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DF102 (df102-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: DF102 (df102-il)
Reynolds number: 500,000
Max Cl/Cd: 75.39 at α=8°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-df102-il-500000-n5.txt
Download as CSV file: xf-df102-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: DF102                                           
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.750  -0.7242   0.08319   0.08039  -0.0377   1.0000   0.0066
 -13.500  -0.7584   0.07308   0.07019  -0.0436   1.0000   0.0065
 -13.250  -0.7916   0.06331   0.06030  -0.0498   1.0000   0.0064
 -13.000  -0.8169   0.05467   0.05151  -0.0559   1.0000   0.0063
 -12.750  -0.8393   0.04601   0.04266  -0.0633   1.0000   0.0063
 -12.500  -0.8558   0.03957   0.03601  -0.0692   1.0000   0.0063
 -12.250  -0.8726   0.03551   0.03175  -0.0707   1.0000   0.0064
 -12.000  -0.8837   0.03319   0.02927  -0.0688   1.0000   0.0064
 -11.750  -0.8936   0.03132   0.02725  -0.0653   1.0000   0.0064
 -11.500  -0.8941   0.02962   0.02538  -0.0627   1.0000   0.0065
 -11.250  -0.8930   0.02801   0.02359  -0.0598   1.0000   0.0066
 -11.000  -0.8888   0.02668   0.02211  -0.0570   1.0000   0.0067
 -10.750  -0.8845   0.02552   0.02080  -0.0539   1.0000   0.0068
 -10.500  -0.8629   0.02380   0.01888  -0.0545   0.9963   0.0070
 -10.250  -0.8381   0.02240   0.01733  -0.0554   0.9921   0.0072
 -10.000  -0.8112   0.02143   0.01626  -0.0562   0.9880   0.0075
  -9.750  -0.7822   0.02055   0.01527  -0.0572   0.9848   0.0078
  -9.500  -0.7526   0.01963   0.01424  -0.0583   0.9821   0.0081
  -9.250  -0.7257   0.01880   0.01330  -0.0588   0.9774   0.0084
  -9.000  -0.6966   0.01807   0.01245  -0.0595   0.9736   0.0089
  -8.750  -0.6661   0.01731   0.01157  -0.0605   0.9705   0.0094
  -8.500  -0.6397   0.01652   0.01070  -0.0607   0.9652   0.0100
  -8.250  -0.6114   0.01596   0.01008  -0.0612   0.9602   0.0105
  -8.000  -0.5820   0.01536   0.00941  -0.0618   0.9561   0.0111
  -7.750  -0.5564   0.01486   0.00883  -0.0615   0.9496   0.0118
  -7.500  -0.5296   0.01434   0.00823  -0.0614   0.9438   0.0125
  -7.250  -0.5037   0.01384   0.00764  -0.0611   0.9380   0.0132
  -7.000  -0.4789   0.01336   0.00712  -0.0606   0.9312   0.0143
  -6.750  -0.4525   0.01298   0.00669  -0.0603   0.9257   0.0153
  -6.500  -0.4273   0.01267   0.00631  -0.0597   0.9186   0.0166
  -6.250  -0.4020   0.01223   0.00581  -0.0592   0.9123   0.0178
  -6.000  -0.3769   0.01185   0.00538  -0.0587   0.9055   0.0192
  -5.750  -0.3510   0.01154   0.00502  -0.0582   0.8987   0.0206
  -5.500  -0.3249   0.01128   0.00470  -0.0577   0.8921   0.0221
  -5.250  -0.2993   0.01093   0.00430  -0.0572   0.8847   0.0246
  -5.000  -0.2731   0.01067   0.00400  -0.0568   0.8779   0.0272
  -4.750  -0.2470   0.01038   0.00369  -0.0563   0.8700   0.0313
  -4.500  -0.2208   0.01010   0.00340  -0.0558   0.8627   0.0388
  -4.250  -0.1954   0.00972   0.00310  -0.0553   0.8543   0.0614
  -4.000  -0.1702   0.00929   0.00283  -0.0548   0.8462   0.1031
  -3.750  -0.1443   0.00901   0.00263  -0.0544   0.8375   0.1352
  -3.500  -0.1178   0.00880   0.00248  -0.0541   0.8286   0.1595
  -3.250  -0.0911   0.00864   0.00234  -0.0537   0.8195   0.1804
  -3.000  -0.0645   0.00847   0.00222  -0.0534   0.8096   0.2057
  -2.750  -0.0379   0.00831   0.00212  -0.0530   0.7997   0.2321
  -2.500  -0.0111   0.00820   0.00203  -0.0527   0.7897   0.2550
  -2.250   0.0158   0.00809   0.00194  -0.0524   0.7786   0.2731
  -2.000   0.0427   0.00801   0.00185  -0.0520   0.7672   0.2894
  -1.750   0.0693   0.00795   0.00177  -0.0516   0.7515   0.3047
  -1.500   0.0955   0.00791   0.00169  -0.0511   0.7326   0.3208
  -1.250   0.1217   0.00788   0.00162  -0.0506   0.7127   0.3396
  -0.750   0.1737   0.00781   0.00152  -0.0496   0.6738   0.3856
  -0.500   0.1996   0.00777   0.00149  -0.0491   0.6558   0.4138
   0.000   0.2505   0.00765   0.00148  -0.0480   0.6173   0.4964
   0.250   0.2753   0.00758   0.00149  -0.0473   0.5979   0.5467
   0.500   0.3000   0.00750   0.00151  -0.0466   0.5784   0.6028
   0.750   0.3243   0.00743   0.00155  -0.0458   0.5584   0.6563
   1.000   0.3478   0.00734   0.00159  -0.0448   0.5393   0.7180
   1.250   0.3701   0.00722   0.00167  -0.0434   0.5183   0.7939
   1.500   0.3936   0.00722   0.00180  -0.0420   0.4917   0.8784
   1.750   0.4239   0.00740   0.00193  -0.0423   0.4591   0.9251
   2.000   0.4570   0.00771   0.00205  -0.0435   0.4157   0.9483
   2.250   0.4892   0.00813   0.00221  -0.0446   0.3584   0.9633
   2.500   0.5210   0.00862   0.00240  -0.0457   0.2975   0.9738
   2.750   0.5523   0.00905   0.00260  -0.0466   0.2544   0.9825
   3.000   0.5875   0.00935   0.00277  -0.0484   0.2298   0.9881
   3.250   0.6206   0.00960   0.00294  -0.0496   0.2144   0.9940
   3.500   0.6559   0.00983   0.00309  -0.0514   0.2017   0.9992
   3.750   0.6811   0.01003   0.00324  -0.0509   0.1924   1.0000
   4.000   0.7034   0.01024   0.00341  -0.0498   0.1832   1.0000
   4.250   0.7259   0.01044   0.00357  -0.0488   0.1754   1.0000
   4.750   0.7710   0.01085   0.00392  -0.0467   0.1613   1.0000
   5.000   0.7936   0.01107   0.00411  -0.0457   0.1552   1.0000
   5.250   0.8163   0.01128   0.00431  -0.0447   0.1502   1.0000
   5.500   0.8391   0.01149   0.00451  -0.0437   0.1450   1.0000
   5.750   0.8615   0.01174   0.00474  -0.0427   0.1399   1.0000
   6.000   0.8846   0.01196   0.00496  -0.0418   0.1358   1.0000
   6.250   0.9074   0.01220   0.00520  -0.0409   0.1308   1.0000
   6.500   0.9298   0.01248   0.00545  -0.0399   0.1257   1.0000
   6.750   0.9528   0.01272   0.00572  -0.0390   0.1224   1.0000
   7.000   0.9757   0.01297   0.00599  -0.0381   0.1189   1.0000
   7.250   0.9982   0.01326   0.00628  -0.0372   0.1152   1.0000
   7.500   1.0201   0.01359   0.00660  -0.0362   0.1115   1.0000
   7.750   1.0428   0.01385   0.00691  -0.0353   0.1093   1.0000
   8.000   1.0652   0.01413   0.00723  -0.0344   0.1064   1.0000
   8.250   1.0871   0.01445   0.00756  -0.0334   0.1034   1.0000
   8.500   1.1082   0.01481   0.00793  -0.0324   0.1002   1.0000
   8.750   1.1289   0.01519   0.00834  -0.0312   0.0979   1.0000
   9.000   1.1505   0.01550   0.00872  -0.0302   0.0963   1.0000
   9.250   1.1716   0.01582   0.00910  -0.0292   0.0939   1.0000
   9.500   1.1920   0.01618   0.00948  -0.0280   0.0909   1.0000
   9.750   1.2112   0.01660   0.00990  -0.0267   0.0874   1.0000
  10.000   1.2303   0.01700   0.01036  -0.0254   0.0848   1.0000
  10.250   1.2498   0.01732   0.01073  -0.0241   0.0816   1.0000
  10.500   1.2669   0.01772   0.01113  -0.0225   0.0770   1.0000
  10.750   1.2830   0.01817   0.01160  -0.0208   0.0728   1.0000
  11.000   1.3000   0.01858   0.01204  -0.0192   0.0678   1.0000
  11.250   1.3149   0.01913   0.01258  -0.0174   0.0630   1.0000
  11.500   1.3307   0.01963   0.01314  -0.0158   0.0589   1.0000
  11.750   1.3446   0.02027   0.01378  -0.0140   0.0532   1.0000
  12.000   1.3565   0.02105   0.01453  -0.0121   0.0444   1.0000
  12.250   1.3654   0.02206   0.01550  -0.0100   0.0349   1.0000
  12.500   1.3697   0.02342   0.01680  -0.0075   0.0237   1.0000
  12.750   1.3739   0.02483   0.01821  -0.0051   0.0173   1.0000
  13.000   1.3806   0.02608   0.01952  -0.0032   0.0141   1.0000
  13.250   1.3869   0.02741   0.02091  -0.0014   0.0120   1.0000
  13.500   1.3923   0.02885   0.02243   0.0003   0.0103   1.0000
  13.750   1.3980   0.03031   0.02398   0.0018   0.0093   1.0000
  14.000   1.4033   0.03185   0.02562   0.0031   0.0085   1.0000
  14.250   1.4069   0.03361   0.02748   0.0044   0.0078   1.0000
  14.500   1.4072   0.03574   0.02971   0.0055   0.0070   1.0000
  14.750   1.4101   0.03773   0.03181   0.0062   0.0067   1.0000
  15.000   1.4110   0.04001   0.03421   0.0068   0.0063   1.0000
  15.250   1.4098   0.04263   0.03695   0.0072   0.0059   1.0000
  15.500   1.4072   0.04551   0.03995   0.0072   0.0057   1.0000
  15.750   1.4006   0.04902   0.04359   0.0069   0.0054   1.0000
  16.000   1.3927   0.05292   0.04762   0.0061   0.0052   1.0000
  16.250   1.3834   0.05723   0.05206   0.0049   0.0050   1.0000
  16.500   1.3730   0.06195   0.05694   0.0033   0.0048   1.0000
  16.750   1.3589   0.06750   0.06266   0.0010   0.0048   1.0000
  17.000   1.3410   0.07402   0.06934  -0.0020   0.0048   1.0000
  17.250   1.3210   0.08127   0.07677  -0.0056   0.0047   1.0000
  17.500   1.2919   0.09061   0.08630  -0.0105   0.0049   1.0000
  17.750   1.2567   0.10165   0.09755  -0.0164   0.0050   1.0000
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