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WORTMANN FX 62-K-131 AIRFOIL (fx62k131-il) Xfoil prediction polar at RE=1,000,000 Ncrit=0


Details Polar file
Airfoil: WORTMANN FX 62-K-131 AIRFOIL (fx62k131-il)
Reynolds number: 1,000,000
Max Cl/Cd: 162.4 at α=3.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx62k131-il-1000000.txt
Download as CSV file: xf-fx62k131-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 62-K-131 AIRFOIL                    
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -14.250  -0.1606   0.13427   0.13265  -0.0721   0.9763   0.0051
 -14.000  -0.1530   0.13115   0.12952  -0.0746   0.9702   0.0053
 -13.750  -0.1435   0.12763   0.12599  -0.0776   0.9640   0.0054
 -13.500  -0.1337   0.12397   0.12231  -0.0807   0.9578   0.0056
 -13.250  -0.1236   0.12008   0.11838  -0.0840   0.9496   0.0059
 -13.000  -0.1144   0.11615   0.11441  -0.0870   0.9371   0.0061
 -12.750  -0.1089   0.11255   0.11072  -0.0890   0.9209   0.0063
 -12.500  -0.1058   0.10919   0.10727  -0.0904   0.9069   0.0064
 -12.250  -0.1025   0.10587   0.10390  -0.0914   0.8973   0.0065
 -12.000  -0.0993   0.10259   0.10058  -0.0924   0.8898   0.0065
 -11.750  -0.0964   0.09912   0.09708  -0.0933   0.8834   0.0065
 -11.500  -0.0938   0.09562   0.09354  -0.0943   0.8782   0.0065
 -11.250  -0.0916   0.09199   0.08990  -0.0952   0.8736   0.0065
 -11.000  -0.0887   0.08820   0.08609  -0.0964   0.8693   0.0065
 -10.750  -0.0874   0.08439   0.08225  -0.0974   0.8653   0.0066
 -10.500  -0.0854   0.08042   0.07828  -0.0987   0.8617   0.0066
 -10.250  -0.0843   0.07628   0.07413  -0.0999   0.8581   0.0066
 -10.000  -0.0837   0.07212   0.06996  -0.1012   0.8548   0.0066
  -9.750  -0.0835   0.06772   0.06553  -0.1027   0.8516   0.0066
  -9.500  -0.0834   0.06323   0.06105  -0.1044   0.8487   0.0066
  -9.250  -0.1614   0.07721   0.07500  -0.1027   0.8604   0.0066
  -9.000  -0.1578   0.07260   0.07038  -0.1059   0.8556   0.0066
  -8.750  -0.1544   0.06752   0.06527  -0.1099   0.8511   0.0066
  -8.500  -0.1511   0.06035   0.05811  -0.1175   0.8467   0.0066
  -8.250  -0.1527   0.05380   0.05147  -0.1246   0.8417   0.0066
  -8.000  -0.1555   0.04883   0.04636  -0.1296   0.8368   0.0066
  -7.750  -0.1500   0.04374   0.04112  -0.1352   0.8328   0.0066
  -7.500  -0.1410   0.03899   0.03616  -0.1385   0.8293   0.0066
  -7.250  -0.1403   0.02983   0.02646  -0.1432   0.8254   0.0069
  -7.000  -0.1196   0.02725   0.02367  -0.1452   0.8226   0.0073
  -6.750  -0.0955   0.02571   0.02201  -0.1467   0.8201   0.0077
  -6.500  -0.0697   0.02386   0.01997  -0.1479   0.8176   0.0086
  -6.250  -0.0385   0.02456   0.02052  -0.1477   0.8152   0.0105
  -6.000  -0.0111   0.02217   0.01780  -0.1491   0.8128   0.0106
  -5.750   0.0151   0.01509   0.01011  -0.1507   0.8104   0.0081
  -5.500   0.0439   0.01431   0.00923  -0.1514   0.8082   0.0088
  -5.250   0.0715   0.01254   0.00727  -0.1513   0.8059   0.0084
  -5.000   0.1000   0.01113   0.00572  -0.1517   0.8031   0.0081
  -4.750   0.1304   0.01037   0.00488  -0.1526   0.8002   0.0085
  -4.500   0.1616   0.00989   0.00432  -0.1537   0.7973   0.0096
  -4.250   0.1924   0.00965   0.00402  -0.1546   0.7946   0.0105
  -4.000   0.2274   0.00886   0.00314  -0.1568   0.7923   0.0125
  -3.750   0.2586   0.00862   0.00289  -0.1579   0.7899   0.0152
  -3.500   0.2910   0.00832   0.00252  -0.1591   0.7875   0.0193
  -3.250   0.3263   0.00785   0.00221  -0.1613   0.7853   0.0766
  -3.000   0.3787   0.00647   0.00187  -0.1688   0.7834   0.4123
  -2.750   0.4218   0.00596   0.00179  -0.1730   0.7812   0.5771
  -2.500   0.4548   0.00585   0.00181  -0.1744   0.7789   0.6324
  -2.250   0.4856   0.00585   0.00183  -0.1752   0.7762   0.6603
  -2.000   0.5157   0.00587   0.00184  -0.1757   0.7735   0.6759
  -1.750   0.5451   0.00593   0.00191  -0.1761   0.7709   0.6926
  -1.500   0.5747   0.00601   0.00193  -0.1766   0.7682   0.7007
  -1.250   0.6041   0.00603   0.00195  -0.1771   0.7655   0.7055
  -1.000   0.6332   0.00606   0.00198  -0.1775   0.7626   0.7100
  -0.750   0.6629   0.00609   0.00199  -0.1780   0.7595   0.7144
  -0.500   0.6924   0.00612   0.00199  -0.1786   0.7565   0.7182
  -0.250   0.7213   0.00617   0.00203  -0.1789   0.7530   0.7214
   0.000   0.7499   0.00618   0.00206  -0.1792   0.7484   0.7253
   0.250   0.7789   0.00621   0.00207  -0.1796   0.7436   0.7296
   0.500   0.8078   0.00627   0.00209  -0.1800   0.7395   0.7329
   0.750   0.8362   0.00628   0.00215  -0.1802   0.7353   0.7360
   1.000   0.8646   0.00633   0.00221  -0.1805   0.7309   0.7398
   1.250   0.8934   0.00640   0.00226  -0.1808   0.7264   0.7435
   1.500   0.9222   0.00642   0.00231  -0.1812   0.7213   0.7465
   1.750   0.9502   0.00645   0.00236  -0.1814   0.7159   0.7490
   2.000   0.9782   0.00651   0.00243  -0.1816   0.7108   0.7515
   2.250   1.0065   0.00655   0.00252  -0.1818   0.7045   0.7542
   2.500   1.0347   0.00663   0.00258  -0.1821   0.6984   0.7570
   2.750   1.0633   0.00668   0.00265  -0.1824   0.6902   0.7594
   3.000   1.0904   0.00674   0.00272  -0.1824   0.6783   0.7615
   3.250   1.1157   0.00687   0.00281  -0.1820   0.6579   0.7637
   3.500   1.1402   0.00708   0.00293  -0.1815   0.6304   0.7659
   3.750   1.1650   0.00731   0.00309  -0.1810   0.6052   0.7683
   4.000   1.1883   0.00766   0.00331  -0.1803   0.5742   0.7709
   4.250   1.2117   0.00802   0.00356  -0.1797   0.5443   0.7733
   4.500   1.2323   0.00852   0.00388  -0.1785   0.5019   0.7753
   4.750   1.2500   0.00919   0.00429  -0.1768   0.4435   0.7773
   5.000   1.2644   0.01009   0.00483  -0.1745   0.3724   0.7795
   5.250   1.2766   0.01114   0.00548  -0.1719   0.2968   0.7819
   5.500   1.2878   0.01223   0.00617  -0.1692   0.2233   0.7843
   5.750   1.2972   0.01341   0.00696  -0.1662   0.1515   0.7866
   6.000   1.3099   0.01431   0.00762  -0.1638   0.1062   0.7888
   6.250   1.3187   0.01527   0.00834  -0.1606   0.0636   0.7908
   6.500   1.3279   0.01606   0.00900  -0.1574   0.0366   0.7928
   6.750   1.3357   0.01710   0.00989  -0.1540   0.0107   0.7950
   7.000   1.3486   0.01790   0.01065  -0.1516   0.0044   0.7973
   7.250   1.3641   0.01856   0.01135  -0.1497   0.0035   0.7996
   7.500   1.3790   0.01927   0.01213  -0.1478   0.0031   0.8015
   7.750   1.3930   0.02001   0.01297  -0.1458   0.0029   0.8033
   8.000   1.4068   0.02076   0.01380  -0.1438   0.0028   0.8051
   8.250   1.4197   0.02160   0.01472  -0.1417   0.0027   0.8071
   8.500   1.4322   0.02249   0.01569  -0.1397   0.0026   0.8091
   8.750   1.4436   0.02350   0.01678  -0.1376   0.0025   0.8112
   9.000   1.4543   0.02459   0.01795  -0.1355   0.0024   0.8132
   9.250   1.4644   0.02578   0.01922  -0.1334   0.0023   0.8150
   9.500   1.4733   0.02703   0.02056  -0.1312   0.0021   0.8169
   9.750   1.4810   0.02843   0.02206  -0.1290   0.0020   0.8187
  10.000   1.4850   0.03013   0.02386  -0.1264   0.0018   0.8205
  10.250   1.4846   0.03227   0.02613  -0.1234   0.0017   0.8222
  10.500   1.4795   0.03490   0.02891  -0.1200   0.0016   0.8241
  10.750   1.4752   0.03754   0.03172  -0.1168   0.0016   0.8258
  11.000   1.4713   0.04027   0.03459  -0.1138   0.0016   0.8274
  11.250   1.4727   0.04254   0.03698  -0.1114   0.0016   0.8288
  11.500   1.4736   0.04490   0.03947  -0.1091   0.0016   0.8304
  11.750   1.4730   0.04754   0.04227  -0.1066   0.0016   0.8319
  12.000   1.4750   0.04990   0.04476  -0.1046   0.0016   0.8334
  12.250   1.4771   0.05226   0.04725  -0.1028   0.0016   0.8349
  12.500   1.4781   0.05483   0.04996  -0.1011   0.0016   0.8365
  12.750   1.4790   0.05746   0.05273  -0.0996   0.0016   0.8381
  13.000   1.4790   0.06020   0.05561  -0.0983   0.0016   0.8398
  13.250   1.4781   0.06311   0.05866  -0.0971   0.0016   0.8413
  13.500   1.4762   0.06624   0.06193  -0.0961   0.0017   0.8428
  13.750   1.4730   0.06968   0.06554  -0.0952   0.0017   0.8442
  14.000   1.2367   0.07593   0.07221  -0.0714   0.0016   0.8361
  14.250   1.2216   0.07999   0.07642  -0.0705   0.0016   0.8369
  14.500   1.1990   0.08351   0.08008  -0.0692   0.0017   0.8373
  14.750   1.1806   0.08730   0.08403  -0.0688   0.0017   0.8381
  15.000   1.1655   0.09124   0.08811  -0.0690   0.0017   0.8390
  15.250   1.1516   0.09518   0.09219  -0.0696   0.0017   0.8400
  15.500   1.1371   0.09940   0.09656  -0.0705   0.0017   0.8409
  15.750   1.1206   0.10398   0.10129  -0.0718   0.0018   0.8416
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