141   0.09422   0.09043  -0.0343   0.0051   1.0000
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