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WORTMANN FX 62-K-131 AIRFOIL (fx62k131-il) Xfoil prediction polar at RE=500,000 Ncrit=0


Details Polar file
Airfoil: WORTMANN FX 62-K-131 AIRFOIL (fx62k131-il)
Reynolds number: 500,000
Max Cl/Cd: 123.98 at α=4.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx62k131-il-500000.txt
Download as CSV file: xf-fx62k131-il-500000.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 =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.250  -0.1797   0.13856   0.13640  -0.0652   0.9894   0.0098
 -14.000  -0.1737   0.13575   0.13357  -0.0677   0.9881   0.0101
 -13.750  -0.1676   0.13274   0.13055  -0.0704   0.9869   0.0102
 -13.500  -0.1619   0.12955   0.12736  -0.0732   0.9851   0.0103
 -13.250  -0.1567   0.12639   0.12420  -0.0752   0.9797   0.0104
 -13.000  -0.1491   0.12287   0.12067  -0.0777   0.9761   0.0105
 -12.750  -0.1414   0.11919   0.11698  -0.0802   0.9725   0.0105
 -12.500  -0.1344   0.11545   0.11324  -0.0825   0.9676   0.0105
 -12.250  -0.1264   0.11141   0.10919  -0.0852   0.9640   0.0105
 -12.000  -0.1183   0.10730   0.10507  -0.0880   0.9607   0.0106
 -11.750  -0.1112   0.10311   0.10087  -0.0906   0.9558   0.0106
 -11.500  -0.1104   0.09739   0.09516  -0.0925   0.9517   0.0111
 -11.250  -0.1006   0.09372   0.09147  -0.0946   0.9469   0.0114
 -11.000  -0.0918   0.08989   0.08761  -0.0968   0.9404   0.0117
 -10.750  -0.0850   0.08610   0.08379  -0.0988   0.9340   0.0121
 -10.500  -0.0804   0.08228   0.07994  -0.1004   0.9265   0.0123
 -10.250  -0.0767   0.07842   0.07604  -0.1020   0.9200   0.0127
 -10.000  -0.0749   0.07459   0.07219  -0.1033   0.9131   0.0130
  -9.750  -0.0732   0.07055   0.06810  -0.1049   0.9075   0.0135
  -9.500  -0.0726   0.06646   0.06401  -0.1064   0.9018   0.0138
  -9.250  -0.0735   0.06228   0.05981  -0.1079   0.8965   0.0142
  -9.000  -0.0742   0.05779   0.05529  -0.1100   0.8921   0.0145
  -8.750  -0.0763   0.05299   0.05050  -0.1125   0.8872   0.0149
  -8.500  -0.0788   0.04748   0.04498  -0.1164   0.8827   0.0152
  -8.250  -0.0873   0.04111   0.03856  -0.1222   0.8782   0.0147
  -8.000  -0.0981   0.03565   0.03303  -0.1275   0.8729   0.0145
  -7.750  -0.1083   0.03159   0.02885  -0.1308   0.8678   0.0146
  -7.500  -0.1042   0.02738   0.02441  -0.1349   0.8638   0.0156
  -7.250  -0.0877   0.02547   0.02224  -0.1365   0.8597   0.0166
  -7.000  -0.0770   0.02219   0.01870  -0.1380   0.8558   0.0167
  -6.750  -0.0756   0.01470   0.01075  -0.1408   0.8525   0.0176
  -6.500  -0.0579   0.01227   0.00823  -0.1419   0.8495   0.0187
  -6.250  -0.0366   0.01075   0.00658  -0.1428   0.8462   0.0203
  -6.000  -0.0112   0.00973   0.00536  -0.1434   0.8433   0.0241
  -5.750   0.0194   0.01006   0.00538  -0.1434   0.8403   0.0260
  -5.250   0.0706   0.01795   0.01215  -0.1526   0.8429   0.0174
  -5.000   0.0968   0.01536   0.00939  -0.1522   0.8404   0.0144
  -4.750   0.1245   0.01402   0.00789  -0.1521   0.8379   0.0143
  -4.500   0.1519   0.01315   0.00695  -0.1521   0.8351   0.0153
  -4.250   0.1804   0.01260   0.00633  -0.1525   0.8318   0.0165
  -4.000   0.2125   0.01152   0.00517  -0.1542   0.8286   0.0199
  -3.750   0.2457   0.01099   0.00456  -0.1557   0.8257   0.0230
  -3.500   0.2798   0.01055   0.00400  -0.1574   0.8231   0.0302
  -3.250   0.3413   0.00820   0.00328  -0.1680   0.8211   0.4973
  -3.000   0.3774   0.00795   0.00340  -0.1702   0.8184   0.6311
  -2.750   0.4066   0.00804   0.00353  -0.1704   0.8154   0.6686
  -2.500   0.4346   0.00825   0.00371  -0.1702   0.8128   0.6946
  -2.250   0.4616   0.00851   0.00392  -0.1698   0.8103   0.7114
  -2.000   0.4874   0.00874   0.00415  -0.1692   0.8073   0.7223
  -1.750   0.5159   0.00882   0.00419  -0.1694   0.8041   0.7284
  -1.500   0.5447   0.00887   0.00419  -0.1697   0.8009   0.7330
  -1.250   0.5724   0.00895   0.00424  -0.1697   0.7981   0.7364
  -0.750   0.6317   0.00907   0.00428  -0.1709   0.7920   0.7456
  -0.500   0.6580   0.00914   0.00436  -0.1705   0.7883   0.7484
  -0.250   0.6854   0.00921   0.00442  -0.1705   0.7851   0.7519
   0.000   0.7152   0.00927   0.00443  -0.1710   0.7822   0.7560
   0.250   0.7446   0.00931   0.00448  -0.1716   0.7785   0.7603
   0.500   0.7702   0.00936   0.00456  -0.1711   0.7742   0.7631
   0.750   0.7976   0.00939   0.00458  -0.1710   0.7700   0.7663
   1.000   0.8262   0.00941   0.00459  -0.1713   0.7652   0.7701
   1.250   0.8560   0.00940   0.00460  -0.1720   0.7597   0.7741
   1.500   0.8831   0.00941   0.00461  -0.1718   0.7556   0.7762
   1.750   0.9098   0.00945   0.00468  -0.1717   0.7510   0.7786
   2.000   0.9372   0.00946   0.00473  -0.1718   0.7456   0.7814
   2.250   0.9668   0.00947   0.00474  -0.1723   0.7409   0.7847
   2.500   0.9961   0.00948   0.00480  -0.1729   0.7348   0.7881
   2.750   1.0226   0.00947   0.00483  -0.1727   0.7290   0.7900
   3.000   1.0491   0.00950   0.00490  -0.1725   0.7230   0.7922
   3.250   1.0759   0.00952   0.00499  -0.1724   0.7160   0.7948
   3.500   1.1038   0.00954   0.00505  -0.1726   0.7086   0.7978
   3.750   1.1323   0.00955   0.00505  -0.1729   0.6975   0.8012
   4.000   1.1563   0.00953   0.00506  -0.1721   0.6800   0.8033
   4.250   1.1800   0.00958   0.00514  -0.1713   0.6619   0.8054
   4.500   1.2038   0.00971   0.00525  -0.1705   0.6432   0.8078
   4.750   1.2267   0.00991   0.00540  -0.1697   0.6166   0.8107
   5.000   1.2492   0.01022   0.00561  -0.1688   0.5852   0.8138
   5.250   1.2674   0.01073   0.00592  -0.1671   0.5412   0.8164
   5.500   1.2824   0.01131   0.00632  -0.1648   0.4968   0.8186
   5.750   1.2957   0.01202   0.00683  -0.1622   0.4464   0.8211
   6.000   1.3044   0.01301   0.00749  -0.1590   0.3788   0.8240
   6.250   1.3091   0.01430   0.00833  -0.1552   0.3024   0.8270
   6.500   1.3128   0.01546   0.00914  -0.1513   0.2378   0.8300
   6.750   1.3103   0.01696   0.01021  -0.1464   0.1621   0.8324
   7.000   1.3141   0.01827   0.01123  -0.1427   0.1124   0.8350
   7.250   1.3211   0.01947   0.01224  -0.1397   0.0757   0.8376
   7.500   1.3269   0.02084   0.01338  -0.1368   0.0410   0.8403
   7.750   1.3308   0.02246   0.01483  -0.1336   0.0137   0.8430
   8.000   1.3380   0.02373   0.01616  -0.1307   0.0081   0.8452
   8.250   1.3499   0.02472   0.01729  -0.1287   0.0073   0.8475
   8.500   1.3616   0.02579   0.01846  -0.1268   0.0066   0.8498
   8.750   1.3727   0.02697   0.01971  -0.1249   0.0059   0.8522
   9.000   1.3786   0.02863   0.02148  -0.1226   0.0051   0.8548
   9.250   1.3861   0.03023   0.02319  -0.1205   0.0049   0.8572
   9.500   1.3939   0.03167   0.02475  -0.1184   0.0047   0.8591
   9.750   1.3992   0.03336   0.02657  -0.1162   0.0046   0.8611
  10.000   1.4044   0.03513   0.02846  -0.1140   0.0044   0.8634
  10.250   1.4093   0.03700   0.03045  -0.1119   0.0042   0.8657
  10.500   1.4138   0.03895   0.03251  -0.1099   0.0041   0.8681
  10.750   1.4178   0.04103   0.03471  -0.1080   0.0039   0.8701
  11.000   1.4207   0.04316   0.03696  -0.1060   0.0038   0.8719
  11.250   1.4228   0.04535   0.03931  -0.1039   0.0037   0.8739
  11.500   1.4247   0.04762   0.04172  -0.1019   0.0036   0.8759
  11.750   1.4269   0.04998   0.04419  -0.1001   0.0034   0.8780
  12.000   1.4281   0.05252   0.04687  -0.0982   0.0034   0.8800
  12.250   1.4298   0.05511   0.04962  -0.0964   0.0034   0.8819
  12.500   1.4303   0.05799   0.05267  -0.0946   0.0033   0.8838
  12.750   1.4301   0.06095   0.05584  -0.0927   0.0033   0.8856
  13.000   1.4277   0.06428   0.05942  -0.0907   0.0034   0.8872
  13.250   1.4194   0.06879   0.06430  -0.0881   0.0037   0.8886
  13.500   1.4036   0.07443   0.07035  -0.0860   0.0040   0.8899
  13.750   1.3849   0.08043   0.07667  -0.0849   0.0042   0.8912
  14.000   1.3673   0.08629   0.08279  -0.0847   0.0043   0.8928
  14.250   1.3479   0.09270   0.08945  -0.0852   0.0045   0.8943
  14.500   1.3292   0.09921   0.09618  -0.0866   0.0046   0.8960
  14.750   1.3098   0.10626   0.10343  -0.0888   0.0047   0.8976
  15.000   1.2862   0.11450   0.11188  -0.0919   0.0048   0.8989
  15.250   1.0711   0.10143   0.09868  -0.0638   0.0040   0.8855
  15.500   1.0509   0.10679   0.10424  -0.0658   0.0041   0.8863
  15.750   1.0301   0.11244   0.11008  -0.0683   0.0041   0.8872
  16.000   1.0099   0.11829   0.11609  -0.0712   0.0042   0.8881
  16.250   0.9905   0.12437   0.12232  -0.0745   0.0042   0.8889
  16.500   0.9692   0.13094   0.12905  -0.0782   0.0043   0.8897
  16.750   0.9511   0.13743   0.13567  -0.0821   0.0043   0.8905
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