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SD7062 (14%) (sd7062-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: SD7062 (14%) (sd7062-il)
Reynolds number: 500,000
Max Cl/Cd: 99.11 at α=6.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-sd7062-il-500000.txt
Download as CSV file: xf-sd7062-il-500000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.500  -0.2839   0.10278   0.10045  -0.0402   1.0000   0.0304
 -10.250  -0.2827   0.09935   0.09705  -0.0413   1.0000   0.0310
 -10.000  -0.3149   0.08823   0.08598  -0.0486   1.0000   0.0330
  -9.750  -0.3076   0.08690   0.08469  -0.0476   1.0000   0.0333
  -9.500  -0.3053   0.08466   0.08249  -0.0474   1.0000   0.0335
  -9.250  -0.2200   0.05864   0.05657  -0.0694   0.9597   0.0382
  -9.000  -0.2038   0.05529   0.05319  -0.0723   0.9426   0.0385
  -8.750  -0.4363   0.02992   0.02561  -0.0973   0.9134   0.0244
  -8.500  -0.4197   0.02772   0.02326  -0.0965   0.8989   0.0240
  -8.250  -0.4050   0.02539   0.02063  -0.0956   0.8853   0.0239
  -8.000  -0.3872   0.02366   0.01857  -0.0946   0.8726   0.0240
  -7.750  -0.3670   0.02220   0.01682  -0.0938   0.8604   0.0241
  -7.500  -0.3454   0.02078   0.01516  -0.0930   0.8499   0.0241
  -7.250  -0.3225   0.01955   0.01370  -0.0924   0.8390   0.0241
  -7.000  -0.2983   0.01856   0.01252  -0.0918   0.8290   0.0242
  -6.750  -0.2746   0.01725   0.01103  -0.0912   0.8193   0.0244
  -6.500  -0.2500   0.01616   0.00988  -0.0907   0.8096   0.0247
  -6.250  -0.2249   0.01541   0.00905  -0.0902   0.8004   0.0251
  -6.000  -0.1991   0.01479   0.00839  -0.0898   0.7907   0.0255
  -5.750  -0.1733   0.01426   0.00776  -0.0893   0.7819   0.0260
  -5.500  -0.1470   0.01374   0.00719  -0.0889   0.7723   0.0265
  -5.000  -0.0938   0.01288   0.00619  -0.0881   0.7541   0.0279
  -4.750  -0.0677   0.01241   0.00563  -0.0877   0.7456   0.0287
  -4.500  -0.0410   0.01195   0.00518  -0.0875   0.7360   0.0299
  -4.250  -0.0140   0.01165   0.00480  -0.0872   0.7274   0.0310
  -4.000   0.0135   0.01134   0.00445  -0.0869   0.7178   0.0323
  -3.750   0.0406   0.01100   0.00405  -0.0867   0.7091   0.0341
  -3.500   0.0684   0.01074   0.00377  -0.0865   0.6995   0.0367
  -3.250   0.0959   0.01048   0.00348  -0.0863   0.6907   0.0414
  -3.000   0.1233   0.01008   0.00317  -0.0861   0.6811   0.0628
  -2.750   0.1502   0.00963   0.00294  -0.0860   0.6721   0.1223
  -2.500   0.1777   0.00934   0.00279  -0.0859   0.6625   0.1726
  -2.250   0.2052   0.00909   0.00268  -0.0858   0.6533   0.2260
  -2.000   0.2326   0.00886   0.00259  -0.0857   0.6435   0.2822
  -1.750   0.2601   0.00862   0.00254  -0.0856   0.6340   0.3465
  -1.500   0.2874   0.00844   0.00251  -0.0855   0.6245   0.4118
  -1.250   0.3151   0.00830   0.00250  -0.0853   0.6148   0.4663
  -1.000   0.3425   0.00823   0.00249  -0.0851   0.6054   0.5150
  -0.750   0.3702   0.00815   0.00251  -0.0849   0.5953   0.5567
  -0.500   0.3976   0.00811   0.00252  -0.0846   0.5859   0.5955
  -0.250   0.4251   0.00808   0.00254  -0.0843   0.5758   0.6302
   0.000   0.4526   0.00807   0.00256  -0.0840   0.5661   0.6624
   0.250   0.4797   0.00808   0.00260  -0.0837   0.5562   0.6950
   0.500   0.5067   0.00806   0.00264  -0.0833   0.5463   0.7284
   0.750   0.5330   0.00808   0.00269  -0.0827   0.5367   0.7612
   1.000   0.5593   0.00807   0.00274  -0.0821   0.5265   0.7946
   1.250   0.5845   0.00808   0.00280  -0.0813   0.5170   0.8301
   1.500   0.6086   0.00808   0.00286  -0.0801   0.5070   0.8690
   1.750   0.6314   0.00807   0.00291  -0.0787   0.4977   0.9145
   2.000   0.6651   0.00812   0.00292  -0.0796   0.4872   0.9681
   2.250   0.7016   0.00821   0.00296  -0.0814   0.4764   1.0000
   2.500   0.7286   0.00837   0.00302  -0.0812   0.4669   1.0000
   2.750   0.7558   0.00851   0.00310  -0.0811   0.4567   1.0000
   3.000   0.7829   0.00867   0.00319  -0.0809   0.4472   1.0000
   3.250   0.8097   0.00884   0.00329  -0.0807   0.4374   1.0000
   3.500   0.8369   0.00899   0.00340  -0.0805   0.4276   1.0000
   3.750   0.8632   0.00921   0.00352  -0.0802   0.4181   1.0000
   4.000   0.8903   0.00935   0.00365  -0.0801   0.4086   1.0000
   4.250   0.9166   0.00956   0.00379  -0.0798   0.3993   1.0000
   4.500   0.9431   0.00975   0.00394  -0.0796   0.3897   1.0000
   4.750   0.9693   0.00995   0.00409  -0.0793   0.3807   1.0000
   5.000   0.9952   0.01018   0.00426  -0.0789   0.3712   1.0000
   5.250   1.0214   0.01037   0.00444  -0.0787   0.3623   1.0000
   5.500   1.0465   0.01064   0.00463  -0.0782   0.3531   1.0000
   5.750   1.0726   0.01083   0.00482  -0.0779   0.3441   1.0000
   6.000   1.0972   0.01112   0.00505  -0.0774   0.3354   1.0000
   6.250   1.1229   0.01133   0.00525  -0.0771   0.3267   1.0000
   6.500   1.1472   0.01162   0.00549  -0.0766   0.3182   1.0000
   6.750   1.1722   0.01186   0.00573  -0.0761   0.3096   1.0000
   7.000   1.1960   0.01217   0.00599  -0.0755   0.3014   1.0000
   7.250   1.2204   0.01243   0.00625  -0.0750   0.2932   1.0000
   7.500   1.2435   0.01275   0.00655  -0.0743   0.2854   1.0000
   7.750   1.2671   0.01304   0.00683  -0.0737   0.2774   1.0000
   8.000   1.2893   0.01339   0.00715  -0.0729   0.2699   1.0000
   8.250   1.3123   0.01369   0.00746  -0.0722   0.2623   1.0000
   8.500   1.3330   0.01409   0.00782  -0.0712   0.2550   1.0000
   8.750   1.3553   0.01439   0.00814  -0.0704   0.2477   1.0000
   9.000   1.3740   0.01486   0.00856  -0.0691   0.2406   1.0000
   9.250   1.3956   0.01515   0.00890  -0.0682   0.2340   1.0000
   9.500   1.4120   0.01561   0.00932  -0.0665   0.2271   1.0000
   9.750   1.4297   0.01598   0.00973  -0.0650   0.2210   1.0000
  10.000   1.4452   0.01644   0.01018  -0.0632   0.2145   1.0000
  10.250   1.4597   0.01696   0.01070  -0.0613   0.2085   1.0000
  10.500   1.4758   0.01743   0.01120  -0.0598   0.2025   1.0000
  10.750   1.4875   0.01811   0.01186  -0.0577   0.1964   1.0000
  11.000   1.5036   0.01862   0.01242  -0.0563   0.1909   1.0000
  11.250   1.5162   0.01932   0.01312  -0.0546   0.1850   1.0000
  11.500   1.5276   0.02011   0.01392  -0.0528   0.1797   1.0000
  11.750   1.5416   0.02080   0.01466  -0.0514   0.1743   1.0000
  12.000   1.5506   0.02179   0.01564  -0.0496   0.1689   1.0000
  12.250   1.5628   0.02266   0.01656  -0.0483   0.1639   1.0000
  12.500   1.5736   0.02364   0.01757  -0.0469   0.1587   1.0000
  12.750   1.5792   0.02501   0.01893  -0.0452   0.1537   1.0000
  13.000   1.5919   0.02596   0.01997  -0.0442   0.1494   1.0000
  13.250   1.6002   0.02726   0.02129  -0.0430   0.1448   1.0000
  13.500   1.6031   0.02902   0.02304  -0.0416   0.1402   1.0000
  13.750   1.6146   0.03018   0.02430  -0.0408   0.1363   1.0000
  14.000   1.6209   0.03179   0.02595  -0.0399   0.1320   1.0000
  14.250   1.6218   0.03392   0.02808  -0.0389   0.1278   1.0000
  14.500   1.6303   0.03546   0.02971  -0.0382   0.1244   1.0000
  14.750   1.6351   0.03736   0.03168  -0.0376   0.1206   1.0000
  15.000   1.6349   0.03980   0.03413  -0.0370   0.1169   1.0000
  15.250   1.6370   0.04211   0.03651  -0.0366   0.1137   1.0000
  15.500   1.6418   0.04422   0.03870  -0.0363   0.1103   1.0000
  15.750   1.6419   0.04688   0.04142  -0.0361   0.1072   1.0000
  16.000   1.6368   0.05021   0.04477  -0.0362   0.1040   1.0000
  16.250   1.6401   0.05270   0.04736  -0.0362   0.1013   1.0000
  16.500   1.6411   0.05552   0.05027  -0.0365   0.0984   1.0000
  16.750   1.6376   0.05896   0.05376  -0.0369   0.0956   1.0000
  17.000   1.6290   0.06311   0.05795  -0.0376   0.0927   1.0000
  17.250   1.6305   0.06609   0.06104  -0.0382   0.0904   1.0000
  17.500   1.6288   0.06956   0.06460  -0.0390   0.0877   1.0000
  17.750   1.6229   0.07367   0.06877  -0.0401   0.0852   1.0000
  18.000   1.6128   0.07841   0.07355  -0.0414   0.0828   1.0000
  18.250   1.6096   0.08230   0.07755  -0.0426   0.0807   1.0000
  18.500   1.6068   0.08620   0.08155  -0.0439   0.0784   1.0000
  18.750   1.6002   0.09074   0.08616  -0.0455   0.0762   1.0000
  19.000   1.5896   0.09590   0.09137  -0.0474   0.0740   1.0000
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