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FX 79-L-100 (fx79l100-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: FX 79-L-100 (fx79l100-il)
Reynolds number: 1,000,000
Max Cl/Cd: 72.67 at α=7.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx79l100-il-1000000-n5.txt
Download as CSV file: xf-fx79l100-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 79-L-100                                     
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -17.500  -1.0284   0.14035   0.13835   0.0352   1.0000   0.0055
 -17.250  -1.0925   0.12165   0.11950   0.0252   1.0000   0.0053
 -17.000  -1.1883   0.09708   0.09468   0.0119   1.0000   0.0053
 -16.750  -1.2433   0.08155   0.07892   0.0030   1.0000   0.0052
 -16.500  -1.2644   0.07339   0.07063  -0.0019   1.0000   0.0052
 -16.250  -1.2994   0.06339   0.06042  -0.0079   1.0000   0.0052
 -16.000  -1.3320   0.05463   0.05145  -0.0131   1.0000   0.0051
 -15.750  -1.3386   0.05026   0.04695  -0.0153   1.0000   0.0051
 -15.500  -1.3436   0.04629   0.04286  -0.0172   1.0000   0.0052
 -15.250  -1.3506   0.04221   0.03864  -0.0191   1.0000   0.0052
 -15.000  -1.3551   0.03868   0.03496  -0.0203   1.0000   0.0052
 -14.750  -1.3541   0.03600   0.03215  -0.0210   1.0000   0.0053
 -14.500  -1.3463   0.03421   0.03028  -0.0212   1.0000   0.0054
 -14.250  -1.3448   0.03193   0.02786  -0.0211   1.0000   0.0054
 -14.000  -1.3417   0.03006   0.02587  -0.0204   1.0000   0.0054
 -13.750  -1.3405   0.02822   0.02390  -0.0189   1.0000   0.0055
 -13.500  -1.3376   0.02667   0.02221  -0.0168   1.0000   0.0057
 -13.250  -1.3288   0.02543   0.02086  -0.0150   1.0000   0.0058
 -13.000  -1.3148   0.02433   0.01966  -0.0139   1.0000   0.0059
 -12.750  -1.2998   0.02329   0.01854  -0.0127   1.0000   0.0061
 -12.500  -1.2824   0.02244   0.01762  -0.0118   1.0000   0.0063
 -12.250  -1.2641   0.02163   0.01673  -0.0109   1.0000   0.0064
 -12.000  -1.2456   0.02080   0.01581  -0.0099   1.0000   0.0066
 -11.750  -1.2257   0.02009   0.01504  -0.0092   1.0000   0.0068
 -11.500  -1.2055   0.01940   0.01427  -0.0084   1.0000   0.0070
 -11.250  -1.1853   0.01865   0.01344  -0.0075   1.0000   0.0072
 -11.000  -1.1642   0.01801   0.01272  -0.0068   1.0000   0.0074
 -10.750  -1.1426   0.01740   0.01204  -0.0060   1.0000   0.0075
 -10.500  -1.1205   0.01684   0.01142  -0.0053   1.0000   0.0078
 -10.250  -1.0990   0.01619   0.01070  -0.0046   1.0000   0.0082
 -10.000  -1.0769   0.01560   0.01007  -0.0038   1.0000   0.0086
  -9.750  -1.0539   0.01512   0.00956  -0.0032   1.0000   0.0092
  -9.500  -1.0307   0.01467   0.00907  -0.0026   1.0000   0.0096
  -9.250  -1.0072   0.01424   0.00859  -0.0020   1.0000   0.0101
  -9.000  -0.9834   0.01385   0.00816  -0.0014   1.0000   0.0106
  -8.750  -0.9602   0.01339   0.00766  -0.0007   1.0000   0.0113
  -8.500  -0.9366   0.01296   0.00722   0.0000   1.0000   0.0122
  -8.250  -0.9127   0.01259   0.00682   0.0006   1.0000   0.0129
  -8.000  -0.8885   0.01226   0.00646   0.0012   1.0000   0.0138
  -7.750  -0.8642   0.01193   0.00610   0.0018   1.0000   0.0143
  -7.500  -0.8402   0.01157   0.00573   0.0025   1.0000   0.0153
  -7.250  -0.8162   0.01124   0.00539   0.0031   1.0000   0.0167
  -7.000  -0.7918   0.01095   0.00509   0.0037   1.0000   0.0177
  -6.750  -0.7673   0.01069   0.00481   0.0044   1.0000   0.0188
  -6.500  -0.7431   0.01037   0.00448   0.0051   0.9894   0.0206
  -6.250  -0.7048   0.01005   0.00418   0.0026   0.9707   0.0230
  -6.000  -0.6527   0.00975   0.00385  -0.0030   0.9509   0.0261
  -5.750  -0.5932   0.00941   0.00349  -0.0103   0.9209   0.0306
  -5.500  -0.5522   0.00928   0.00321  -0.0134   0.8732   0.0341
  -5.250  -0.5268   0.00918   0.00300  -0.0128   0.8353   0.0389
  -5.000  -0.5024   0.00910   0.00282  -0.0121   0.8086   0.0419
  -4.750  -0.4781   0.00895   0.00263  -0.0113   0.7873   0.0484
  -4.500  -0.4534   0.00883   0.00245  -0.0106   0.7689   0.0543
  -4.250  -0.4288   0.00868   0.00229  -0.0099   0.7518   0.0633
  -4.000  -0.4040   0.00853   0.00213  -0.0092   0.7359   0.0747
  -3.750  -0.3791   0.00837   0.00197  -0.0086   0.7218   0.0899
  -3.500  -0.3541   0.00819   0.00182  -0.0080   0.7095   0.1079
  -3.250  -0.3293   0.00799   0.00167  -0.0073   0.6983   0.1338
  -3.000  -0.3053   0.00770   0.00151  -0.0066   0.6880   0.1752
  -2.750  -0.2811   0.00740   0.00136  -0.0059   0.6784   0.2237
  -2.500  -0.2573   0.00708   0.00121  -0.0051   0.6694   0.2788
  -2.250  -0.2333   0.00678   0.00109  -0.0044   0.6605   0.3341
  -2.000  -0.2094   0.00648   0.00098  -0.0036   0.6524   0.3950
  -1.750  -0.1840   0.00634   0.00092  -0.0031   0.6442   0.4314
  -1.500  -0.1586   0.00618   0.00087  -0.0025   0.6367   0.4702
  -1.250  -0.1325   0.00610   0.00084  -0.0020   0.6287   0.4953
  -1.000  -0.1064   0.00601   0.00082  -0.0016   0.6212   0.5225
  -0.750  -0.0801   0.00596   0.00081  -0.0011   0.6135   0.5432
  -0.500  -0.0532   0.00593   0.00080  -0.0008   0.6059   0.5569
   0.000   0.0000   0.00590   0.00080   0.0000   0.5863   0.5860
   0.250   0.0269   0.00591   0.00080   0.0003   0.5751   0.5962
   0.500   0.0534   0.00592   0.00081   0.0007   0.5606   0.6056
   0.750   0.0800   0.00597   0.00081   0.0011   0.5423   0.6135
   1.000   0.1061   0.00602   0.00082   0.0016   0.5202   0.6215
   1.250   0.1325   0.00610   0.00084   0.0020   0.4953   0.6287
   1.500   0.1585   0.00618   0.00087   0.0025   0.4684   0.6366
   1.750   0.1839   0.00634   0.00092   0.0031   0.4295   0.6442
   2.000   0.2092   0.00649   0.00098   0.0036   0.3936   0.6527
   2.250   0.2334   0.00677   0.00108   0.0043   0.3367   0.6604
   2.500   0.2571   0.00710   0.00122   0.0051   0.2755   0.6693
   2.750   0.2810   0.00740   0.00136   0.0059   0.2224   0.6783
   3.000   0.3051   0.00771   0.00152   0.0066   0.1736   0.6881
   3.250   0.3297   0.00793   0.00166   0.0073   0.1413   0.6990
   3.500   0.3541   0.00817   0.00181   0.0079   0.1102   0.7101
   3.750   0.3790   0.00837   0.00197   0.0086   0.0894   0.7220
   4.000   0.4039   0.00854   0.00213   0.0092   0.0734   0.7356
   4.250   0.4287   0.00869   0.00229   0.0099   0.0632   0.7512
   4.500   0.4534   0.00883   0.00245   0.0106   0.0545   0.7681
   4.750   0.4781   0.00894   0.00262   0.0113   0.0488   0.7872
   5.000   0.5023   0.00909   0.00282   0.0121   0.0423   0.8093
   5.250   0.5267   0.00917   0.00301   0.0129   0.0391   0.8378
   5.500   0.5523   0.00927   0.00321   0.0133   0.0352   0.8738
   5.750   0.5911   0.00941   0.00348   0.0108   0.0307   0.9182
   6.000   0.6522   0.00975   0.00385   0.0031   0.0257   0.9507
   6.250   0.7045   0.01004   0.00417  -0.0025   0.0232   0.9702
   6.500   0.7430   0.01036   0.00448  -0.0051   0.0207   0.9894
   6.750   0.7673   0.01069   0.00480  -0.0044   0.0189   1.0000
   7.000   0.7918   0.01094   0.00508  -0.0038   0.0176   1.0000
   7.250   0.8161   0.01123   0.00538  -0.0031   0.0165   1.0000
   7.500   0.8401   0.01157   0.00571  -0.0025   0.0152   1.0000
   7.750   0.8642   0.01191   0.00609  -0.0018   0.0141   1.0000
   8.000   0.8885   0.01223   0.00643  -0.0012   0.0134   1.0000
   8.250   0.9127   0.01257   0.00680  -0.0006   0.0127   1.0000
   8.500   0.9364   0.01297   0.00721   0.0000   0.0118   1.0000
   8.750   0.9597   0.01343   0.00769   0.0007   0.0109   1.0000
   9.000   0.9833   0.01385   0.00817   0.0014   0.0104   1.0000
   9.250   1.0069   0.01426   0.00861   0.0020   0.0100   1.0000
   9.500   1.0304   0.01468   0.00908   0.0026   0.0094   1.0000
   9.750   1.0536   0.01514   0.00957   0.0032   0.0090   1.0000
  10.000   1.0763   0.01566   0.01013   0.0039   0.0085   1.0000
  10.250   1.0984   0.01624   0.01075   0.0046   0.0080   1.0000
  10.500   1.1198   0.01690   0.01148   0.0054   0.0078   1.0000
  10.750   1.1414   0.01754   0.01219   0.0062   0.0076   1.0000
  11.000   1.1633   0.01810   0.01281   0.0069   0.0075   1.0000
  11.250   1.1846   0.01871   0.01350   0.0076   0.0072   1.0000
  11.500   1.2049   0.01944   0.01431   0.0084   0.0070   1.0000
  11.750   1.2252   0.02012   0.01507   0.0092   0.0068   1.0000
  12.000   1.2446   0.02089   0.01592   0.0101   0.0067   1.0000
  12.250   1.2634   0.02168   0.01679   0.0110   0.0065   1.0000
  12.500   1.2810   0.02256   0.01775   0.0119   0.0064   1.0000
  12.750   1.2978   0.02346   0.01874   0.0129   0.0062   1.0000
  13.000   1.3130   0.02447   0.01984   0.0140   0.0061   1.0000
  13.250   1.3269   0.02558   0.02104   0.0152   0.0060   1.0000
  13.500   1.3372   0.02668   0.02222   0.0169   0.0058   1.0000
  13.750   1.3384   0.02838   0.02406   0.0191   0.0055   1.0000
  14.000   1.3411   0.03009   0.02590   0.0204   0.0055   1.0000
  14.250   1.3437   0.03204   0.02797   0.0210   0.0054   1.0000
  14.500   1.3456   0.03428   0.03035   0.0211   0.0054   1.0000
  14.750   1.3480   0.03668   0.03286   0.0207   0.0054   1.0000
  15.000   1.3463   0.03976   0.03608   0.0198   0.0053   1.0000
  15.250   1.3431   0.04320   0.03966   0.0184   0.0053   1.0000
  15.500   1.3348   0.04755   0.04415   0.0164   0.0053   1.0000
  15.750   1.3301   0.05155   0.04828   0.0144   0.0053   1.0000
  16.000   1.3098   0.05814   0.05505   0.0107   0.0053   1.0000
  16.250   1.2854   0.06588   0.06296   0.0061   0.0053   1.0000
  16.500   1.2565   0.07501   0.07227   0.0006   0.0053   1.0000
  16.750   1.2150   0.08739   0.08485  -0.0069   0.0053   1.0000
  17.000   1.1754   0.09998   0.09761  -0.0139   0.0053   1.0000
  17.250   1.0939   0.12155   0.11939  -0.0254   0.0055   1.0000
  17.500   1.0301   0.14029   0.13831  -0.0354   0.0058   1.0000
  18.000   0.8249   0.21770   0.21600  -0.0716   0.0041   1.0000
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