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SD7043 (9.1%) (sd7043-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: SD7043 (9.1%) (sd7043-il)
Reynolds number: 1,000,000
Max Cl/Cd: 126.66 at α=2.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-sd7043-il-1000000.txt
Download as CSV file: xf-sd7043-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: SD7043 (9.1%)                                   
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -10.000  -0.2763   0.09187   0.09032  -0.0370   1.0000   0.0118
  -9.750  -0.2756   0.08786   0.08633  -0.0379   1.0000   0.0118
  -9.500  -0.2809   0.08336   0.08185  -0.0383   1.0000   0.0121
  -9.250  -0.2773   0.08046   0.07898  -0.0387   0.9991   0.0122
  -9.000  -0.2691   0.07642   0.07494  -0.0412   0.9932   0.0123
  -8.750  -0.2611   0.07204   0.07055  -0.0441   0.9898   0.0125
  -8.500  -0.2497   0.06811   0.06662  -0.0472   0.9865   0.0129
  -8.250  -0.2417   0.06307   0.06159  -0.0512   0.9823   0.0131
  -8.000  -0.3908   0.02936   0.02701  -0.0971   0.9563   0.0091
  -7.750  -0.3837   0.02384   0.02088  -0.0982   0.9442   0.0090
  -7.500  -0.3728   0.01810   0.01438  -0.0987   0.9346   0.0092
  -7.250  -0.3501   0.01667   0.01272  -0.0985   0.9288   0.0094
  -7.000  -0.3246   0.01605   0.01200  -0.0984   0.9232   0.0098
  -6.750  -0.2992   0.01524   0.01105  -0.0982   0.9176   0.0101
  -6.500  -0.2737   0.01442   0.01006  -0.0979   0.9126   0.0106
  -6.250  -0.2473   0.01352   0.00900  -0.0978   0.9072   0.0110
  -6.000  -0.2208   0.01275   0.00807  -0.0976   0.9019   0.0114
  -5.750  -0.1939   0.01229   0.00746  -0.0973   0.8971   0.0117
  -5.500  -0.1677   0.01098   0.00602  -0.0973   0.8917   0.0124
  -5.250  -0.1404   0.01060   0.00560  -0.0972   0.8864   0.0131
  -5.000  -0.1129   0.01032   0.00526  -0.0970   0.8814   0.0139
  -4.750  -0.0849   0.01008   0.00497  -0.0970   0.8758   0.0148
  -4.500  -0.0577   0.00944   0.00424  -0.0968   0.8703   0.0159
  -4.250  -0.0300   0.00906   0.00383  -0.0968   0.8649   0.0169
  -4.000  -0.0019   0.00878   0.00352  -0.0967   0.8590   0.0182
  -3.750   0.0260   0.00858   0.00325  -0.0966   0.8533   0.0192
  -3.500   0.0541   0.00810   0.00273  -0.0966   0.8473   0.0211
  -3.250   0.0822   0.00789   0.00249  -0.0966   0.8409   0.0229
  -3.000   0.1105   0.00771   0.00226  -0.0965   0.8346   0.0244
  -2.750   0.1388   0.00743   0.00193  -0.0965   0.8276   0.0268
  -2.500   0.1670   0.00726   0.00173  -0.0964   0.8210   0.0298
  -2.250   0.1955   0.00708   0.00153  -0.0964   0.8133   0.0346
  -2.000   0.2237   0.00679   0.00136  -0.0964   0.8059   0.0701
  -1.750   0.2520   0.00649   0.00125  -0.0965   0.7972   0.1321
  -1.500   0.2801   0.00625   0.00116  -0.0965   0.7886   0.1935
  -1.250   0.3082   0.00601   0.00109  -0.0966   0.7791   0.2626
  -1.000   0.3363   0.00576   0.00106  -0.0967   0.7692   0.3463
  -0.750   0.3643   0.00557   0.00103  -0.0967   0.7588   0.4231
  -0.500   0.3921   0.00541   0.00102  -0.0967   0.7472   0.4980
  -0.250   0.4199   0.00525   0.00103  -0.0967   0.7342   0.5733
   0.000   0.4474   0.00511   0.00106  -0.0965   0.7203   0.6541
   0.250   0.4746   0.00502   0.00109  -0.0962   0.7051   0.7180
   0.500   0.5012   0.00496   0.00113  -0.0958   0.6890   0.7793
   0.750   0.5273   0.00493   0.00117  -0.0952   0.6722   0.8299
   1.000   0.5518   0.00488   0.00120  -0.0942   0.6542   0.8854
   1.250   0.5799   0.00479   0.00118  -0.0940   0.6346   1.0000
   1.750   0.6351   0.00509   0.00127  -0.0937   0.5915   1.0000
   2.250   0.6898   0.00546   0.00141  -0.0935   0.5437   1.0000
   2.500   0.7169   0.00566   0.00150  -0.0933   0.5182   1.0000
   2.750   0.7437   0.00589   0.00160  -0.0931   0.4914   1.0000
   3.000   0.7705   0.00613   0.00171  -0.0929   0.4631   1.0000
   3.250   0.7971   0.00639   0.00184  -0.0927   0.4342   1.0000
   3.500   0.8235   0.00666   0.00198  -0.0925   0.4048   1.0000
   3.750   0.8500   0.00693   0.00213  -0.0922   0.3774   1.0000
   4.000   0.8761   0.00724   0.00230  -0.0920   0.3478   1.0000
   4.250   0.9022   0.00753   0.00248  -0.0917   0.3211   1.0000
   4.500   0.9281   0.00786   0.00267  -0.0914   0.2941   1.0000
   4.750   0.9538   0.00819   0.00288  -0.0911   0.2692   1.0000
   5.000   0.9796   0.00850   0.00309  -0.0908   0.2451   1.0000
   5.250   1.0052   0.00884   0.00332  -0.0905   0.2231   1.0000
   5.500   1.0308   0.00916   0.00354  -0.0902   0.2029   1.0000
   5.750   1.0563   0.00948   0.00379  -0.0899   0.1857   1.0000
   6.000   1.0817   0.00981   0.00404  -0.0895   0.1700   1.0000
   6.500   1.1321   0.01048   0.00457  -0.0888   0.1410   1.0000
   6.750   1.1573   0.01080   0.00485  -0.0884   0.1293   1.0000
   7.000   1.1822   0.01114   0.00515  -0.0880   0.1182   1.0000
   7.250   1.2069   0.01149   0.00546  -0.0876   0.1073   1.0000
   7.500   1.2313   0.01187   0.00579  -0.0871   0.0975   1.0000
   7.750   1.2554   0.01226   0.00613  -0.0866   0.0884   1.0000
   8.000   1.2796   0.01261   0.00647  -0.0861   0.0808   1.0000
   8.250   1.3032   0.01303   0.00686  -0.0855   0.0731   1.0000
   8.500   1.3268   0.01343   0.00725  -0.0849   0.0668   1.0000
   8.750   1.3500   0.01384   0.00765  -0.0843   0.0608   1.0000
   9.000   1.3727   0.01430   0.00808  -0.0836   0.0554   1.0000
   9.250   1.3952   0.01475   0.00855  -0.0828   0.0509   1.0000
   9.500   1.4177   0.01517   0.00899  -0.0821   0.0475   1.0000
   9.750   1.4382   0.01578   0.00957  -0.0811   0.0428   1.0000
  10.000   1.4604   0.01618   0.01002  -0.0803   0.0411   1.0000
  10.250   1.4818   0.01662   0.01050  -0.0794   0.0389   1.0000
  10.500   1.5014   0.01721   0.01108  -0.0783   0.0361   1.0000
  10.750   1.5196   0.01787   0.01180  -0.0770   0.0336   1.0000
  11.000   1.5400   0.01830   0.01228  -0.0760   0.0325   1.0000
  11.250   1.5590   0.01880   0.01282  -0.0748   0.0308   1.0000
  11.500   1.5752   0.01943   0.01344  -0.0732   0.0285   1.0000
  11.750   1.5874   0.02016   0.01422  -0.0709   0.0265   1.0000
  12.000   1.6037   0.02060   0.01472  -0.0693   0.0255   1.0000
  12.250   1.6177   0.02118   0.01535  -0.0674   0.0242   1.0000
  12.500   1.6296   0.02192   0.01611  -0.0654   0.0230   1.0000
  12.750   1.6380   0.02291   0.01714  -0.0630   0.0212   1.0000
  13.000   1.6502   0.02369   0.01799  -0.0612   0.0205   1.0000
  13.250   1.6626   0.02446   0.01884  -0.0595   0.0197   1.0000
  13.500   1.6740   0.02535   0.01978  -0.0578   0.0188   1.0000
  13.750   1.6833   0.02641   0.02088  -0.0560   0.0178   1.0000
  14.000   1.6892   0.02777   0.02230  -0.0541   0.0166   1.0000
  14.250   1.6964   0.02909   0.02370  -0.0524   0.0159   1.0000
  14.500   1.7061   0.03025   0.02494  -0.0510   0.0153   1.0000
  14.750   1.7138   0.03161   0.02638  -0.0496   0.0145   1.0000
  15.000   1.7194   0.03321   0.02804  -0.0483   0.0138   1.0000
  15.250   1.7220   0.03516   0.03006  -0.0470   0.0130   1.0000
  15.500   1.7229   0.03736   0.03235  -0.0458   0.0123   1.0000
  15.750   1.7284   0.03919   0.03427  -0.0449   0.0118   1.0000
  16.000   1.7314   0.04135   0.03653  -0.0442   0.0112   1.0000
  16.250   1.7322   0.04385   0.03910  -0.0437   0.0104   1.0000
  16.500   1.7289   0.04694   0.04228  -0.0434   0.0099   1.0000
  16.750   1.7237   0.05041   0.04586  -0.0434   0.0092   1.0000
  17.000   1.7230   0.05349   0.04905  -0.0436   0.0088   1.0000
  17.250   1.7180   0.05730   0.05297  -0.0443   0.0083   1.0000
  17.500   1.7111   0.06156   0.05733  -0.0453   0.0078   1.0000
  17.750   1.6998   0.06670   0.06259  -0.0468   0.0074   1.0000
  18.000   1.6846   0.07276   0.06878  -0.0491   0.0070   1.0000
  18.250   1.6697   0.07906   0.07523  -0.0517   0.0068   1.0000
  18.500   1.6559   0.08546   0.08178  -0.0546   0.0066   1.0000
  18.750   1.6386   0.09271   0.08918  -0.0581   0.0065   1.0000
  19.000   1.6177   0.10087   0.09750  -0.0623   0.0064   1.0000
  19.250   1.5946   0.10976   0.10655  -0.0671   0.0063   1.0000
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