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DF102 (df102-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: DF102 (df102-il)
Reynolds number: 1,000,000
Max Cl/Cd: 93.02 at α=8°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-df102-il-1000000-n5.txt
Download as CSV file: xf-df102-il-1000000-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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.500  -0.8460   0.08867   0.08628  -0.0356   1.0000   0.0043
 -15.250  -0.8786   0.07936   0.07688  -0.0408   1.0000   0.0043
 -15.000  -0.9407   0.06557   0.06291  -0.0492   1.0000   0.0042
 -14.750  -0.9784   0.05554   0.05274  -0.0557   1.0000   0.0041
 -14.500  -1.0231   0.04263   0.03957  -0.0663   1.0000   0.0040
 -14.250  -1.0349   0.03643   0.03319  -0.0722   1.0000   0.0041
 -14.000  -1.0506   0.03215   0.02874  -0.0744   1.0000   0.0040
 -13.750  -1.0572   0.02995   0.02641  -0.0732   1.0000   0.0041
 -13.500  -1.0610   0.02844   0.02480  -0.0706   1.0000   0.0042
 -13.250  -1.0639   0.02710   0.02335  -0.0673   1.0000   0.0042
 -13.000  -1.0583   0.02586   0.02199  -0.0651   1.0000   0.0043
 -12.750  -1.0489   0.02483   0.02087  -0.0631   1.0000   0.0043
 -12.500  -1.0392   0.02381   0.01976  -0.0610   1.0000   0.0044
 -12.250  -1.0275   0.02295   0.01881  -0.0589   1.0000   0.0045
 -12.000  -1.0161   0.02214   0.01790  -0.0567   1.0000   0.0045
 -11.750  -0.9903   0.02111   0.01675  -0.0575   0.9968   0.0046
 -11.500  -0.9643   0.02024   0.01579  -0.0580   0.9924   0.0047
 -11.250  -0.9405   0.01895   0.01436  -0.0585   0.9878   0.0048
 -11.000  -0.9129   0.01795   0.01324  -0.0594   0.9847   0.0050
 -10.750  -0.8844   0.01714   0.01235  -0.0602   0.9814   0.0052
 -10.500  -0.8564   0.01651   0.01166  -0.0607   0.9768   0.0055
 -10.250  -0.8274   0.01582   0.01089  -0.0615   0.9725   0.0056
 -10.000  -0.7984   0.01527   0.01028  -0.0622   0.9680   0.0058
  -9.750  -0.7719   0.01475   0.00969  -0.0622   0.9615   0.0061
  -9.500  -0.7449   0.01423   0.00909  -0.0623   0.9558   0.0063
  -9.250  -0.7205   0.01377   0.00856  -0.0617   0.9486   0.0065
  -9.000  -0.6954   0.01337   0.00807  -0.0613   0.9420   0.0067
  -8.750  -0.6709   0.01296   0.00760  -0.0607   0.9353   0.0069
  -8.500  -0.6469   0.01249   0.00706  -0.0601   0.9284   0.0074
  -8.250  -0.6219   0.01215   0.00669  -0.0596   0.9222   0.0079
  -8.000  -0.5966   0.01184   0.00634  -0.0591   0.9156   0.0084
  -7.750  -0.5710   0.01156   0.00600  -0.0586   0.9097   0.0091
  -7.500  -0.5454   0.01127   0.00566  -0.0581   0.9031   0.0095
  -7.250  -0.5199   0.01095   0.00530  -0.0576   0.8968   0.0104
  -7.000  -0.4938   0.01069   0.00502  -0.0572   0.8905   0.0112
  -6.750  -0.4677   0.01045   0.00473  -0.0568   0.8837   0.0121
  -6.500  -0.4411   0.01024   0.00447  -0.0565   0.8774   0.0128
  -6.250  -0.4150   0.00997   0.00416  -0.0561   0.8701   0.0138
  -6.000  -0.3886   0.00974   0.00390  -0.0557   0.8634   0.0149
  -5.750  -0.3618   0.00955   0.00368  -0.0554   0.8556   0.0161
  -5.500  -0.3350   0.00939   0.00346  -0.0551   0.8482   0.0170
  -5.250  -0.3084   0.00915   0.00319  -0.0548   0.8399   0.0183
  -5.000  -0.2816   0.00896   0.00297  -0.0544   0.8318   0.0198
  -4.750  -0.2548   0.00879   0.00277  -0.0541   0.8228   0.0214
  -4.500  -0.2278   0.00862   0.00256  -0.0538   0.8138   0.0240
  -4.250  -0.2010   0.00845   0.00237  -0.0535   0.8046   0.0278
  -4.000  -0.1744   0.00824   0.00218  -0.0532   0.7942   0.0381
  -3.750  -0.1482   0.00796   0.00197  -0.0528   0.7841   0.0617
  -3.500  -0.1223   0.00767   0.00177  -0.0524   0.7736   0.0963
  -3.250  -0.0959   0.00746   0.00163  -0.0520   0.7625   0.1253
  -3.000  -0.0691   0.00731   0.00152  -0.0518   0.7508   0.1476
  -2.750  -0.0423   0.00717   0.00143  -0.0515   0.7393   0.1705
  -2.500  -0.0156   0.00710   0.00135  -0.0511   0.7229   0.1878
  -2.250   0.0104   0.00703   0.00128  -0.0507   0.7018   0.2143
  -2.000   0.0369   0.00699   0.00123  -0.0503   0.6804   0.2354
  -1.750   0.0635   0.00698   0.00118  -0.0499   0.6597   0.2497
  -1.500   0.0901   0.00698   0.00114  -0.0496   0.6397   0.2671
  -1.250   0.1170   0.00697   0.00111  -0.0493   0.6213   0.2811
  -1.000   0.1439   0.00699   0.00109  -0.0490   0.6021   0.2939
  -0.750   0.1706   0.00701   0.00107  -0.0487   0.5831   0.3089
  -0.500   0.1975   0.00702   0.00106  -0.0484   0.5650   0.3252
  -0.250   0.2240   0.00706   0.00107  -0.0481   0.5419   0.3437
   0.000   0.2504   0.00709   0.00108  -0.0477   0.5187   0.3649
   0.250   0.2770   0.00711   0.00109  -0.0474   0.4997   0.3889
   0.500   0.3030   0.00713   0.00112  -0.0470   0.4763   0.4203
   0.750   0.3285   0.00719   0.00116  -0.0466   0.4453   0.4547
   1.000   0.3536   0.00726   0.00122  -0.0461   0.4122   0.4971
   1.250   0.3779   0.00737   0.00131  -0.0454   0.3723   0.5454
   1.500   0.4015   0.00756   0.00143  -0.0447   0.3225   0.5901
   1.750   0.4245   0.00778   0.00157  -0.0438   0.2718   0.6379
   2.000   0.4482   0.00788   0.00170  -0.0430   0.2414   0.6912
   2.250   0.4717   0.00788   0.00181  -0.0421   0.2231   0.7544
   2.500   0.4935   0.00778   0.00193  -0.0407   0.2106   0.8392
   2.750   0.5170   0.00777   0.00208  -0.0395   0.2004   0.9092
   3.000   0.5454   0.00789   0.00220  -0.0395   0.1911   0.9416
   3.250   0.5782   0.00806   0.00233  -0.0405   0.1809   0.9596
   3.500   0.6109   0.00823   0.00246  -0.0416   0.1719   0.9703
   3.750   0.6455   0.00841   0.00259  -0.0431   0.1630   0.9774
   4.000   0.6780   0.00859   0.00273  -0.0442   0.1555   0.9835
   4.250   0.7127   0.00876   0.00286  -0.0457   0.1497   0.9875
   4.500   0.7475   0.00894   0.00302  -0.0473   0.1435   0.9941
   4.750   0.7896   0.00915   0.00319  -0.0505   0.1373   1.0000
   5.000   0.8126   0.00930   0.00333  -0.0495   0.1333   1.0000
   5.250   0.8352   0.00948   0.00348  -0.0485   0.1285   1.0000
   5.500   0.8581   0.00966   0.00364  -0.0475   0.1238   1.0000
   5.750   0.8813   0.00983   0.00381  -0.0466   0.1199   1.0000
   6.000   0.9044   0.01003   0.00398  -0.0456   0.1158   1.0000
   6.250   0.9272   0.01024   0.00417  -0.0447   0.1114   1.0000
   6.500   0.9507   0.01041   0.00435  -0.0438   0.1092   1.0000
   6.750   0.9741   0.01060   0.00456  -0.0429   0.1063   1.0000
   7.000   0.9972   0.01082   0.00477  -0.0421   0.1031   1.0000
   7.250   1.0201   0.01106   0.00499  -0.0412   0.0993   1.0000
   7.500   1.0436   0.01127   0.00522  -0.0404   0.0970   1.0000
   7.750   1.0671   0.01148   0.00545  -0.0396   0.0947   1.0000
   8.000   1.0902   0.01172   0.00570  -0.0388   0.0924   1.0000
   8.250   1.1131   0.01198   0.00596  -0.0379   0.0899   1.0000
   8.500   1.1352   0.01228   0.00626  -0.0370   0.0858   1.0000
   8.750   1.1585   0.01250   0.00652  -0.0362   0.0845   1.0000
   9.000   1.1811   0.01277   0.00679  -0.0353   0.0809   1.0000
   9.250   1.2027   0.01310   0.00709  -0.0344   0.0765   1.0000
   9.500   1.2243   0.01341   0.00742  -0.0334   0.0736   1.0000
   9.750   1.2465   0.01368   0.00772  -0.0325   0.0706   1.0000
  10.000   1.2667   0.01406   0.00807  -0.0313   0.0651   1.0000
  10.250   1.2869   0.01444   0.00844  -0.0302   0.0598   1.0000
  10.500   1.3053   0.01491   0.00887  -0.0288   0.0531   1.0000
  10.750   1.3235   0.01537   0.00932  -0.0273   0.0468   1.0000
  11.000   1.3371   0.01604   0.00992  -0.0252   0.0371   1.0000
  11.250   1.3468   0.01682   0.01065  -0.0224   0.0277   1.0000
  11.500   1.3549   0.01770   0.01149  -0.0195   0.0187   1.0000
  11.750   1.3652   0.01848   0.01228  -0.0170   0.0141   1.0000
  12.000   1.3768   0.01921   0.01303  -0.0148   0.0115   1.0000
  12.250   1.3881   0.01998   0.01382  -0.0126   0.0096   1.0000
  12.500   1.4005   0.02069   0.01458  -0.0107   0.0085   1.0000
  12.750   1.4108   0.02155   0.01548  -0.0087   0.0072   1.0000
  13.000   1.4226   0.02233   0.01632  -0.0070   0.0064   1.0000
  13.250   1.4319   0.02330   0.01734  -0.0051   0.0054   1.0000
  13.500   1.4419   0.02424   0.01834  -0.0033   0.0049   1.0000
  13.750   1.4514   0.02526   0.01942  -0.0017   0.0043   1.0000
  14.000   1.4595   0.02640   0.02062  -0.0001   0.0040   1.0000
  14.250   1.4666   0.02766   0.02194   0.0015   0.0036   1.0000
  14.500   1.4732   0.02901   0.02337   0.0029   0.0033   1.0000
  14.750   1.4796   0.03042   0.02486   0.0041   0.0031   1.0000
  15.000   1.4847   0.03201   0.02652   0.0053   0.0030   1.0000
  15.250   1.4883   0.03379   0.02839   0.0063   0.0028   1.0000
  15.500   1.4920   0.03564   0.03033   0.0071   0.0028   1.0000
  15.750   1.4914   0.03799   0.03277   0.0078   0.0025   1.0000
  16.000   1.4923   0.04032   0.03520   0.0082   0.0025   1.0000
  16.250   1.4888   0.04323   0.03821   0.0084   0.0023   1.0000
  16.500   1.4843   0.04638   0.04147   0.0082   0.0022   1.0000
  16.750   1.4797   0.04975   0.04496   0.0078   0.0022   1.0000
  17.000   1.4727   0.05358   0.04890   0.0069   0.0022   1.0000
  17.250   1.4643   0.05780   0.05324   0.0057   0.0022   1.0000
  17.500   1.4526   0.06272   0.05830   0.0039   0.0022   1.0000
  17.750   1.4372   0.06842   0.06414   0.0016   0.0022   1.0000
  18.000   1.4195   0.07483   0.07069  -0.0013   0.0021   1.0000
  18.250   1.3966   0.08244   0.07847  -0.0050   0.0021   1.0000
  18.500   1.3615   0.09268   0.08891  -0.0103   0.0021   1.0000
  18.750   1.3189   0.10495   0.10139  -0.0169   0.0022   1.0000
  19.000   1.2658   0.11963   0.11630  -0.0248   0.0022   1.0000
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