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SD7062 (14%) (sd7062-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: SD7062 (14%) (sd7062-il)
Reynolds number: 500,000
Max Cl/Cd: 94.55 at α=6.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-sd7062-il-500000-n5.txt
Download as CSV file: xf-sd7062-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: SD7062 (14%)                                    
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -12.000  -0.5996   0.05550   0.05250  -0.0689   1.0000   0.0136
 -11.750  -0.6390   0.04501   0.04177  -0.0782   1.0000   0.0135
 -11.500  -0.6639   0.03928   0.03586  -0.0827   1.0000   0.0135
 -11.250  -0.6684   0.03437   0.03066  -0.0892   0.9806   0.0135
 -11.000  -0.6534   0.03100   0.02697  -0.0934   0.9614   0.0136
 -10.750  -0.6346   0.02855   0.02422  -0.0957   0.9427   0.0138
 -10.500  -0.6179   0.02675   0.02215  -0.0962   0.9223   0.0140
 -10.250  -0.6023   0.02538   0.02052  -0.0956   0.9031   0.0141
 -10.000  -0.5855   0.02425   0.01914  -0.0948   0.8859   0.0142
  -9.750  -0.5693   0.02290   0.01759  -0.0939   0.8707   0.0144
  -9.500  -0.5507   0.02179   0.01633  -0.0931   0.8569   0.0146
  -9.250  -0.5303   0.02086   0.01526  -0.0924   0.8448   0.0147
  -9.000  -0.5087   0.02006   0.01434  -0.0917   0.8334   0.0149
  -8.750  -0.4862   0.01933   0.01349  -0.0912   0.8220   0.0151
  -8.500  -0.4631   0.01862   0.01266  -0.0906   0.8120   0.0152
  -8.250  -0.4395   0.01797   0.01189  -0.0901   0.8016   0.0154
  -8.000  -0.4153   0.01734   0.01114  -0.0897   0.7921   0.0156
  -7.750  -0.3909   0.01675   0.01043  -0.0892   0.7824   0.0159
  -7.500  -0.3659   0.01617   0.00976  -0.0888   0.7731   0.0161
  -7.000  -0.3151   0.01514   0.00853  -0.0881   0.7546   0.0166
  -6.750  -0.2894   0.01469   0.00797  -0.0877   0.7456   0.0169
  -6.500  -0.2631   0.01426   0.00746  -0.0874   0.7365   0.0171
  -6.250  -0.2371   0.01383   0.00693  -0.0870   0.7277   0.0174
  -6.000  -0.2110   0.01334   0.00641  -0.0868   0.7186   0.0178
  -5.750  -0.1845   0.01299   0.00600  -0.0865   0.7099   0.0182
  -5.500  -0.1573   0.01268   0.00564  -0.0863   0.7007   0.0188
  -5.250  -0.1303   0.01240   0.00529  -0.0861   0.6920   0.0194
  -5.000  -0.1029   0.01212   0.00495  -0.0859   0.6828   0.0200
  -4.750  -0.0756   0.01188   0.00463  -0.0857   0.6741   0.0205
  -4.500  -0.0482   0.01158   0.00429  -0.0855   0.6647   0.0211
  -4.250  -0.0207   0.01135   0.00401  -0.0853   0.6559   0.0219
  -4.000   0.0070   0.01115   0.00376  -0.0852   0.6464   0.0229
  -3.750   0.0348   0.01099   0.00353  -0.0850   0.6374   0.0240
  -3.500   0.0626   0.01080   0.00331  -0.0849   0.6279   0.0257
  -3.250   0.0905   0.01064   0.00312  -0.0847   0.6188   0.0287
  -3.000   0.1182   0.01046   0.00293  -0.0846   0.6091   0.0356
  -2.750   0.1460   0.01026   0.00277  -0.0845   0.5999   0.0515
  -2.500   0.1736   0.01009   0.00263  -0.0843   0.5903   0.0718
  -2.250   0.2015   0.00992   0.00252  -0.0843   0.5809   0.0959
  -2.000   0.2290   0.00977   0.00242  -0.0842   0.5711   0.1244
  -1.750   0.2568   0.00956   0.00233  -0.0842   0.5615   0.1671
  -1.500   0.2842   0.00935   0.00227  -0.0841   0.5522   0.2237
  -1.250   0.3118   0.00916   0.00222  -0.0841   0.5425   0.2791
  -1.000   0.3393   0.00900   0.00220  -0.0840   0.5332   0.3371
  -0.750   0.3669   0.00888   0.00219  -0.0839   0.5232   0.3893
  -0.500   0.3946   0.00879   0.00220  -0.0838   0.5140   0.4374
  -0.250   0.4222   0.00876   0.00222  -0.0837   0.5042   0.4766
   0.000   0.4500   0.00874   0.00225  -0.0835   0.4948   0.5096
   0.250   0.4775   0.00875   0.00229  -0.0833   0.4853   0.5414
   0.500   0.5052   0.00874   0.00233  -0.0832   0.4754   0.5737
   0.750   0.5326   0.00877   0.00238  -0.0830   0.4663   0.6034
   1.000   0.5600   0.00880   0.00244  -0.0828   0.4562   0.6307
   1.250   0.5873   0.00884   0.00251  -0.0825   0.4471   0.6586
   1.500   0.6142   0.00889   0.00259  -0.0822   0.4372   0.6864
   2.250   0.6939   0.00903   0.00287  -0.0810   0.4098   0.7779
   2.500   0.7191   0.00910   0.00298  -0.0803   0.4010   0.8119
   2.750   0.7438   0.00913   0.00308  -0.0794   0.3921   0.8494
   3.000   0.7668   0.00918   0.00319  -0.0782   0.3837   0.8934
   3.250   0.7954   0.00922   0.00327  -0.0781   0.3747   0.9507
   3.500   0.8295   0.00938   0.00337  -0.0795   0.3652   1.0000
   3.750   0.8563   0.00957   0.00349  -0.0792   0.3561   1.0000
   4.000   0.8829   0.00975   0.00363  -0.0790   0.3482   1.0000
   4.250   0.9093   0.00995   0.00377  -0.0788   0.3391   1.0000
   4.500   0.9357   0.01015   0.00393  -0.0785   0.3310   1.0000
   4.750   0.9617   0.01037   0.00409  -0.0782   0.3222   1.0000
   5.000   0.9878   0.01058   0.00426  -0.0779   0.3144   1.0000
   5.250   1.0134   0.01081   0.00445  -0.0776   0.3057   1.0000
   5.500   1.0392   0.01103   0.00464  -0.0773   0.2981   1.0000
   5.750   1.0644   0.01129   0.00485  -0.0769   0.2895   1.0000
   6.000   1.0898   0.01153   0.00506  -0.0765   0.2823   1.0000
   6.250   1.1145   0.01180   0.00529  -0.0760   0.2742   1.0000
   6.500   1.1393   0.01205   0.00553  -0.0756   0.2669   1.0000
   6.750   1.1635   0.01234   0.00578  -0.0750   0.2590   1.0000
   7.000   1.1877   0.01262   0.00604  -0.0745   0.2521   1.0000
   7.250   1.2114   0.01291   0.00631  -0.0739   0.2447   1.0000
   7.500   1.2346   0.01322   0.00661  -0.0732   0.2381   1.0000
   7.750   1.2579   0.01352   0.00689  -0.0726   0.2311   1.0000
   8.000   1.2798   0.01388   0.00722  -0.0717   0.2243   1.0000
   8.250   1.3024   0.01418   0.00754  -0.0710   0.2179   1.0000
   8.500   1.3230   0.01458   0.00790  -0.0700   0.2112   1.0000
   8.750   1.3445   0.01491   0.00824  -0.0691   0.2052   1.0000
   9.000   1.3644   0.01530   0.00863  -0.0679   0.1990   1.0000
   9.250   1.3822   0.01569   0.00902  -0.0665   0.1936   1.0000
   9.500   1.3997   0.01608   0.00942  -0.0649   0.1875   1.0000
   9.750   1.4145   0.01658   0.00990  -0.0630   0.1818   1.0000
  10.000   1.4314   0.01701   0.01035  -0.0615   0.1768   1.0000
  10.250   1.4465   0.01753   0.01087  -0.0598   0.1711   1.0000
  10.500   1.4603   0.01812   0.01147  -0.0580   0.1661   1.0000
  10.750   1.4757   0.01866   0.01205  -0.0565   0.1611   1.0000
  11.000   1.4885   0.01935   0.01274  -0.0548   0.1558   1.0000
  11.250   1.5015   0.02007   0.01347  -0.0532   0.1511   1.0000
  11.500   1.5147   0.02080   0.01423  -0.0517   0.1463   1.0000
  11.750   1.5252   0.02172   0.01516  -0.0501   0.1414   1.0000
  12.000   1.5373   0.02259   0.01607  -0.0487   0.1373   1.0000
  12.250   1.5483   0.02356   0.01707  -0.0474   0.1326   1.0000
  12.500   1.5563   0.02477   0.01829  -0.0459   0.1278   1.0000
  12.750   1.5673   0.02584   0.01942  -0.0447   0.1241   1.0000
  13.000   1.5763   0.02708   0.02069  -0.0436   0.1199   1.0000
  13.250   1.5830   0.02856   0.02219  -0.0424   0.1161   1.0000
  13.500   1.5913   0.02996   0.02365  -0.0414   0.1127   1.0000
  13.750   1.5986   0.03148   0.02522  -0.0405   0.1090   1.0000
  14.000   1.6035   0.03327   0.02704  -0.0396   0.1054   1.0000
  14.250   1.6082   0.03515   0.02897  -0.0388   0.1021   1.0000
  14.500   1.6139   0.03697   0.03086  -0.0382   0.0990   1.0000
  14.750   1.6172   0.03908   0.03302  -0.0377   0.0959   1.0000
  15.000   1.6174   0.04157   0.03555  -0.0372   0.0927   1.0000
  15.250   1.6214   0.04377   0.03783  -0.0369   0.0902   1.0000
  15.500   1.6234   0.04622   0.04035  -0.0367   0.0874   1.0000
  15.750   1.6235   0.04899   0.04317  -0.0367   0.0847   1.0000
  16.000   1.6205   0.05219   0.04642  -0.0369   0.0821   1.0000
  16.250   1.6222   0.05493   0.04926  -0.0371   0.0800   1.0000
  16.500   1.6215   0.05803   0.05244  -0.0375   0.0776   1.0000
  16.750   1.6185   0.06151   0.05599  -0.0380   0.0753   1.0000
  17.000   1.6125   0.06546   0.06000  -0.0388   0.0729   1.0000
  17.250   1.6104   0.06897   0.06361  -0.0396   0.0711   1.0000
  17.500   1.6072   0.07273   0.06746  -0.0406   0.0690   1.0000
  17.750   1.6015   0.07692   0.07173  -0.0417   0.0669   1.0000
  18.000   1.5935   0.08149   0.07638  -0.0431   0.0650   1.0000
  18.250   1.5862   0.08608   0.08105  -0.0447   0.0634   1.0000
  18.500   1.5821   0.09026   0.08534  -0.0461   0.0617   1.0000
  18.750   1.5758   0.09481   0.08998  -0.0478   0.0600   1.0000
  19.000   1.5673   0.09979   0.09504  -0.0497   0.0583   1.0000
  19.250   1.5571   0.10513   0.10045  -0.0519   0.0566   1.0000
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