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WORTMANN FX 60-126 AIRFOIL (fx60126-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: WORTMANN FX 60-126 AIRFOIL (fx60126-il)
Reynolds number: 1,000,000
Max Cl/Cd: 112.33 at α=4.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx60126-il-1000000.txt
Download as CSV file: xf-fx60126-il-1000000.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 =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.000  -0.5596   0.08759   0.08571  -0.0474   1.0000   0.0094
 -12.750  -0.5183   0.09342   0.09164  -0.0440   1.0000   0.0098
 -12.500  -0.6582   0.05945   0.05704  -0.0663   1.0000   0.0083
 -12.250  -0.6726   0.05383   0.05131  -0.0703   1.0000   0.0083
 -12.000  -0.6926   0.04789   0.04525  -0.0743   1.0000   0.0082
 -11.750  -0.7037   0.04368   0.04094  -0.0769   1.0000   0.0082
 -11.500  -0.7192   0.03981   0.03697  -0.0784   1.0000   0.0082
 -11.250  -0.7446   0.03729   0.03440  -0.0762   1.0000   0.0082
 -11.000  -0.7262   0.03160   0.02843  -0.0880   0.9941   0.0081
 -10.750  -0.7000   0.02776   0.02432  -0.0959   0.9884   0.0081
 -10.500  -0.6713   0.02506   0.02139  -0.1007   0.9850   0.0081
 -10.250  -0.6400   0.02274   0.01885  -0.1048   0.9829   0.0081
 -10.000  -0.6120   0.02097   0.01692  -0.1071   0.9775   0.0081
  -9.750  -0.5811   0.01961   0.01542  -0.1093   0.9730   0.0082
  -9.500  -0.5494   0.01847   0.01415  -0.1114   0.9687   0.0083
  -9.250  -0.5234   0.01759   0.01317  -0.1119   0.9604   0.0084
  -9.000  -0.4969   0.01649   0.01197  -0.1127   0.9531   0.0084
  -8.750  -0.4728   0.01559   0.01096  -0.1126   0.9439   0.0085
  -8.500  -0.4477   0.01481   0.01008  -0.1127   0.9360   0.0085
  -8.250  -0.4227   0.01402   0.00921  -0.1127   0.9280   0.0086
  -8.000  -0.3983   0.01281   0.00787  -0.1130   0.9203   0.0088
  -7.750  -0.3723   0.01206   0.00702  -0.1131   0.9125   0.0091
  -7.500  -0.3452   0.01151   0.00639  -0.1132   0.9055   0.0094
  -7.250  -0.3177   0.01104   0.00587  -0.1134   0.8987   0.0098
  -7.000  -0.2900   0.01065   0.00541  -0.1135   0.8927   0.0102
  -6.750  -0.2619   0.01028   0.00498  -0.1136   0.8859   0.0107
  -6.500  -0.2338   0.00998   0.00460  -0.1137   0.8794   0.0111
  -6.250  -0.2055   0.00957   0.00412  -0.1138   0.8726   0.0118
  -6.000  -0.1771   0.00925   0.00376  -0.1139   0.8655   0.0129
  -5.750  -0.1486   0.00901   0.00345  -0.1140   0.8588   0.0142
  -5.500  -0.1199   0.00849   0.00302  -0.1144   0.8517   0.0332
  -5.250  -0.0913   0.00817   0.00274  -0.1146   0.8456   0.0502
  -5.000  -0.0623   0.00790   0.00253  -0.1149   0.8388   0.0700
  -4.750  -0.0336   0.00766   0.00232  -0.1150   0.8318   0.0864
  -4.500  -0.0047   0.00742   0.00213  -0.1153   0.8243   0.1113
  -4.250   0.0241   0.00708   0.00193  -0.1156   0.8166   0.1553
  -4.000   0.0532   0.00679   0.00176  -0.1159   0.8089   0.1970
  -3.750   0.0821   0.00656   0.00162  -0.1162   0.8009   0.2346
  -3.500   0.1112   0.00637   0.00152  -0.1164   0.7925   0.2702
  -3.250   0.1399   0.00625   0.00143  -0.1165   0.7835   0.3019
  -3.000   0.1690   0.00615   0.00137  -0.1166   0.7737   0.3223
  -2.750   0.1978   0.00610   0.00131  -0.1167   0.7640   0.3395
  -2.500   0.2264   0.00608   0.00127  -0.1167   0.7522   0.3546
  -2.250   0.2549   0.00609   0.00122  -0.1167   0.7370   0.3675
  -2.000   0.2833   0.00610   0.00119  -0.1166   0.7203   0.3795
  -1.750   0.3118   0.00612   0.00117  -0.1166   0.7036   0.3921
  -1.500   0.3402   0.00615   0.00116  -0.1166   0.6882   0.4027
  -1.250   0.3686   0.00620   0.00116  -0.1165   0.6723   0.4144
  -1.000   0.3970   0.00625   0.00117  -0.1165   0.6566   0.4266
  -0.750   0.4253   0.00630   0.00118  -0.1165   0.6408   0.4362
  -0.250   0.4819   0.00644   0.00123  -0.1164   0.6097   0.4533
   0.000   0.5101   0.00653   0.00126  -0.1163   0.5950   0.4616
   0.250   0.5383   0.00661   0.00131  -0.1163   0.5799   0.4723
   0.500   0.5665   0.00670   0.00136  -0.1163   0.5648   0.4818
   0.750   0.5947   0.00679   0.00142  -0.1162   0.5509   0.4896
   1.000   0.6228   0.00688   0.00148  -0.1162   0.5367   0.4973
   1.250   0.6508   0.00699   0.00154  -0.1161   0.5209   0.5056
   1.500   0.6789   0.00709   0.00161  -0.1161   0.5059   0.5131
   1.750   0.7070   0.00719   0.00168  -0.1161   0.4932   0.5214
   2.000   0.7350   0.00729   0.00176  -0.1160   0.4809   0.5298
   2.250   0.7628   0.00741   0.00185  -0.1159   0.4688   0.5389
   2.500   0.7906   0.00753   0.00196  -0.1159   0.4553   0.5483
   2.750   0.8184   0.00766   0.00206  -0.1158   0.4401   0.5575
   3.000   0.8459   0.00780   0.00217  -0.1157   0.4242   0.5672
   3.250   0.8732   0.00797   0.00230  -0.1156   0.4076   0.5764
   3.500   0.9004   0.00814   0.00243  -0.1154   0.3903   0.5857
   3.750   0.9275   0.00832   0.00257  -0.1153   0.3714   0.5949
   4.000   0.9543   0.00853   0.00273  -0.1151   0.3532   0.6043
   4.250   0.9810   0.00875   0.00291  -0.1149   0.3351   0.6144
   4.500   1.0076   0.00897   0.00309  -0.1147   0.3168   0.6246
   4.750   1.0339   0.00921   0.00328  -0.1144   0.2979   0.6358
   5.000   1.0602   0.00945   0.00349  -0.1142   0.2817   0.6483
   5.250   1.0864   0.00969   0.00371  -0.1139   0.2639   0.6627
   5.750   1.1370   0.01033   0.00424  -0.1132   0.2225   0.6968
   6.000   1.1611   0.01075   0.00458  -0.1126   0.1928   0.7188
   6.250   1.1851   0.01115   0.00493  -0.1121   0.1706   0.7476
   6.500   1.2095   0.01145   0.00526  -0.1116   0.1532   0.7877
   7.000   1.2512   0.01183   0.00585  -0.1089   0.1290   1.0000
   7.250   1.2764   0.01213   0.00615  -0.1085   0.1217   1.0000
   7.750   1.3248   0.01290   0.00682  -0.1075   0.1018   1.0000
   8.000   1.3485   0.01331   0.00719  -0.1069   0.0946   1.0000
   8.250   1.3715   0.01375   0.00759  -0.1062   0.0883   1.0000
   8.500   1.3956   0.01407   0.00794  -0.1056   0.0839   1.0000
   8.750   1.4187   0.01447   0.00832  -0.1049   0.0767   1.0000
   9.000   1.4406   0.01493   0.00875  -0.1041   0.0686   1.0000
   9.250   1.4617   0.01545   0.00921  -0.1031   0.0618   1.0000
   9.500   1.4824   0.01596   0.00970  -0.1021   0.0582   1.0000
   9.750   1.5020   0.01652   0.01025  -0.1009   0.0540   1.0000
  10.000   1.5229   0.01694   0.01071  -0.0999   0.0518   1.0000
  10.250   1.5437   0.01733   0.01116  -0.0989   0.0496   1.0000
  10.500   1.5619   0.01787   0.01170  -0.0975   0.0465   1.0000
  10.750   1.5756   0.01851   0.01235  -0.0954   0.0428   1.0000
  11.000   1.5923   0.01893   0.01281  -0.0937   0.0411   1.0000
  11.250   1.6064   0.01950   0.01339  -0.0917   0.0385   1.0000
  11.500   1.6181   0.02022   0.01410  -0.0895   0.0357   1.0000
  11.750   1.6313   0.02089   0.01481  -0.0875   0.0340   1.0000
  12.000   1.6438   0.02161   0.01556  -0.0856   0.0323   1.0000
  12.250   1.6546   0.02248   0.01644  -0.0836   0.0306   1.0000
  12.500   1.6639   0.02348   0.01747  -0.0815   0.0286   1.0000
  12.750   1.6754   0.02438   0.01843  -0.0798   0.0278   1.0000
  13.000   1.6874   0.02528   0.01939  -0.0783   0.0270   1.0000
  13.250   1.6977   0.02632   0.02049  -0.0767   0.0258   1.0000
  13.500   1.7064   0.02754   0.02175  -0.0750   0.0246   1.0000
  13.750   1.7128   0.02899   0.02323  -0.0734   0.0230   1.0000
  14.000   1.7218   0.03028   0.02459  -0.0720   0.0220   1.0000
  14.250   1.7308   0.03162   0.02598  -0.0708   0.0205   1.0000
  14.500   1.7348   0.03346   0.02783  -0.0695   0.0183   1.0000
  14.750   1.7396   0.03529   0.02971  -0.0683   0.0155   1.0000
  15.000   1.7329   0.03835   0.03274  -0.0670   0.0094   1.0000
  15.250   1.7247   0.04175   0.03618  -0.0659   0.0067   1.0000
  15.500   1.7202   0.04495   0.03947  -0.0653   0.0057   1.0000
  15.750   1.7167   0.04819   0.04282  -0.0650   0.0053   1.0000
  16.000   1.7115   0.05183   0.04657  -0.0650   0.0049   1.0000
  16.250   1.7075   0.05549   0.05034  -0.0652   0.0046   1.0000
  16.500   1.7038   0.05926   0.05423  -0.0658   0.0044   1.0000
  16.750   1.6996   0.06326   0.05834  -0.0665   0.0043   1.0000
  17.000   1.6935   0.06770   0.06290  -0.0676   0.0042   1.0000
  17.250   1.6862   0.07244   0.06776  -0.0690   0.0041   1.0000
  17.500   1.6769   0.07766   0.07310  -0.0706   0.0040   1.0000
  17.750   1.6665   0.08322   0.07879  -0.0726   0.0039   1.0000
  18.000   1.6548   0.08916   0.08486  -0.0750   0.0038   1.0000
  18.250   1.6417   0.09550   0.09133  -0.0776   0.0038   1.0000
  18.500   1.6274   0.10224   0.09821  -0.0806   0.0037   1.0000
  18.750   1.6116   0.10942   0.10553  -0.0840   0.0037   1.0000
  19.000   1.5957   0.11675   0.11300  -0.0877   0.0036   1.0000
  19.250   1.5788   0.12442   0.12081  -0.0917   0.0036   1.0000
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