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WORTMANN FX 60-126 AIRFOIL (fx60126-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 60-126 AIRFOIL (fx60126-il)
Reynolds number: 500,000
Max Cl/Cd: 88.35 at α=4.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx60126-il-500000-n5.txt
Download as CSV file: xf-fx60126-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 60-126 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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.750  -0.6176   0.08691   0.08397  -0.0493   1.0000   0.0068
 -13.500  -0.6562   0.07501   0.07183  -0.0565   1.0000   0.0066
 -13.250  -0.6726   0.06821   0.06491  -0.0608   1.0000   0.0066
 -13.000  -0.6890   0.06198   0.05857  -0.0647   1.0000   0.0066
 -12.750  -0.7032   0.05643   0.05290  -0.0681   1.0000   0.0066
 -12.500  -0.7169   0.05134   0.04769  -0.0712   1.0000   0.0066
 -12.250  -0.7265   0.04710   0.04334  -0.0736   1.0000   0.0066
 -12.000  -0.7362   0.04322   0.03934  -0.0755   1.0000   0.0066
 -11.750  -0.7452   0.03988   0.03591  -0.0766   1.0000   0.0066
 -11.500  -0.7581   0.03706   0.03302  -0.0763   1.0000   0.0065
 -11.250  -0.7592   0.03379   0.02963  -0.0793   0.9954   0.0066
 -11.000  -0.7356   0.02993   0.02557  -0.0873   0.9864   0.0066
 -10.750  -0.7068   0.02705   0.02249  -0.0940   0.9806   0.0067
 -10.500  -0.6797   0.02503   0.02032  -0.0977   0.9748   0.0068
 -10.250  -0.6498   0.02332   0.01846  -0.1011   0.9708   0.0069
 -10.000  -0.6223   0.02190   0.01691  -0.1033   0.9650   0.0070
  -9.750  -0.5935   0.02061   0.01550  -0.1054   0.9594   0.0072
  -9.500  -0.5631   0.01946   0.01423  -0.1075   0.9550   0.0073
  -9.250  -0.5370   0.01849   0.01316  -0.1083   0.9468   0.0075
  -9.000  -0.5083   0.01754   0.01209  -0.1095   0.9401   0.0077
  -8.750  -0.4826   0.01673   0.01118  -0.1100   0.9312   0.0078
  -8.500  -0.4553   0.01597   0.01031  -0.1105   0.9242   0.0081
  -8.250  -0.4295   0.01531   0.00955  -0.1107   0.9156   0.0082
  -8.000  -0.4024   0.01472   0.00885  -0.1110   0.9087   0.0085
  -7.750  -0.3761   0.01407   0.00812  -0.1112   0.9004   0.0087
  -7.250  -0.3216   0.01299   0.00688  -0.1116   0.8859   0.0095
  -7.000  -0.2940   0.01258   0.00637  -0.1118   0.8788   0.0099
  -6.750  -0.2663   0.01219   0.00591  -0.1119   0.8713   0.0105
  -6.500  -0.2383   0.01186   0.00549  -0.1120   0.8643   0.0112
  -6.250  -0.2102   0.01145   0.00504  -0.1122   0.8579   0.0127
  -6.000  -0.1819   0.01109   0.00463  -0.1124   0.8514   0.0153
  -5.750  -0.1536   0.01068   0.00422  -0.1126   0.8454   0.0228
  -5.500  -0.1252   0.01032   0.00389  -0.1129   0.8379   0.0377
  -5.000  -0.0682   0.00978   0.00336  -0.1132   0.8220   0.0620
  -4.750  -0.0397   0.00955   0.00311  -0.1134   0.8143   0.0767
  -4.500  -0.0110   0.00914   0.00284  -0.1138   0.8061   0.1139
  -4.250   0.0177   0.00878   0.00260  -0.1141   0.7988   0.1562
  -4.000   0.0466   0.00849   0.00241  -0.1145   0.7909   0.1930
  -3.750   0.0753   0.00831   0.00225  -0.1146   0.7826   0.2169
  -3.500   0.1041   0.00815   0.00212  -0.1148   0.7726   0.2439
  -3.250   0.1328   0.00803   0.00201  -0.1148   0.7620   0.2653
  -3.000   0.1613   0.00794   0.00191  -0.1149   0.7508   0.2885
  -2.750   0.1900   0.00787   0.00183  -0.1149   0.7393   0.3074
  -2.500   0.2186   0.00781   0.00177  -0.1150   0.7283   0.3259
  -2.250   0.2471   0.00777   0.00173  -0.1150   0.7167   0.3504
  -2.000   0.2755   0.00775   0.00170  -0.1150   0.7038   0.3705
  -1.500   0.3322   0.00780   0.00165  -0.1149   0.6760   0.3939
  -1.250   0.3603   0.00784   0.00164  -0.1148   0.6610   0.4039
  -1.000   0.3882   0.00791   0.00164  -0.1147   0.6434   0.4150
  -0.750   0.4160   0.00799   0.00165  -0.1145   0.6234   0.4267
  -0.500   0.4436   0.00808   0.00168  -0.1144   0.6032   0.4378
  -0.250   0.4713   0.00818   0.00171  -0.1142   0.5853   0.4475
   0.000   0.4992   0.00827   0.00175  -0.1141   0.5696   0.4565
   0.250   0.5270   0.00837   0.00180  -0.1140   0.5548   0.4642
   0.500   0.5549   0.00847   0.00186  -0.1139   0.5408   0.4718
   0.750   0.5826   0.00859   0.00192  -0.1138   0.5253   0.4790
   1.000   0.6103   0.00870   0.00199  -0.1137   0.5104   0.4872
   1.250   0.6381   0.00880   0.00207  -0.1136   0.4979   0.4955
   1.500   0.6657   0.00892   0.00215  -0.1135   0.4849   0.5037
   1.750   0.6934   0.00904   0.00225  -0.1134   0.4723   0.5111
   2.000   0.7211   0.00916   0.00235  -0.1133   0.4594   0.5199
   2.250   0.7484   0.00930   0.00247  -0.1132   0.4430   0.5286
   2.500   0.7754   0.00948   0.00260  -0.1130   0.4256   0.5373
   2.750   0.8025   0.00965   0.00273  -0.1128   0.4105   0.5447
   3.000   0.8296   0.00982   0.00287  -0.1126   0.3958   0.5529
   3.250   0.8564   0.01000   0.00303  -0.1124   0.3793   0.5605
   3.750   0.9094   0.01044   0.00338  -0.1119   0.3453   0.5773
   4.000   0.9358   0.01067   0.00358  -0.1117   0.3293   0.5872
   4.250   0.9621   0.01089   0.00379  -0.1114   0.3121   0.5981
   4.500   0.9878   0.01118   0.00402  -0.1111   0.2921   0.6087
   4.750   1.0132   0.01149   0.00428  -0.1107   0.2728   0.6193
   5.000   1.0383   0.01181   0.00455  -0.1103   0.2500   0.6299
   5.250   1.0633   0.01215   0.00484  -0.1099   0.2315   0.6411
   5.500   1.0885   0.01245   0.00513  -0.1095   0.2164   0.6533
   5.750   1.1132   0.01279   0.00545  -0.1090   0.1980   0.6664
   6.250   1.1618   0.01351   0.00614  -0.1080   0.1692   0.6978
   6.750   1.2080   0.01434   0.00696  -0.1066   0.1351   0.7444
   7.000   1.2303   0.01472   0.00739  -0.1058   0.1240   0.7822
   7.250   1.2479   0.01477   0.00770  -0.1037   0.1153   0.8821
   7.500   1.2692   0.01513   0.00807  -0.1026   0.1045   1.0000
   7.750   1.2917   0.01560   0.00850  -0.1019   0.0966   1.0000
   8.000   1.3144   0.01605   0.00893  -0.1012   0.0914   1.0000
   8.250   1.3361   0.01654   0.00942  -0.1003   0.0863   1.0000
   8.500   1.3590   0.01691   0.00983  -0.0996   0.0827   1.0000
   8.750   1.3806   0.01736   0.01030  -0.0987   0.0765   1.0000
   9.000   1.4008   0.01788   0.01082  -0.0977   0.0703   1.0000
   9.250   1.4199   0.01846   0.01137  -0.0965   0.0637   1.0000
   9.500   1.4384   0.01903   0.01195  -0.0952   0.0601   1.0000
   9.750   1.4546   0.01964   0.01256  -0.0935   0.0569   1.0000
  10.000   1.4687   0.02030   0.01324  -0.0915   0.0536   1.0000
  10.250   1.4840   0.02088   0.01387  -0.0897   0.0516   1.0000
  10.500   1.4992   0.02146   0.01452  -0.0879   0.0493   1.0000
  10.750   1.5126   0.02218   0.01529  -0.0861   0.0464   1.0000
  11.000   1.5238   0.02305   0.01619  -0.0840   0.0436   1.0000
  11.250   1.5368   0.02383   0.01703  -0.0823   0.0413   1.0000
  11.500   1.5493   0.02468   0.01792  -0.0806   0.0388   1.0000
  11.750   1.5601   0.02568   0.01894  -0.0789   0.0363   1.0000
  12.000   1.5702   0.02676   0.02006  -0.0772   0.0342   1.0000
  12.250   1.5804   0.02787   0.02124  -0.0756   0.0327   1.0000
  12.500   1.5898   0.02909   0.02251  -0.0741   0.0312   1.0000
  12.750   1.5979   0.03046   0.02393  -0.0726   0.0298   1.0000
  13.000   1.6048   0.03199   0.02551  -0.0712   0.0284   1.0000
  13.250   1.6129   0.03347   0.02708  -0.0700   0.0274   1.0000
  13.500   1.6202   0.03506   0.02876  -0.0688   0.0265   1.0000
  13.750   1.6265   0.03683   0.03061  -0.0678   0.0254   1.0000
  14.000   1.6314   0.03879   0.03265  -0.0669   0.0242   1.0000
  14.250   1.6343   0.04103   0.03495  -0.0661   0.0230   1.0000
  14.500   1.6382   0.04325   0.03727  -0.0655   0.0220   1.0000
  14.750   1.6422   0.04555   0.03966  -0.0650   0.0209   1.0000
  15.000   1.6443   0.04813   0.04233  -0.0647   0.0197   1.0000
  15.250   1.6443   0.05106   0.04534  -0.0646   0.0184   1.0000
  15.500   1.6442   0.05413   0.04851  -0.0647   0.0171   1.0000
  15.750   1.6439   0.05735   0.05182  -0.0650   0.0154   1.0000
  16.000   1.6408   0.06106   0.05561  -0.0655   0.0135   1.0000
  16.250   1.6352   0.06528   0.05990  -0.0664   0.0106   1.0000
  16.500   1.6248   0.07035   0.06504  -0.0677   0.0081   1.0000
  16.750   1.6150   0.07552   0.07032  -0.0693   0.0071   1.0000
  17.000   1.6037   0.08113   0.07604  -0.0712   0.0063   1.0000
  17.250   1.5935   0.08672   0.08177  -0.0733   0.0058   1.0000
  17.500   1.5821   0.09267   0.08785  -0.0756   0.0055   1.0000
  17.750   1.5701   0.09887   0.09418  -0.0783   0.0052   1.0000
  18.000   1.5574   0.10536   0.10082  -0.0812   0.0050   1.0000
  18.250   1.5446   0.11202   0.10761  -0.0844   0.0048   1.0000
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