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DF102 (df102-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: DF102 (df102-il)
Reynolds number: 1,000,000
Max Cl/Cd: 93.45 at α=7.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-df102-il-1000000.txt
Download as CSV file: xf-df102-il-1000000.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 =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.750  -0.7848   0.07161   0.06938  -0.0446   1.0000   0.0072
 -13.500  -0.8107   0.06293   0.06057  -0.0503   1.0000   0.0072
 -13.250  -0.8403   0.05328   0.05077  -0.0576   1.0000   0.0072
 -13.000  -0.7982   0.05681   0.05440  -0.0544   1.0000   0.0069
 -12.750  -0.8459   0.04312   0.04038  -0.0669   1.0000   0.0070
 -12.500  -0.8799   0.03556   0.03253  -0.0728   1.0000   0.0071
 -12.250  -0.8635   0.03519   0.03217  -0.0724   1.0000   0.0070
 -12.000  -0.9128   0.03054   0.02719  -0.0674   1.0000   0.0072
 -11.750  -0.9184   0.02859   0.02508  -0.0642   1.0000   0.0072
 -11.500  -0.9198   0.02683   0.02317  -0.0611   1.0000   0.0073
 -11.250  -0.9155   0.02577   0.02204  -0.0581   1.0000   0.0075
 -11.000  -0.9149   0.02481   0.02100  -0.0542   1.0000   0.0076
 -10.750  -0.8993   0.02376   0.01985  -0.0531   0.9991   0.0077
 -10.500  -0.8698   0.02282   0.01882  -0.0545   0.9970   0.0079
 -10.250  -0.8413   0.02150   0.01735  -0.0559   0.9947   0.0081
 -10.000  -0.8136   0.02032   0.01603  -0.0569   0.9922   0.0083
  -9.750  -0.7850   0.01935   0.01495  -0.0578   0.9892   0.0086
  -9.500  -0.7555   0.01830   0.01377  -0.0589   0.9868   0.0089
  -9.250  -0.7244   0.01739   0.01275  -0.0601   0.9849   0.0091
  -9.000  -0.6920   0.01664   0.01190  -0.0615   0.9835   0.0094
  -8.750  -0.6657   0.01532   0.01043  -0.0619   0.9798   0.0097
  -8.500  -0.6382   0.01436   0.00939  -0.0624   0.9757   0.0102
  -8.250  -0.6073   0.01387   0.00888  -0.0633   0.9725   0.0107
  -8.000  -0.5770   0.01339   0.00835  -0.0640   0.9690   0.0112
  -7.750  -0.5516   0.01302   0.00793  -0.0635   0.9626   0.0119
  -7.500  -0.5236   0.01273   0.00758  -0.0635   0.9576   0.0124
  -7.250  -0.5019   0.01193   0.00669  -0.0625   0.9506   0.0132
  -7.000  -0.4776   0.01149   0.00622  -0.0617   0.9443   0.0139
  -6.750  -0.4523   0.01118   0.00587  -0.0612   0.9384   0.0148
  -6.500  -0.4273   0.01089   0.00552  -0.0605   0.9319   0.0157
  -6.250  -0.4018   0.01057   0.00514  -0.0599   0.9261   0.0165
  -6.000  -0.3780   0.01004   0.00456  -0.0591   0.9192   0.0180
  -5.750  -0.3521   0.00978   0.00426  -0.0585   0.9131   0.0195
  -5.500  -0.3257   0.00959   0.00403  -0.0581   0.9068   0.0207
  -5.250  -0.3006   0.00917   0.00356  -0.0574   0.9000   0.0232
  -5.000  -0.2742   0.00893   0.00328  -0.0570   0.8936   0.0252
  -4.750  -0.2478   0.00870   0.00302  -0.0566   0.8864   0.0277
  -4.500  -0.2215   0.00843   0.00273  -0.0561   0.8797   0.0332
  -4.250  -0.1963   0.00797   0.00241  -0.0555   0.8719   0.0624
  -4.000  -0.1719   0.00745   0.00213  -0.0549   0.8645   0.1239
  -3.750  -0.1457   0.00718   0.00199  -0.0545   0.8562   0.1586
  -3.500  -0.1189   0.00701   0.00186  -0.0542   0.8484   0.1824
  -3.250  -0.0919   0.00687   0.00175  -0.0539   0.8395   0.2032
  -3.000  -0.0647   0.00675   0.00166  -0.0536   0.8307   0.2214
  -2.750  -0.0377   0.00665   0.00157  -0.0533   0.8214   0.2394
  -2.500  -0.0106   0.00654   0.00149  -0.0530   0.8096   0.2591
  -2.000   0.0427   0.00636   0.00134  -0.0522   0.7801   0.3033
  -1.750   0.0695   0.00630   0.00128  -0.0519   0.7646   0.3243
  -1.500   0.0962   0.00624   0.00122  -0.0515   0.7490   0.3455
  -1.250   0.1228   0.00618   0.00117  -0.0511   0.7328   0.3696
  -1.000   0.1493   0.00611   0.00113  -0.0507   0.7172   0.3996
  -0.750   0.1754   0.00603   0.00111  -0.0503   0.7003   0.4375
  -0.500   0.2013   0.00592   0.00109  -0.0498   0.6835   0.4865
  -0.250   0.2269   0.00580   0.00108  -0.0493   0.6673   0.5448
   0.000   0.2523   0.00569   0.00109  -0.0487   0.6505   0.6036
   0.250   0.2773   0.00556   0.00111  -0.0480   0.6347   0.6661
   0.500   0.3016   0.00542   0.00113  -0.0471   0.6197   0.7326
   0.750   0.3243   0.00524   0.00118  -0.0458   0.6039   0.8166
   1.000   0.3472   0.00517   0.00128  -0.0443   0.5859   0.8976
   1.250   0.3745   0.00526   0.00136  -0.0439   0.5667   0.9348
   1.500   0.4039   0.00539   0.00142  -0.0440   0.5446   0.9558
   1.750   0.4359   0.00557   0.00150  -0.0448   0.5186   0.9691
   2.000   0.4727   0.00578   0.00158  -0.0467   0.4881   0.9764
   2.250   0.5058   0.00607   0.00168  -0.0479   0.4461   0.9832
   2.500   0.5429   0.00646   0.00181  -0.0501   0.3889   0.9867
   2.750   0.5765   0.00694   0.00199  -0.0516   0.3227   0.9911
   3.000   0.6103   0.00742   0.00218  -0.0531   0.2657   0.9950
   3.250   0.6466   0.00773   0.00234  -0.0551   0.2358   0.9979
   3.500   0.6819   0.00797   0.00247  -0.0569   0.2168   1.0000
   3.750   0.7038   0.00816   0.00260  -0.0557   0.2039   1.0000
   4.000   0.7256   0.00837   0.00274  -0.0545   0.1919   1.0000
   4.250   0.7482   0.00852   0.00287  -0.0534   0.1837   1.0000
   4.500   0.7704   0.00871   0.00301  -0.0523   0.1755   1.0000
   4.750   0.7929   0.00889   0.00316  -0.0512   0.1682   1.0000
   5.000   0.8153   0.00908   0.00332  -0.0501   0.1614   1.0000
   5.250   0.8382   0.00925   0.00347  -0.0491   0.1554   1.0000
   5.500   0.8604   0.00948   0.00366  -0.0480   0.1485   1.0000
   5.750   0.8839   0.00963   0.00382  -0.0471   0.1443   1.0000
   6.000   0.9065   0.00986   0.00401  -0.0461   0.1381   1.0000
   6.250   0.9294   0.01007   0.00421  -0.0451   0.1332   1.0000
   6.500   0.9527   0.01025   0.00440  -0.0442   0.1292   1.0000
   6.750   0.9753   0.01050   0.00462  -0.0432   0.1243   1.0000
   7.000   0.9981   0.01075   0.00487  -0.0423   0.1201   1.0000
   7.250   1.0217   0.01094   0.00508  -0.0415   0.1173   1.0000
   7.500   1.0448   0.01118   0.00531  -0.0406   0.1136   1.0000
   7.750   1.0666   0.01151   0.00562  -0.0395   0.1088   1.0000
   8.000   1.0899   0.01173   0.00588  -0.0387   0.1065   1.0000
   8.250   1.1133   0.01195   0.00613  -0.0379   0.1044   1.0000
   8.500   1.1361   0.01221   0.00640  -0.0371   0.1018   1.0000
   8.750   1.1581   0.01252   0.00670  -0.0361   0.0981   1.0000
   9.000   1.1793   0.01288   0.00706  -0.0350   0.0944   1.0000
   9.250   1.2032   0.01304   0.00726  -0.0344   0.0920   1.0000
   9.500   1.2257   0.01329   0.00751  -0.0336   0.0885   1.0000
   9.750   1.2464   0.01366   0.00787  -0.0325   0.0842   1.0000
  10.000   1.2681   0.01395   0.00819  -0.0315   0.0816   1.0000
  10.250   1.2903   0.01418   0.00846  -0.0306   0.0789   1.0000
  10.500   1.3109   0.01451   0.00878  -0.0295   0.0755   1.0000
  10.750   1.3295   0.01495   0.00921  -0.0282   0.0708   1.0000
  11.000   1.3506   0.01520   0.00952  -0.0271   0.0688   1.0000
  11.250   1.3685   0.01555   0.00988  -0.0256   0.0649   1.0000
  11.500   1.3835   0.01602   0.01032  -0.0236   0.0599   1.0000
  11.750   1.3994   0.01643   0.01075  -0.0217   0.0547   1.0000
  12.000   1.4117   0.01706   0.01133  -0.0195   0.0463   1.0000
  12.250   1.4178   0.01809   0.01224  -0.0165   0.0332   1.0000
  12.500   1.4184   0.01951   0.01356  -0.0130   0.0193   1.0000
  12.750   1.4243   0.02065   0.01471  -0.0103   0.0142   1.0000
  13.000   1.4313   0.02174   0.01584  -0.0079   0.0113   1.0000
  13.250   1.4370   0.02296   0.01711  -0.0055   0.0095   1.0000
  13.500   1.4464   0.02395   0.01817  -0.0037   0.0089   1.0000
  13.750   1.4540   0.02510   0.01939  -0.0019   0.0080   1.0000
  14.000   1.4582   0.02654   0.02090   0.0001   0.0073   1.0000
  14.250   1.4622   0.02805   0.02251   0.0019   0.0067   1.0000
  14.500   1.4684   0.02945   0.02400   0.0033   0.0064   1.0000
  14.750   1.4745   0.03091   0.02553   0.0046   0.0061   1.0000
  15.000   1.4767   0.03276   0.02748   0.0058   0.0058   1.0000
  15.250   1.4775   0.03484   0.02965   0.0068   0.0055   1.0000
  15.500   1.4747   0.03737   0.03229   0.0077   0.0053   1.0000
  15.750   1.4626   0.04103   0.03610   0.0082   0.0050   1.0000
  16.000   1.4644   0.04340   0.03857   0.0083   0.0048   1.0000
  16.250   1.4616   0.04639   0.04166   0.0081   0.0048   1.0000
  16.500   1.4530   0.05029   0.04569   0.0075   0.0048   1.0000
  16.750   1.4444   0.05441   0.04994   0.0065   0.0047   1.0000
  17.000   1.4320   0.05928   0.05494   0.0049   0.0046   1.0000
  17.250   1.4200   0.06439   0.06019   0.0030   0.0045   1.0000
  17.500   1.4032   0.07049   0.06643   0.0003   0.0045   1.0000
  17.750   1.3778   0.07842   0.07453  -0.0035   0.0045   1.0000
  18.000   1.3481   0.08756   0.08385  -0.0081   0.0046   1.0000
  18.250   1.3134   0.09818   0.09467  -0.0137   0.0046   1.0000
  18.500   1.2623   0.11236   0.10906  -0.0212   0.0049   1.0000
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