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SD7062 (14%) (sd7062-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: SD7062 (14%) (sd7062-il)
Reynolds number: 200,000
Max Cl/Cd: 70.27 at α=6.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-sd7062-il-200000-n5.txt
Download as CSV file: xf-sd7062-il-200000-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 =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.000  -0.3202   0.08750   0.08385  -0.0473   1.0000   0.0237
  -9.750  -0.3292   0.08267   0.07908  -0.0489   1.0000   0.0235
  -9.500  -0.4546   0.04741   0.04346  -0.0816   0.9724   0.0216
  -9.250  -0.4679   0.03865   0.03396  -0.0911   0.9447   0.0214
  -9.000  -0.4560   0.03495   0.02985  -0.0935   0.9289   0.0216
  -8.750  -0.4401   0.03221   0.02674  -0.0946   0.9146   0.0217
  -8.500  -0.4223   0.02992   0.02410  -0.0949   0.9016   0.0219
  -8.250  -0.4027   0.02800   0.02186  -0.0949   0.8895   0.0222
  -8.000  -0.3832   0.02636   0.01994  -0.0944   0.8768   0.0225
  -7.750  -0.3622   0.02489   0.01818  -0.0939   0.8655   0.0228
  -7.500  -0.3401   0.02358   0.01661  -0.0933   0.8548   0.0232
  -7.250  -0.3175   0.02248   0.01525  -0.0927   0.8437   0.0238
  -7.000  -0.2938   0.02149   0.01403  -0.0921   0.8339   0.0244
  -6.750  -0.2702   0.02069   0.01319  -0.0916   0.8233   0.0250
  -6.500  -0.2457   0.01997   0.01237  -0.0910   0.8137   0.0256
  -6.250  -0.2211   0.01923   0.01152  -0.0905   0.8037   0.0262
  -6.000  -0.1963   0.01852   0.01069  -0.0899   0.7943   0.0268
  -5.750  -0.1713   0.01786   0.00992  -0.0894   0.7847   0.0274
  -5.500  -0.1459   0.01727   0.00921  -0.0888   0.7753   0.0281
  -5.250  -0.1208   0.01669   0.00858  -0.0884   0.7660   0.0289
  -5.000  -0.0951   0.01620   0.00804  -0.0880   0.7566   0.0298
  -4.750  -0.0691   0.01577   0.00753  -0.0876   0.7475   0.0312
  -4.500  -0.0428   0.01537   0.00706  -0.0872   0.7381   0.0332
  -4.250  -0.0164   0.01501   0.00663  -0.0869   0.7292   0.0354
  -4.000   0.0103   0.01465   0.00621  -0.0865   0.7196   0.0381
  -3.750   0.0370   0.01430   0.00580  -0.0862   0.7109   0.0420
  -3.500   0.0639   0.01396   0.00544  -0.0859   0.7011   0.0490
  -3.250   0.0907   0.01361   0.00510  -0.0856   0.6925   0.0650
  -3.000   0.1174   0.01324   0.00485  -0.0854   0.6825   0.0933
  -2.750   0.1443   0.01295   0.00462  -0.0852   0.6737   0.1272
  -2.500   0.1711   0.01264   0.00444  -0.0851   0.6637   0.1693
  -2.250   0.1975   0.01227   0.00431  -0.0849   0.6548   0.2416
  -2.000   0.2237   0.01191   0.00423  -0.0847   0.6449   0.3224
  -1.750   0.2505   0.01171   0.00416  -0.0844   0.6355   0.3807
  -1.500   0.2774   0.01158   0.00411  -0.0841   0.6259   0.4288
  -1.250   0.3043   0.01147   0.00408  -0.0837   0.6161   0.4754
  -1.000   0.3310   0.01140   0.00405  -0.0833   0.6068   0.5178
  -0.750   0.3578   0.01134   0.00406  -0.0829   0.5966   0.5561
  -0.500   0.3844   0.01131   0.00405  -0.0823   0.5873   0.5924
  -0.250   0.4108   0.01128   0.00407  -0.0818   0.5771   0.6280
   0.000   0.4371   0.01127   0.00408  -0.0812   0.5676   0.6618
   0.250   0.4631   0.01126   0.00411  -0.0805   0.5577   0.6938
   0.500   0.4888   0.01126   0.00415  -0.0798   0.5481   0.7257
   0.750   0.5138   0.01128   0.00418  -0.0789   0.5385   0.7584
   1.000   0.5386   0.01129   0.00423  -0.0779   0.5287   0.7928
   1.250   0.5624   0.01132   0.00426  -0.0767   0.5194   0.8299
   1.500   0.5870   0.01133   0.00431  -0.0756   0.5095   0.8714
   1.750   0.6156   0.01136   0.00433  -0.0754   0.4998   0.9190
   2.000   0.6550   0.01143   0.00433  -0.0776   0.4887   0.9801
   2.250   0.6839   0.01158   0.00439  -0.0779   0.4786   1.0000
   2.750   0.7366   0.01194   0.00457  -0.0773   0.4590   1.0000
   3.000   0.7627   0.01214   0.00468  -0.0770   0.4497   1.0000
   3.250   0.7888   0.01234   0.00481  -0.0767   0.4398   1.0000
   3.500   0.8149   0.01255   0.00495  -0.0764   0.4305   1.0000
   3.750   0.8406   0.01277   0.00511  -0.0760   0.4209   1.0000
   4.000   0.8665   0.01299   0.00528  -0.0757   0.4116   1.0000
   4.250   0.8916   0.01325   0.00545  -0.0752   0.4025   1.0000
   4.500   0.9174   0.01347   0.00566  -0.0749   0.3931   1.0000
   4.750   0.9422   0.01375   0.00586  -0.0744   0.3844   1.0000
   5.000   0.9675   0.01400   0.00609  -0.0740   0.3751   1.0000
   5.250   0.9920   0.01429   0.00633  -0.0735   0.3664   1.0000
   5.500   1.0167   0.01456   0.00658  -0.0730   0.3574   1.0000
   5.750   1.0408   0.01487   0.00685  -0.0725   0.3489   1.0000
   6.000   1.0648   0.01517   0.00713  -0.0719   0.3400   1.0000
   6.250   1.0885   0.01549   0.00743  -0.0713   0.3319   1.0000
   6.500   1.1117   0.01582   0.00774  -0.0706   0.3232   1.0000
   6.750   1.1347   0.01617   0.00807  -0.0699   0.3152   1.0000
   7.000   1.1571   0.01653   0.00842  -0.0692   0.3069   1.0000
   7.250   1.1793   0.01690   0.00878  -0.0684   0.2991   1.0000
   7.500   1.2008   0.01729   0.00916  -0.0675   0.2910   1.0000
   7.750   1.2220   0.01769   0.00957  -0.0666   0.2836   1.0000
   8.000   1.2425   0.01811   0.00999  -0.0656   0.2758   1.0000
   8.250   1.2622   0.01856   0.01043  -0.0645   0.2689   1.0000
   8.500   1.2817   0.01900   0.01090  -0.0634   0.2614   1.0000
   8.750   1.2989   0.01951   0.01139  -0.0619   0.2548   1.0000
   9.000   1.3164   0.01995   0.01188  -0.0605   0.2478   1.0000
   9.250   1.3304   0.02052   0.01244  -0.0586   0.2415   1.0000
   9.500   1.3466   0.02104   0.01301  -0.0571   0.2350   1.0000
   9.750   1.3605   0.02165   0.01364  -0.0553   0.2287   1.0000
  10.000   1.3741   0.02232   0.01432  -0.0536   0.2230   1.0000
  10.250   1.3882   0.02298   0.01504  -0.0521   0.2165   1.0000
  10.500   1.3991   0.02382   0.01587  -0.0503   0.2111   1.0000
  10.750   1.4130   0.02456   0.01669  -0.0490   0.2054   1.0000
  11.000   1.4243   0.02545   0.01761  -0.0474   0.1997   1.0000
  11.250   1.4339   0.02648   0.01866  -0.0459   0.1946   1.0000
  11.500   1.4459   0.02742   0.01968  -0.0446   0.1890   1.0000
  11.750   1.4545   0.02860   0.02089  -0.0432   0.1837   1.0000
  12.000   1.4635   0.02981   0.02215  -0.0420   0.1789   1.0000
  12.250   1.4733   0.03103   0.02345  -0.0409   0.1737   1.0000
  12.500   1.4794   0.03253   0.02498  -0.0398   0.1689   1.0000
  12.750   1.4872   0.03399   0.02650  -0.0388   0.1644   1.0000
  13.000   1.4946   0.03552   0.02812  -0.0379   0.1594   1.0000
  13.250   1.4989   0.03735   0.02998  -0.0371   0.1552   1.0000
  13.500   1.5044   0.03915   0.03186  -0.0363   0.1511   1.0000
  13.750   1.5100   0.04100   0.03381  -0.0358   0.1466   1.0000
  14.000   1.5122   0.04321   0.03606  -0.0353   0.1424   1.0000
  14.250   1.5145   0.04548   0.03838  -0.0349   0.1388   1.0000
  14.500   1.5188   0.04764   0.04067  -0.0346   0.1347   1.0000
  14.750   1.5198   0.05020   0.04330  -0.0345   0.1308   1.0000
  15.000   1.5179   0.05312   0.04625  -0.0345   0.1275   1.0000
  15.250   1.5211   0.05563   0.04889  -0.0346   0.1239   1.0000
  15.500   1.5215   0.05853   0.05189  -0.0349   0.1202   1.0000
  15.750   1.5193   0.06179   0.05520  -0.0353   0.1171   1.0000
  16.000   1.5171   0.06512   0.05860  -0.0359   0.1142   1.0000
  16.250   1.5174   0.06828   0.06190  -0.0365   0.1108   1.0000
  16.500   1.5148   0.07188   0.06560  -0.0374   0.1076   1.0000
  16.750   1.5100   0.07583   0.06960  -0.0384   0.1048   1.0000
  17.000   1.5065   0.07967   0.07353  -0.0395   0.1022   1.0000
  17.250   1.5041   0.08350   0.07750  -0.0407   0.0992   1.0000
  17.500   1.4993   0.08772   0.08182  -0.0421   0.0963   1.0000
  17.750   1.4929   0.09221   0.08637  -0.0438   0.0938   1.0000
  18.000   1.4880   0.09653   0.09077  -0.0454   0.0914   1.0000
  18.250   1.4839   0.10087   0.09526  -0.0471   0.0888   1.0000
  18.500   1.4778   0.10558   0.10008  -0.0490   0.0862   1.0000
  18.750   1.4710   0.11038   0.10495  -0.0511   0.0839   1.0000
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